[ISSTLE LIST] 2010-08-01T00:22:04Z [ISSTLE LIST] List Owner list.admin@aus-city.com http://www.aus-city.com/cgi-bin/dada/mail.cgi Pro Dada 4.1.0 Stable 06/09/10 [ISSTLE LIST] Current ISS TLEs @ 18:30 UTC tag:www.aus-city.com,2010-08-01:%2Fcgi-bin%2Fdada%2Fmail.cgi%2Farchive%2FISSTLE_LIST%2F20100801044502%2F 2010-08-01T04:45:02Z 2010-08-01T04:45:02Z <p>&#60;B&#62; ISS TRAJECTORY DATA&#60;/B&#62; </p><p> Lift off time (UTC) : N/A<br/> Area (sq ft) : 9149.32<br/> Drag Coefficient (Cd) : 2.00<br/> Monthly MSFC 50% solar flux (F10.7-jansky) : 74.8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0.74 ET - UTC (sec) : 66.18<br/> UT1 - UTC (sec) : 0.00 </p><p> Maneuvers contained within the current ephemeris are as follows: </p><pre> IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP </pre> <hr/> There are no maneuvers. <p> Coasting Arc #1 (Orbit 3028) </p><hr/> <p> Vector Time (GMT): 2010/211/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5886772.53 A = 6736192.33 meter Y = 1453024.09 meter E = .0017697 Z = 2909467.41 I = 51.70110 XDOT = -3624.406982 Wp = 121.91121 YDOT = -4560.767225 meter/sec RA = 8.40280 deg ZDOT = -5042.500272 TA = 24.63621 MA = 24.55178 Ha = 196.145 n.mi Hp = 186.771 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -19313558.18 X = -5916716.47 Y = 4767139.42 feet Y = 1387027.14 meter Z = 9545496.75 Z = 2880797.19 XDOT = -11891.099021 XDOT = -3548.643054 YDOT = -14963.147063 feet/sec YDOT = -4600.873679 meter/sec ZDOT = -16543.636064 ZDOT = -5059.923567 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15517127.17 X = 4729620.36 Y = 12535298.83 feet Y = 3820759.08 meter Z = 9430837.90 Z = 2874519.39 XDOT = -3861.988708 XDOT = -1177.134158 YDOT = 17312.292654 feet/sec YDOT = 5276.786801 meter/sec ZDOT = -16613.263137 ZDOT = -5063.722604 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10211.53766810 .00016717 00000-0 10270-3 0 9008 2 25544 51.6422 8.7446 0007649 167.4000 192.7355 15.71333273 30296 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10211.53766810 = yrday.fracday Element set: 900 Inclination: 51.6422 deg RA of node: 8.7446 deg Eccentricity: .0007649 Arg of perigee: 167.4000 deg Mean anomaly: 192.7355 deg </pre> <p> Mean motion: 15.71333273 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3029 Checksum: 288 </pre> <p> Coasting Arc #2 (Orbit 3044) </p><hr/> <p> Vector Time (GMT): 2010/212/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4403939.30 A = 6733087.50 meter Y = 3316504.31 meter E = .0015483 Z = 3862163.07 I = 51.66218 XDOT = -5817.533868 Wp = 127.13796 YDOT = 2915.774610 meter/sec RA = 3.33999 deg ZDOT = 4109.325400 TA = 279.87419 MA = 280.04895 Ha = 195.851 n.mi Hp = 186.803 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 14448619.76 X = 4347764.73 Y = 10880919.65 feet Y = 3365437.54 meter Z = 12671138.68 Z = 3883420.89 XDOT = -19086.397205 XDOT = -5869.668385 YDOT = 9566.189665 feet/sec YDOT = 2850.427797 meter/sec ZDOT = 13482.038713 ZDOT = 4080.937582 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -345548.62 X = -105323.22 Y = -18024347.84 feet Y = -5493821.22 meter Z = 12756106.85 Z = 3888061.37 XDOT = 18060.093134 XDOT = 5504.716387 YDOT = 9162.037204 feet/sec YDOT = 2792.588940 meter/sec ZDOT = 13368.499903 ZDOT = 4074.718770 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10212.55521023 .00016717 00000-0 10270-3 0 9017 2 25544 51.6431 3.5398 0007677 171.3351 188.7945 15.71382511 30456 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10212.55521023 = yrday.fracday Element set: 901 Inclination: 51.6431 deg RA of node: 3.5398 deg Eccentricity: .0007677 Arg of perigee: 171.3351 deg Mean anomaly: 188.7945 deg </pre> <p> Mean motion: 15.71382511 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3045 Checksum: 287 </pre> <p> Coasting Arc #3 (Orbit 3059) </p><hr/> <p> Vector Time (GMT): 2010/213/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4034796.50 A = 6732241.50 meter Y = -3431398.38 meter E = .0013066 Z = -4169465.53 I = 51.62973 XDOT = 6154.530716 Wp = 140.96198 YDOT = 2735.484062 meter/sec RA = 358.17491 deg ZDOT = 3700.820262 TA = 166.95153 MA = 166.91770 Ha = 195.823 n.mi Hp = 187.068 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 13237521.32 X = 4093121.53 Y = -11257868.70 feet Y = -3385952.56 meter Z = -13679348.84 Z = -4149723.10 XDOT = 20192.029908 XDOT = 6105.506814 YDOT = 8974.685243 feet/sec YDOT = 2804.033420 meter/sec ZDOT = 12141.798759 ZDOT = 3730.599834 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -17142740.47 X = -5225107.29 Y = -3201932.10 feet Y = -975948.90 meter Z = -13600376.58 Z = -4145394.78 XDOT = -5998.832653 XDOT = -1828.444193 YDOT = -20013.019266 feet/sec YDOT = -6099.968272 meter/sec ZDOT = 12260.841561 ZDOT = 3737.104508 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10213.50914917 .00016717 00000-0 10270-3 0 9022 2 25544 51.6442 358.6609 0007609 174.0799 186.0454 15.71370390 30603 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10213.50914917 = yrday.fracday Element set: 902 Inclination: 51.6442 deg RA of node: 358.6609 deg Eccentricity: .0007609 Arg of perigee: 174.0799 deg Mean anomaly: 186.0454 deg </pre> <p> Mean motion: 15.71370390 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3060 Checksum: 309 </pre> <p> Coasting Arc #4 (Orbit 3075) </p><hr/> <p> Vector Time (GMT): 2010/214/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -6097573.56 A = 6736715.92 meter Y = -1291998.91 meter E = .0011505 Z = -2543244.12 I = 51.61493 XDOT = 3174.176473 Wp = 157.68464 YDOT = -4604.441598 meter/sec RA = 353.10498 deg ZDOT = -5289.396247 TA = 51.12935 MA = 51.02676 Ha = 195.573 n.mi Hp = 187.096 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -20005162.59 X = -6070318.44 Y = -4238841.58 feet Y = -1360033.08 meter Z = -8343976.77 Z = -2572799.88 XDOT = 10413.964808 XDOT = 3251.123090 YDOT = -15106.435690 feet/sec YDOT = -4568.515509 meter/sec ZDOT = -17353.662229 ZDOT = -5273.789536 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 9641619.94 X = 2938765.76 Y = 17978534.22 feet Y = 5479857.23 meter Z = -8462135.01 Z = -2579258.75 XDOT = -17015.707449 XDOT = -5186.387631 YDOT = 1014.413853 feet/sec YDOT = 309.193342 meter/sec ZDOT = -17291.214696 ZDOT = -5270.362239 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10214.52667404 .00016717 00000-0 10270-3 0 9032 2 25544 51.6440 353.4557 0007532 178.1212 181.9980 15.71393501 30760 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10214.52667404 = yrday.fracday Element set: 903 Inclination: 51.6440 deg RA of node: 353.4557 deg Eccentricity: .0007532 Arg of perigee: 178.1212 deg Mean anomaly: 181.9980 deg </pre> <p> Mean motion: 15.71393501 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3076 Checksum: 296 </pre> <p> Coasting Arc #5 (Orbit 3091) </p><hr/> <p> Vector Time (GMT): 2010/215/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1371872.07 A = 6729001.25 meter Y = 4322991.60 meter E = .0006436 Z = 4965333.78 I = 51.55905 XDOT = -7432.911066 Wp = 129.85057 YDOT = -47.895012 meter/sec RA = 347.94790 deg ZDOT = -2014.273460 TA = 339.64444 MA = 339.67008 Ha = 195.625 n.mi Hp = 187.310 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4500892.63 X = -1444231.20 Y = 14183043.29 feet Y = 4307245.54 meter Z = 16290465.16 Z = 4958493.82 XDOT = -24386.191162 XDOT = -7422.038122 YDOT = -157.135866 feet/sec YDOT = -130.953320 meter/sec ZDOT = -6608.508727 ZDOT = -2050.356009 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13701883.08 X = 4176333.96 Y = -5879363.79 feet Y = -1792030.08 meter Z = 16263071.30 Z = 4956984.13 XDOT = 15484.161929 XDOT = 4719.572556 YDOT = 17428.087009 feet/sec YDOT = 5312.080920 meter/sec ZDOT = -6752.773111 ZDOT = -2058.245244 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10215.54419145 .00016717 00000-0 10270-3 0 9043 2 25544 51.6444 348.2512 0007526 181.0944 179.0203 15.71367854 30921 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10215.54419145 = yrday.fracday Element set: 904 Inclination: 51.6444 deg RA of node: 348.2512 deg Eccentricity: .0007526 Arg of perigee: 181.0944 deg Mean anomaly: 179.0203 deg </pre> <p> Mean motion: 15.71367854 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3092 Checksum: 298 </pre> <p> Coasting Arc #6 (Orbit 3107) </p><hr/> <p> Vector Time (GMT): 2010/216/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6555126.59 A = 6739080.95 meter Y = -1237044.90 meter E = .0010593 Z = 945855.02 I = 51.56530 XDOT = 61.906571 Wp = 88.01616 YDOT = 4903.216536 meter/sec RA = 342.85250 deg ZDOT = 5926.981240 TA = 282.30813 MA = 282.42671 Ha = 195.373 n.mi Hp = 187.380 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 21506320.83 X = 6563877.49 Y = -4058546.25 feet Y = -1163692.71 meter Z = 3103198.89 Z = 977720.82 XDOT = 203.105548 XDOT = -21.718756 YDOT = 16086.668426 feet/sec YDOT = 4903.440688 meter/sec ZDOT = 19445.476510 ZDOT = 5927.079311 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -17432840.66 X = -5313529.83 Y = -13201615.44 feet Y = -4023852.39 meter Z = 3230618.03 Z = 984692.37 XDOT = 10901.806470 XDOT = 3322.870612 YDOT = -9593.538187 feet/sec YDOT = -2924.110439 meter/sec ZDOT = 19445.814717 ZDOT = 5927.084326 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10216.56169618 .00016717 00000-0 10270-3 0 9054 2 25544 51.6454 343.0463 0007480 185.6533 174.4545 15.71429694 31080 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10216.56169618 = yrday.fracday Element set: 905 Inclination: 51.6454 deg RA of node: 343.0463 deg Eccentricity: .0007480 Arg of perigee: 185.6533 deg Mean anomaly: 174.4545 deg </pre> <p> Mean motion: 15.71429694 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3108 Checksum: 318 </pre> <p> Coasting Arc #7 (Orbit 3122) </p><hr/> <p> Vector Time (GMT): 2010/217/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1430093.20 A = 6727390.25 meter Y = -3944958.80 meter E = .0015772 Z = -5270397.92 I = 51.49756 XDOT = 7155.643262 Wp = 118.52036 YDOT = -2803.326845 meter/sec RA = 337.71910 deg ZDOT = 149.623062 TA = 152.94608 MA = 152.86379 Ha = 195.163 n.mi Hp = 187.519 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4691906.82 X = -1360271.22 Y = -12942778.21 feet Y = -3960560.00 meter Z = -17291331.76 Z = -5277176.08 XDOT = 23476.519890 XDOT = 7185.731915 YDOT = -9197.266551 feet/sec YDOT = -2723.139946 meter/sec ZDOT = 490.889312 ZDOT = 184.457695 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -6303435.90 X = -1921287.26 Y = 12200808.82 feet Y = 3718806.53 meter Z = -17318389.39 Z = -5278645.09 XDOT = -21874.601567 XDOT = -6667.378558 YDOT = -10373.961954 feet/sec YDOT = -3161.983604 meter/sec ZDOT = 630.198039 ZDOT = 192.084362 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10217.51560057 .00016717 00000-0 10270-3 0 9063 2 25544 51.6455 338.1675 0007331 189.5309 170.5715 15.71451001 31230 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10217.51560057 = yrday.fracday Element set: 906 Inclination: 51.6455 deg RA of node: 338.1675 deg Eccentricity: .0007331 Arg of perigee: 189.5309 deg Mean anomaly: 170.5715 deg </pre> <p> Mean motion: 15.71451001 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3123 Checksum: 287 </pre> <p> Coasting Arc #8 (Orbit 3138) </p><hr/> <p> Vector Time (GMT): 2010/218/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5668315.21 A = 6739293.94 meter Y = 3558442.54 meter E = .0017708 Z = 690817.10 I = 51.51017 XDOT = -3089.554469 Wp = 149.97622 YDOT = -3751.257183 meter/sec RA = 332.58813 deg ZDOT = -5976.821625 TA = 22.48622 MA = 22.40871 Ha = 195.060 n.mi Hp = 187.805 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -18596834.68 X = -5711040.91 Y = 11674680.26 feet Y = 3494817.08 meter Z = 2266460.30 Z = 663177.38 XDOT = -10136.333561 XDOT = -3018.343645 YDOT = -12307.274222 feet/sec YDOT = -3785.407593 meter/sec ZDOT = -19608.994833 ZDOT = -5991.657951 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 21338438.78 X = 6503956.14 Y = 5224973.79 feet Y = 1592572.01 meter Z = 2155908.42 Z = 657120.89 XDOT = -1473.701921 XDOT = -449.184346 YDOT = 14206.142288 feet/sec YDOT = 4330.032169 meter/sec ZDOT = -19668.276580 ZDOT = -5994.890702 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10218.53308976 .00016717 00000-0 10270-3 0 9077 2 25544 51.6457 332.9620 0007380 193.6676 166.4287 15.71439190 31391 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10218.53308976 = yrday.fracday Element set: 907 Inclination: 51.6457 deg RA of node: 332.9620 deg Eccentricity: .0007380 Arg of perigee: 193.6676 deg Mean anomaly: 166.4287 deg </pre> <p> Mean motion: 15.71439190 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3139 Checksum: 332 </pre> <p> Coasting Arc #9 (Orbit 3154) </p><hr/> <p> Vector Time (GMT): 2010/219/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3785930.69 A = 6728196.49 meter Y = 2351004.55 meter E = .0010105 Z = 5041444.49 I = 51.44802 XDOT = -5482.734137 Wp = 168.43646 YDOT = 5120.218712 meter/sec RA = 327.48149 deg ZDOT = 1719.241985 TA = 264.90851 MA = 265.02386 Ha = 194.735 n.mi Hp = 187.911 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12421032.46 X = 3734869.96 Y = 7713269.53 feet Y = 2393055.06 meter Z = 16540172.23 Z = 5059712.45 XDOT = -17987.972890 XDOT = -5547.933489 YDOT = 16798.617821 feet/sec YDOT = 5058.542769 meter/sec ZDOT = 5640.557693 ZDOT = 1692.449509 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -3290009.02 X = -1002794.75 Y = -14160913.50 feet Y = -4316246.43 meter Z = 16613194.79 Z = 5063701.77 XDOT = 23590.558399 XDOT = 7190.402200 YDOT = 1050.430793 feet/sec YDOT = 320.171306 meter/sec ZDOT = 5533.377431 ZDOT = 1686.573441 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10219.55056819 .00016717 00000-0 10270-3 0 9087 2 25544 51.6466 327.7571 0007280 198.1513 161.9390 15.71494074 31552 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10219.55056819 = yrday.fracday Element set: 908 Inclination: 51.6466 deg RA of node: 327.7571 deg Eccentricity: .0007280 Arg of perigee: 198.1513 deg Mean anomaly: 161.9390 deg </pre> <p> Mean motion: 15.71494074 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3155 Checksum: 323 </pre> <p> Coasting Arc #10 (Orbit 3169) </p><hr/> <p> Vector Time (GMT): 2010/220/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3711722.68 A = 6737266.64 meter Y = -5148078.37 meter E = .0002595 Z = -2265936.53 I = 51.45323 XDOT = 5260.943075 Wp = 146.10152 YDOT = 1403.406083 meter/sec RA = 322.31852 deg ZDOT = 5430.112501 TA = 188.43582 MA = 188.44018 Ha = 194.686 n.mi Hp = 188.243 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12177567.86 X = 3780020.84 Y = -16890020.90 feet Y = -5106189.59 meter Z = -7434174.98 Z = -2247739.94 XDOT = 17260.311926 XDOT = 5218.481016 YDOT = 4604.350667 feet/sec YDOT = 1461.999206 meter/sec ZDOT = 17815.329729 ZDOT = 5455.566575 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -20517180.26 X = -6253636.54 Y = 3699792.73 feet Y = 1127696.83 meter Z = -7361370.16 Z = -2243745.62 XDOT = -8900.665088 XDOT = -2712.922719 YDOT = -13715.194095 feet/sec YDOT = -4180.391160 meter/sec ZDOT = 17917.100945 ZDOT = 5461.132368 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10220.50444842 .00016717 00000-0 10270-3 0 9092 2 25544 51.6467 322.8780 0007067 202.3646 157.7209 15.71446669 31705 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10220.50444842 = yrday.fracday Element set: 909 Inclination: 51.6467 deg RA of node: 322.8780 deg Eccentricity: .0007067 Arg of perigee: 202.3646 deg Mean anomaly: 157.7209 deg </pre> <p> Mean motion: 15.71446669 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3170 Checksum: 311 </pre> <p> Coasting Arc #11 (Orbit 3185) </p><hr/> <p> Vector Time (GMT): 2010/221/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5136470.09 A = 6731045.96 meter Y = 19200.35 meter E = .0006339 Z = -4352924.83 I = 51.40944 XDOT = 2836.922562 Wp = 120.34210 YDOT = -6300.690623 meter/sec RA = 317.23213 deg ZDOT = -3382.184244 TA = 115.46472 MA = 115.39913 Ha = 194.460 n.mi Hp = 188.229 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -16851935.99 X = -5115157.85 Y = 62993.27 feet Y = -38119.32 meter Z = -14281249.43 Z = -4377825.41 XDOT = 9307.488719 XDOT = 2923.596817 YDOT = -20671.557161 feet/sec YDOT = -6268.481645 meter/sec ZDOT = -11096.405000 ZDOT = -3368.192649 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 12324415.10 X = 3756481.72 Y = 11368666.12 feet Y = 3465169.43 meter Z = -14380821.37 Z = -4383274.35 XDOT = -20109.514053 XDOT = -6129.379883 YDOT = 7862.568548 feet/sec YDOT = 2396.510893 meter/sec ZDOT = -11040.415039 ZDOT = -3365.118504 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10221.52191099 .00016717 00000-0 10270-3 0 9100 2 25544 51.6466 317.6735 0007190 205.8403 154.2401 15.71473815 31868 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10221.52191099 = yrday.fracday Element set: 910 Inclination: 51.6466 deg RA of node: 317.6735 deg Eccentricity: .0007190 Arg of perigee: 205.8403 deg Mean anomaly: 154.2401 deg </pre> <p> Mean motion: 15.71473815 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3186 Checksum: 292 </pre> <p> Coasting Arc #12 (Orbit 3201) </p><hr/> <p> Vector Time (GMT): 2010/222/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1164305.44 A = 6733743.18 meter Y = 5569201.58 meter E = .0010216 Z = 3589218.91 I = 51.39680 XDOT = -6129.108029 Wp = 121.32462 YDOT = 1554.579537 meter/sec RA = 312.04998 deg ZDOT = -4396.411965 TA = 15.61791 MA = 15.58642 Ha = 194.351 n.mi Hp = 188.451 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -3819899.73 X = -1243930.08 Y = 18271658.73 feet Y = 5555736.33 meter Z = 11775652.59 Z = 3583369.59 XDOT = -20108.622144 XDOT = -6124.679645 YDOT = 5100.326564 feet/sec YDOT = 1486.065050 meter/sec ZDOT = -14423.923771 ZDOT = -4426.175647 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15101194.47 X = 4602844.08 Y = -10997726.66 feet Y = -3352107.09 meter Z = 11752237.00 Z = 3582081.84 XDOT = 17504.086811 XDOT = 5335.245660 YDOT = 8480.588989 feet/sec YDOT = 2584.883524 meter/sec ZDOT = -14542.949406 ZDOT = -4432.690979 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10222.53936499 .00016717 00000-0 10270-3 0 9114 2 25544 51.6463 312.4690 0006979 208.8906 151.1870 15.71495421 32025 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10222.53936499 = yrday.fracday Element set: 911 Inclination: 51.6463 deg RA of node: 312.4690 deg Eccentricity: .0006979 Arg of perigee: 208.8906 deg Mean anomaly: 151.1870 deg </pre> <p> Mean motion: 15.71495421 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3202 Checksum: 313 </pre> <p> Coasting Arc #13 (Orbit 3217) </p><hr/> <p> Vector Time (GMT): 2010/223/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 5258542.94 A = 6734559.54 meter Y = -2674023.07 meter E = .0010418 Z = 3246535.46 I = 51.38045 XDOT = 157.914461 Wp = 121.09529 YDOT = 6069.261879 meter/sec RA = 306.96651 deg ZDOT = 4726.693877 TA = 277.00825 MA = 277.12673 Ha = 194.122 n.mi Hp = 188.556 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 17252437.46 X = 5272282.77 Y = -8773041.57 feet Y = -2615142.07 meter Z = 10651363.05 Z = 3272114.30 XDOT = 518.092064 XDOT = 67.074181 YDOT = 19912.276505 feet/sec YDOT = 6070.519859 meter/sec ZDOT = 15507.525842 ZDOT = 4727.240360 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -18733617.04 X = -5710006.47 Y = -4634104.42 feet Y = -1412475.03 meter Z = 10753653.35 Z = 3277713.54 XDOT = 12386.302565 XDOT = 3775.345022 YDOT = -13956.911682 feet/sec YDOT = -4254.066681 meter/sec ZDOT = 15509.693915 ZDOT = 4727.354705 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10223.55680824 .00016717 00000-0 10270-3 0 9126 2 25544 51.6461 307.2636 0007007 213.6571 146.4147 15.71531311 32180 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10223.55680824 = yrday.fracday Element set: 912 Inclination: 51.6461 deg RA of node: 307.2636 deg Eccentricity: .0007007 Arg of perigee: 213.6571 deg Mean anomaly: 146.4147 deg </pre> <p> Mean motion: 15.71531311 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3218 Checksum: 280 </pre> <p> Coasting Arc #14 (Orbit 3232) </p><hr/> <p> Vector Time (GMT): 2010/224/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1361085.73 A = 6730051.23 meter Y = -4752248.11 meter E = .0010606 Z = -4576215.72 I = 51.34718 XDOT = 5535.616561 Wp = 147.89623 YDOT = -4440.417348 meter/sec RA = 301.78372 deg ZDOT = 2959.085518 TA = 151.65831 MA = 151.60058 Ha = 193.927 n.mi Hp = 188.677 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4465504.37 X = -1285613.98 Y = -15591365.17 feet Y = -4767046.65 meter Z = -15013831.09 Z = -4582644.40 XDOT = 18161.471658 XDOT = 5570.484220 YDOT = -14568.298385 feet/sec YDOT = -4378.319781 meter/sec ZDOT = 9708.285819 ZDOT = 2986.061870 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -6655967.34 X = -2028738.84 Y = 14763372.02 feet Y = 4499875.79 meter Z = -15039530.14 Z = -4584048.79 XDOT = -22156.188064 XDOT = -6753.206122 YDOT = 29.840209 feet/sec YDOT = 9.095296 meter/sec ZDOT = 9816.160431 ZDOT = 2991.965699 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10224.51065509 .00016717 00000-0 10270-3 0 9131 2 25544 51.6452 302.3844 0006843 217.1411 142.9279 15.71554390 32332 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10224.51065509 = yrday.fracday Element set: 913 Inclination: 51.6452 deg RA of node: 302.3844 deg Eccentricity: .0006843 Arg of perigee: 217.1411 deg Mean anomaly: 142.9279 deg </pre> <p> Mean motion: 15.71554390 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3233 Checksum: 287 </pre> <p> Coasting Arc #15 (Orbit 3248) </p><hr/> <p> Vector Time (GMT): 2010/225/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4165371.74 A = 6737637.36 meter Y = 4942250.42 meter E = .0010604 Z = -1878727.23 I = 51.35679 XDOT = -2778.228543 Wp = 180.16326 YDOT = -4472.865737 meter/sec RA = 296.68621 deg ZDOT = -5617.175003 TA = 20.77501 MA = 20.73194 Ha = 193.709 n.mi Hp = 188.952 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -13665917.80 X = -4211200.89 Y = 16214732.35 feet Y = 4895414.48 meter Z = -6163803.25 Z = -1899073.76 XDOT = -9114.923042 XDOT = -2700.718710 YDOT = -14674.756356 feet/sec YDOT = -4503.500214 meter/sec ZDOT = -18429.051846 ZDOT = -5630.483197 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 20793261.04 X = 6337785.97 Y = -4038016.06 feet Y = -1230787.30 meter Z = -6245161.86 Z = -1903525.33 XDOT = -2519.739768 XDOT = -768.016681 YDOT = 15557.522047 feet/sec YDOT = 4741.932720 meter/sec ZDOT = -18482.262817 ZDOT = -5633.393706 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10225.52808320 .00016717 00000-0 10270-3 0 9140 2 25544 51.6443 297.1789 0006813 221.4446 138.6200 15.71532026 32499 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10225.52808320 = yrday.fracday Element set: 914 Inclination: 51.6443 deg RA of node: 297.1789 deg Eccentricity: .0006813 Arg of perigee: 221.4446 deg Mean anomaly: 138.6200 deg </pre> <p> Mean motion: 15.71532026 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3249 Checksum: 293</pre> <hr/> <p><strong>INTERNATIONAL SPACE STATION ORBITAL DATA:</strong> </p> <p>The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability. The data normally contains past, current and predicted orbital data. Careful attention to the orbit # / epoch times! These sources include: </p><p>NASA Orbital Flight Dynamics<br/> DOD C-Band Radar Network<br/> Goddard Space Flight Center (GSFC)<br/> NASA Johnson Space Center (JSC)<br/> DoD/ USSTRATCOM/ US Space Command with permission </p> <p>By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command. </p><pre> David Cottle Director Of Engineering IDB Communications</pre> <hr/> <p>The following information is a reminder of your current mailing list subscription: </p><p>You are subscribed to the following list: </p><p><strong>[ISSTLE LIST]</strong> </p><p>using the following email: </p><p> <a href="mailto:&#101;&#x78;&#x61;&#x6D;&#x70;&#108;&#101;&#x40;&#x65;&#120;&#x61;&#109;&#x70;&#x6C;&#101;&#46;&#99;&#111;&#109;">&#101;&#x78;&#x61;&#x6D;&#x70;&#108;&#101;&#x40;&#x65;&#120;&#x61;&#109;&#x70;&#x6C;&#101;&#46;&#99;&#111;&#109;</a> </p><p>You may automatically unsubscribe from this list at any time by visiting the following URL: </p><p>&#60;<a href="http://www.aus-city.com/cgi-bin/dada/mail.cgi/u/ISSTLE_LIST/example/example.com/">http://www.aus-city.com/cgi-bin/dada/mail.cgi/u/ISSTLE_LIST/example/example.com/</a>&#62; </p><p>If the above URL is inoperable, make sure that you have copied the entire address. 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subscription_form_widget.tmpl --> [ISSTLE LIST] Current ISS TLEs @ 06:30 UTC tag:www.aus-city.com,2010-07-31:%2Fcgi-bin%2Fdada%2Fmail.cgi%2Farchive%2FISSTLE_LIST%2F20100731164502%2F 2010-07-31T16:45:02Z 2010-07-31T16:45:02Z <p>&#60;B&#62; ISS TRAJECTORY DATA&#60;/B&#62; </p><p> Lift off time (UTC) : N/A<br/> Area (sq ft) : 9149.32<br/> Drag Coefficient (Cd) : 2.00<br/> Monthly MSFC 50% solar flux (F10.7-jansky) : 74.8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0.74 ET - UTC (sec) : 66.18<br/> UT1 - UTC (sec) : 0.00 </p><p> Maneuvers contained within the current ephemeris are as follows: </p><pre> IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP </pre> <hr/> There are no maneuvers. <p> Coasting Arc #1 (Orbit 3028) </p><hr/> <p> Vector Time (GMT): 2010/211/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5886772.53 A = 6736192.33 meter Y = 1453024.09 meter E = .0017697 Z = 2909467.41 I = 51.70110 XDOT = -3624.406982 Wp = 121.91121 YDOT = -4560.767225 meter/sec RA = 8.40280 deg ZDOT = -5042.500272 TA = 24.63621 MA = 24.55178 Ha = 196.145 n.mi Hp = 186.771 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -19313558.18 X = -5916716.47 Y = 4767139.42 feet Y = 1387027.14 meter Z = 9545496.75 Z = 2880797.19 XDOT = -11891.099021 XDOT = -3548.643054 YDOT = -14963.147063 feet/sec YDOT = -4600.873679 meter/sec ZDOT = -16543.636064 ZDOT = -5059.923567 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15517127.17 X = 4729620.36 Y = 12535298.83 feet Y = 3820759.08 meter Z = 9430837.90 Z = 2874519.39 XDOT = -3861.988708 XDOT = -1177.134158 YDOT = 17312.292654 feet/sec YDOT = 5276.786801 meter/sec ZDOT = -16613.263137 ZDOT = -5063.722604 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10211.53766810 .00016717 00000-0 10270-3 0 9008 2 25544 51.6422 8.7446 0007649 167.4000 192.7355 15.71333273 30296 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10211.53766810 = yrday.fracday Element set: 900 Inclination: 51.6422 deg RA of node: 8.7446 deg Eccentricity: .0007649 Arg of perigee: 167.4000 deg Mean anomaly: 192.7355 deg </pre> <p> Mean motion: 15.71333273 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3029 Checksum: 288 </pre> <p> Coasting Arc #2 (Orbit 3044) </p><hr/> <p> Vector Time (GMT): 2010/212/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4403939.30 A = 6733087.50 meter Y = 3316504.31 meter E = .0015483 Z = 3862163.07 I = 51.66218 XDOT = -5817.533868 Wp = 127.13796 YDOT = 2915.774610 meter/sec RA = 3.33999 deg ZDOT = 4109.325400 TA = 279.87419 MA = 280.04895 Ha = 195.851 n.mi Hp = 186.803 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 14448619.76 X = 4347764.73 Y = 10880919.65 feet Y = 3365437.54 meter Z = 12671138.68 Z = 3883420.89 XDOT = -19086.397205 XDOT = -5869.668385 YDOT = 9566.189665 feet/sec YDOT = 2850.427797 meter/sec ZDOT = 13482.038713 ZDOT = 4080.937582 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -345548.62 X = -105323.22 Y = -18024347.84 feet Y = -5493821.22 meter Z = 12756106.85 Z = 3888061.37 XDOT = 18060.093134 XDOT = 5504.716387 YDOT = 9162.037204 feet/sec YDOT = 2792.588940 meter/sec ZDOT = 13368.499903 ZDOT = 4074.718770 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10212.55521023 .00016717 00000-0 10270-3 0 9017 2 25544 51.6431 3.5398 0007677 171.3351 188.7945 15.71382511 30456 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10212.55521023 = yrday.fracday Element set: 901 Inclination: 51.6431 deg RA of node: 3.5398 deg Eccentricity: .0007677 Arg of perigee: 171.3351 deg Mean anomaly: 188.7945 deg </pre> <p> Mean motion: 15.71382511 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3045 Checksum: 287 </pre> <p> Coasting Arc #3 (Orbit 3059) </p><hr/> <p> Vector Time (GMT): 2010/213/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4034796.50 A = 6732241.50 meter Y = -3431398.38 meter E = .0013066 Z = -4169465.53 I = 51.62973 XDOT = 6154.530716 Wp = 140.96198 YDOT = 2735.484062 meter/sec RA = 358.17491 deg ZDOT = 3700.820262 TA = 166.95153 MA = 166.91770 Ha = 195.823 n.mi Hp = 187.068 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 13237521.32 X = 4093121.53 Y = -11257868.70 feet Y = -3385952.56 meter Z = -13679348.84 Z = -4149723.10 XDOT = 20192.029908 XDOT = 6105.506814 YDOT = 8974.685243 feet/sec YDOT = 2804.033420 meter/sec ZDOT = 12141.798759 ZDOT = 3730.599834 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -17142740.47 X = -5225107.29 Y = -3201932.10 feet Y = -975948.90 meter Z = -13600376.58 Z = -4145394.78 XDOT = -5998.832653 XDOT = -1828.444193 YDOT = -20013.019266 feet/sec YDOT = -6099.968272 meter/sec ZDOT = 12260.841561 ZDOT = 3737.104508 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10213.50914917 .00016717 00000-0 10270-3 0 9022 2 25544 51.6442 358.6609 0007609 174.0799 186.0454 15.71370390 30603 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10213.50914917 = yrday.fracday Element set: 902 Inclination: 51.6442 deg RA of node: 358.6609 deg Eccentricity: .0007609 Arg of perigee: 174.0799 deg Mean anomaly: 186.0454 deg </pre> <p> Mean motion: 15.71370390 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3060 Checksum: 309 </pre> <p> Coasting Arc #4 (Orbit 3075) </p><hr/> <p> Vector Time (GMT): 2010/214/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -6097573.56 A = 6736715.92 meter Y = -1291998.91 meter E = .0011505 Z = -2543244.12 I = 51.61493 XDOT = 3174.176473 Wp = 157.68464 YDOT = -4604.441598 meter/sec RA = 353.10498 deg ZDOT = -5289.396247 TA = 51.12935 MA = 51.02676 Ha = 195.573 n.mi Hp = 187.096 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -20005162.59 X = -6070318.44 Y = -4238841.58 feet Y = -1360033.08 meter Z = -8343976.77 Z = -2572799.88 XDOT = 10413.964808 XDOT = 3251.123090 YDOT = -15106.435690 feet/sec YDOT = -4568.515509 meter/sec ZDOT = -17353.662229 ZDOT = -5273.789536 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 9641619.94 X = 2938765.76 Y = 17978534.22 feet Y = 5479857.23 meter Z = -8462135.01 Z = -2579258.75 XDOT = -17015.707449 XDOT = -5186.387631 YDOT = 1014.413853 feet/sec YDOT = 309.193342 meter/sec ZDOT = -17291.214696 ZDOT = -5270.362239 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10214.52667404 .00016717 00000-0 10270-3 0 9032 2 25544 51.6440 353.4557 0007532 178.1212 181.9980 15.71393501 30760 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10214.52667404 = yrday.fracday Element set: 903 Inclination: 51.6440 deg RA of node: 353.4557 deg Eccentricity: .0007532 Arg of perigee: 178.1212 deg Mean anomaly: 181.9980 deg </pre> <p> Mean motion: 15.71393501 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3076 Checksum: 296 </pre> <p> Coasting Arc #5 (Orbit 3091) </p><hr/> <p> Vector Time (GMT): 2010/215/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1371872.07 A = 6729001.25 meter Y = 4322991.60 meter E = .0006436 Z = 4965333.78 I = 51.55905 XDOT = -7432.911066 Wp = 129.85057 YDOT = -47.895012 meter/sec RA = 347.94790 deg ZDOT = -2014.273460 TA = 339.64444 MA = 339.67008 Ha = 195.625 n.mi Hp = 187.310 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4500892.63 X = -1444231.20 Y = 14183043.29 feet Y = 4307245.54 meter Z = 16290465.16 Z = 4958493.82 XDOT = -24386.191162 XDOT = -7422.038122 YDOT = -157.135866 feet/sec YDOT = -130.953320 meter/sec ZDOT = -6608.508727 ZDOT = -2050.356009 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13701883.08 X = 4176333.96 Y = -5879363.79 feet Y = -1792030.08 meter Z = 16263071.30 Z = 4956984.13 XDOT = 15484.161929 XDOT = 4719.572556 YDOT = 17428.087009 feet/sec YDOT = 5312.080920 meter/sec ZDOT = -6752.773111 ZDOT = -2058.245244 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10215.54419145 .00016717 00000-0 10270-3 0 9043 2 25544 51.6444 348.2512 0007526 181.0944 179.0203 15.71367854 30921 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10215.54419145 = yrday.fracday Element set: 904 Inclination: 51.6444 deg RA of node: 348.2512 deg Eccentricity: .0007526 Arg of perigee: 181.0944 deg Mean anomaly: 179.0203 deg </pre> <p> Mean motion: 15.71367854 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3092 Checksum: 298 </pre> <p> Coasting Arc #6 (Orbit 3107) </p><hr/> <p> Vector Time (GMT): 2010/216/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6555126.59 A = 6739080.95 meter Y = -1237044.90 meter E = .0010593 Z = 945855.02 I = 51.56530 XDOT = 61.906571 Wp = 88.01616 YDOT = 4903.216536 meter/sec RA = 342.85250 deg ZDOT = 5926.981240 TA = 282.30813 MA = 282.42671 Ha = 195.373 n.mi Hp = 187.380 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 21506320.83 X = 6563877.49 Y = -4058546.25 feet Y = -1163692.71 meter Z = 3103198.89 Z = 977720.82 XDOT = 203.105548 XDOT = -21.718756 YDOT = 16086.668426 feet/sec YDOT = 4903.440688 meter/sec ZDOT = 19445.476510 ZDOT = 5927.079311 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -17432840.66 X = -5313529.83 Y = -13201615.44 feet Y = -4023852.39 meter Z = 3230618.03 Z = 984692.37 XDOT = 10901.806470 XDOT = 3322.870612 YDOT = -9593.538187 feet/sec YDOT = -2924.110439 meter/sec ZDOT = 19445.814717 ZDOT = 5927.084326 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10216.56169618 .00016717 00000-0 10270-3 0 9054 2 25544 51.6454 343.0463 0007480 185.6533 174.4545 15.71429694 31080 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10216.56169618 = yrday.fracday Element set: 905 Inclination: 51.6454 deg RA of node: 343.0463 deg Eccentricity: .0007480 Arg of perigee: 185.6533 deg Mean anomaly: 174.4545 deg </pre> <p> Mean motion: 15.71429694 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3108 Checksum: 318 </pre> <p> Coasting Arc #7 (Orbit 3122) </p><hr/> <p> Vector Time (GMT): 2010/217/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1430093.20 A = 6727390.25 meter Y = -3944958.80 meter E = .0015772 Z = -5270397.92 I = 51.49756 XDOT = 7155.643262 Wp = 118.52036 YDOT = -2803.326845 meter/sec RA = 337.71910 deg ZDOT = 149.623062 TA = 152.94608 MA = 152.86379 Ha = 195.163 n.mi Hp = 187.519 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4691906.82 X = -1360271.22 Y = -12942778.21 feet Y = -3960560.00 meter Z = -17291331.76 Z = -5277176.08 XDOT = 23476.519890 XDOT = 7185.731915 YDOT = -9197.266551 feet/sec YDOT = -2723.139946 meter/sec ZDOT = 490.889312 ZDOT = 184.457695 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -6303435.90 X = -1921287.26 Y = 12200808.82 feet Y = 3718806.53 meter Z = -17318389.39 Z = -5278645.09 XDOT = -21874.601567 XDOT = -6667.378558 YDOT = -10373.961954 feet/sec YDOT = -3161.983604 meter/sec ZDOT = 630.198039 ZDOT = 192.084362 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10217.51560057 .00016717 00000-0 10270-3 0 9063 2 25544 51.6455 338.1675 0007331 189.5309 170.5715 15.71451001 31230 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10217.51560057 = yrday.fracday Element set: 906 Inclination: 51.6455 deg RA of node: 338.1675 deg Eccentricity: .0007331 Arg of perigee: 189.5309 deg Mean anomaly: 170.5715 deg </pre> <p> Mean motion: 15.71451001 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3123 Checksum: 287 </pre> <p> Coasting Arc #8 (Orbit 3138) </p><hr/> <p> Vector Time (GMT): 2010/218/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5668315.21 A = 6739293.94 meter Y = 3558442.54 meter E = .0017708 Z = 690817.10 I = 51.51017 XDOT = -3089.554469 Wp = 149.97622 YDOT = -3751.257183 meter/sec RA = 332.58813 deg ZDOT = -5976.821625 TA = 22.48622 MA = 22.40871 Ha = 195.060 n.mi Hp = 187.805 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -18596834.68 X = -5711040.91 Y = 11674680.26 feet Y = 3494817.08 meter Z = 2266460.30 Z = 663177.38 XDOT = -10136.333561 XDOT = -3018.343645 YDOT = -12307.274222 feet/sec YDOT = -3785.407593 meter/sec ZDOT = -19608.994833 ZDOT = -5991.657951 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 21338438.78 X = 6503956.14 Y = 5224973.79 feet Y = 1592572.01 meter Z = 2155908.42 Z = 657120.89 XDOT = -1473.701921 XDOT = -449.184346 YDOT = 14206.142288 feet/sec YDOT = 4330.032169 meter/sec ZDOT = -19668.276580 ZDOT = -5994.890702 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10218.53308976 .00016717 00000-0 10270-3 0 9077 2 25544 51.6457 332.9620 0007380 193.6676 166.4287 15.71439190 31391 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10218.53308976 = yrday.fracday Element set: 907 Inclination: 51.6457 deg RA of node: 332.9620 deg Eccentricity: .0007380 Arg of perigee: 193.6676 deg Mean anomaly: 166.4287 deg </pre> <p> Mean motion: 15.71439190 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3139 Checksum: 332 </pre> <p> Coasting Arc #9 (Orbit 3154) </p><hr/> <p> Vector Time (GMT): 2010/219/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3785930.69 A = 6728196.49 meter Y = 2351004.55 meter E = .0010105 Z = 5041444.49 I = 51.44802 XDOT = -5482.734137 Wp = 168.43646 YDOT = 5120.218712 meter/sec RA = 327.48149 deg ZDOT = 1719.241985 TA = 264.90851 MA = 265.02386 Ha = 194.735 n.mi Hp = 187.911 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12421032.46 X = 3734869.96 Y = 7713269.53 feet Y = 2393055.06 meter Z = 16540172.23 Z = 5059712.45 XDOT = -17987.972890 XDOT = -5547.933489 YDOT = 16798.617821 feet/sec YDOT = 5058.542769 meter/sec ZDOT = 5640.557693 ZDOT = 1692.449509 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -3290009.02 X = -1002794.75 Y = -14160913.50 feet Y = -4316246.43 meter Z = 16613194.79 Z = 5063701.77 XDOT = 23590.558399 XDOT = 7190.402200 YDOT = 1050.430793 feet/sec YDOT = 320.171306 meter/sec ZDOT = 5533.377431 ZDOT = 1686.573441 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10219.55056819 .00016717 00000-0 10270-3 0 9087 2 25544 51.6466 327.7571 0007280 198.1513 161.9390 15.71494074 31552 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10219.55056819 = yrday.fracday Element set: 908 Inclination: 51.6466 deg RA of node: 327.7571 deg Eccentricity: .0007280 Arg of perigee: 198.1513 deg Mean anomaly: 161.9390 deg </pre> <p> Mean motion: 15.71494074 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3155 Checksum: 323 </pre> <p> Coasting Arc #10 (Orbit 3169) </p><hr/> <p> Vector Time (GMT): 2010/220/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3711722.68 A = 6737266.64 meter Y = -5148078.37 meter E = .0002595 Z = -2265936.53 I = 51.45323 XDOT = 5260.943075 Wp = 146.10152 YDOT = 1403.406083 meter/sec RA = 322.31852 deg ZDOT = 5430.112501 TA = 188.43582 MA = 188.44018 Ha = 194.686 n.mi Hp = 188.243 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12177567.86 X = 3780020.84 Y = -16890020.90 feet Y = -5106189.59 meter Z = -7434174.98 Z = -2247739.94 XDOT = 17260.311926 XDOT = 5218.481016 YDOT = 4604.350667 feet/sec YDOT = 1461.999206 meter/sec ZDOT = 17815.329729 ZDOT = 5455.566575 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -20517180.26 X = -6253636.54 Y = 3699792.73 feet Y = 1127696.83 meter Z = -7361370.16 Z = -2243745.62 XDOT = -8900.665088 XDOT = -2712.922719 YDOT = -13715.194095 feet/sec YDOT = -4180.391160 meter/sec ZDOT = 17917.100945 ZDOT = 5461.132368 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10220.50444842 .00016717 00000-0 10270-3 0 9092 2 25544 51.6467 322.8780 0007067 202.3646 157.7209 15.71446669 31705 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10220.50444842 = yrday.fracday Element set: 909 Inclination: 51.6467 deg RA of node: 322.8780 deg Eccentricity: .0007067 Arg of perigee: 202.3646 deg Mean anomaly: 157.7209 deg </pre> <p> Mean motion: 15.71446669 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3170 Checksum: 311 </pre> <p> Coasting Arc #11 (Orbit 3185) </p><hr/> <p> Vector Time (GMT): 2010/221/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5136470.09 A = 6731045.96 meter Y = 19200.35 meter E = .0006339 Z = -4352924.83 I = 51.40944 XDOT = 2836.922562 Wp = 120.34210 YDOT = -6300.690623 meter/sec RA = 317.23213 deg ZDOT = -3382.184244 TA = 115.46472 MA = 115.39913 Ha = 194.460 n.mi Hp = 188.229 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -16851935.99 X = -5115157.85 Y = 62993.27 feet Y = -38119.32 meter Z = -14281249.43 Z = -4377825.41 XDOT = 9307.488719 XDOT = 2923.596817 YDOT = -20671.557161 feet/sec YDOT = -6268.481645 meter/sec ZDOT = -11096.405000 ZDOT = -3368.192649 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 12324415.10 X = 3756481.72 Y = 11368666.12 feet Y = 3465169.43 meter Z = -14380821.37 Z = -4383274.35 XDOT = -20109.514053 XDOT = -6129.379883 YDOT = 7862.568548 feet/sec YDOT = 2396.510893 meter/sec ZDOT = -11040.415039 ZDOT = -3365.118504 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10221.52191099 .00016717 00000-0 10270-3 0 9100 2 25544 51.6466 317.6735 0007190 205.8403 154.2401 15.71473815 31868 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10221.52191099 = yrday.fracday Element set: 910 Inclination: 51.6466 deg RA of node: 317.6735 deg Eccentricity: .0007190 Arg of perigee: 205.8403 deg Mean anomaly: 154.2401 deg </pre> <p> Mean motion: 15.71473815 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3186 Checksum: 292 </pre> <p> Coasting Arc #12 (Orbit 3201) </p><hr/> <p> Vector Time (GMT): 2010/222/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1164305.44 A = 6733743.18 meter Y = 5569201.58 meter E = .0010216 Z = 3589218.91 I = 51.39680 XDOT = -6129.108029 Wp = 121.32462 YDOT = 1554.579537 meter/sec RA = 312.04998 deg ZDOT = -4396.411965 TA = 15.61791 MA = 15.58642 Ha = 194.351 n.mi Hp = 188.451 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -3819899.73 X = -1243930.08 Y = 18271658.73 feet Y = 5555736.33 meter Z = 11775652.59 Z = 3583369.59 XDOT = -20108.622144 XDOT = -6124.679645 YDOT = 5100.326564 feet/sec YDOT = 1486.065050 meter/sec ZDOT = -14423.923771 ZDOT = -4426.175647 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15101194.47 X = 4602844.08 Y = -10997726.66 feet Y = -3352107.09 meter Z = 11752237.00 Z = 3582081.84 XDOT = 17504.086811 XDOT = 5335.245660 YDOT = 8480.588989 feet/sec YDOT = 2584.883524 meter/sec ZDOT = -14542.949406 ZDOT = -4432.690979 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10222.53936499 .00016717 00000-0 10270-3 0 9114 2 25544 51.6463 312.4690 0006979 208.8906 151.1870 15.71495421 32025 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10222.53936499 = yrday.fracday Element set: 911 Inclination: 51.6463 deg RA of node: 312.4690 deg Eccentricity: .0006979 Arg of perigee: 208.8906 deg Mean anomaly: 151.1870 deg </pre> <p> Mean motion: 15.71495421 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3202 Checksum: 313 </pre> <p> Coasting Arc #13 (Orbit 3217) </p><hr/> <p> Vector Time (GMT): 2010/223/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 5258542.94 A = 6734559.54 meter Y = -2674023.07 meter E = .0010418 Z = 3246535.46 I = 51.38045 XDOT = 157.914461 Wp = 121.09529 YDOT = 6069.261879 meter/sec RA = 306.96651 deg ZDOT = 4726.693877 TA = 277.00825 MA = 277.12673 Ha = 194.122 n.mi Hp = 188.556 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 17252437.46 X = 5272282.77 Y = -8773041.57 feet Y = -2615142.07 meter Z = 10651363.05 Z = 3272114.30 XDOT = 518.092064 XDOT = 67.074181 YDOT = 19912.276505 feet/sec YDOT = 6070.519859 meter/sec ZDOT = 15507.525842 ZDOT = 4727.240360 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -18733617.04 X = -5710006.47 Y = -4634104.42 feet Y = -1412475.03 meter Z = 10753653.35 Z = 3277713.54 XDOT = 12386.302565 XDOT = 3775.345022 YDOT = -13956.911682 feet/sec YDOT = -4254.066681 meter/sec ZDOT = 15509.693915 ZDOT = 4727.354705 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10223.55680824 .00016717 00000-0 10270-3 0 9126 2 25544 51.6461 307.2636 0007007 213.6571 146.4147 15.71531311 32180 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10223.55680824 = yrday.fracday Element set: 912 Inclination: 51.6461 deg RA of node: 307.2636 deg Eccentricity: .0007007 Arg of perigee: 213.6571 deg Mean anomaly: 146.4147 deg </pre> <p> Mean motion: 15.71531311 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3218 Checksum: 280 </pre> <p> Coasting Arc #14 (Orbit 3232) </p><hr/> <p> Vector Time (GMT): 2010/224/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1361085.73 A = 6730051.23 meter Y = -4752248.11 meter E = .0010606 Z = -4576215.72 I = 51.34718 XDOT = 5535.616561 Wp = 147.89623 YDOT = -4440.417348 meter/sec RA = 301.78372 deg ZDOT = 2959.085518 TA = 151.65831 MA = 151.60058 Ha = 193.927 n.mi Hp = 188.677 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4465504.37 X = -1285613.98 Y = -15591365.17 feet Y = -4767046.65 meter Z = -15013831.09 Z = -4582644.40 XDOT = 18161.471658 XDOT = 5570.484220 YDOT = -14568.298385 feet/sec YDOT = -4378.319781 meter/sec ZDOT = 9708.285819 ZDOT = 2986.061870 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -6655967.34 X = -2028738.84 Y = 14763372.02 feet Y = 4499875.79 meter Z = -15039530.14 Z = -4584048.79 XDOT = -22156.188064 XDOT = -6753.206122 YDOT = 29.840209 feet/sec YDOT = 9.095296 meter/sec ZDOT = 9816.160431 ZDOT = 2991.965699 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10224.51065509 .00016717 00000-0 10270-3 0 9131 2 25544 51.6452 302.3844 0006843 217.1411 142.9279 15.71554390 32332 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10224.51065509 = yrday.fracday Element set: 913 Inclination: 51.6452 deg RA of node: 302.3844 deg Eccentricity: .0006843 Arg of perigee: 217.1411 deg Mean anomaly: 142.9279 deg </pre> <p> Mean motion: 15.71554390 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3233 Checksum: 287 </pre> <p> Coasting Arc #15 (Orbit 3248) </p><hr/> <p> Vector Time (GMT): 2010/225/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4165371.74 A = 6737637.36 meter Y = 4942250.42 meter E = .0010604 Z = -1878727.23 I = 51.35679 XDOT = -2778.228543 Wp = 180.16326 YDOT = -4472.865737 meter/sec RA = 296.68621 deg ZDOT = -5617.175003 TA = 20.77501 MA = 20.73194 Ha = 193.709 n.mi Hp = 188.952 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -13665917.80 X = -4211200.89 Y = 16214732.35 feet Y = 4895414.48 meter Z = -6163803.25 Z = -1899073.76 XDOT = -9114.923042 XDOT = -2700.718710 YDOT = -14674.756356 feet/sec YDOT = -4503.500214 meter/sec ZDOT = -18429.051846 ZDOT = -5630.483197 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 20793261.04 X = 6337785.97 Y = -4038016.06 feet Y = -1230787.30 meter Z = -6245161.86 Z = -1903525.33 XDOT = -2519.739768 XDOT = -768.016681 YDOT = 15557.522047 feet/sec YDOT = 4741.932720 meter/sec ZDOT = -18482.262817 ZDOT = -5633.393706 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10225.52808320 .00016717 00000-0 10270-3 0 9140 2 25544 51.6443 297.1789 0006813 221.4446 138.6200 15.71532026 32499 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10225.52808320 = yrday.fracday Element set: 914 Inclination: 51.6443 deg RA of node: 297.1789 deg Eccentricity: .0006813 Arg of perigee: 221.4446 deg Mean anomaly: 138.6200 deg </pre> <p> Mean motion: 15.71532026 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3249 Checksum: 293</pre> <hr/> <p><strong>INTERNATIONAL SPACE STATION ORBITAL DATA:</strong> </p> <p>The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability. The data normally contains past, current and predicted orbital data. Careful attention to the orbit # / epoch times! These sources include: </p><p>NASA Orbital Flight Dynamics<br/> DOD C-Band Radar Network<br/> Goddard Space Flight Center (GSFC)<br/> NASA Johnson Space Center (JSC)<br/> DoD/ USSTRATCOM/ US Space Command with permission </p> <p>By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command. </p><pre> David Cottle Director Of Engineering IDB Communications</pre> <hr/> <p>The following information is a reminder of your current mailing list subscription: </p><p>You are subscribed to the following list: </p><p><strong>[ISSTLE LIST]</strong> </p><p>using the following email: </p><p> <a href="mailto:&#101;&#x78;&#x61;&#x6D;&#112;&#x6C;&#101;&#64;&#101;&#120;&#x61;&#109;&#112;&#x6C;&#x65;&#x2E;&#99;&#x6F;&#x6D;">&#101;&#x78;&#x61;&#x6D;&#112;&#x6C;&#101;&#64;&#101;&#120;&#x61;&#109;&#112;&#x6C;&#x65;&#x2E;&#99;&#x6F;&#x6D;</a> </p><p>You may automatically unsubscribe from this list at any time by visiting the following URL: </p><p>&#60;<a href="http://www.aus-city.com/cgi-bin/dada/mail.cgi/u/ISSTLE_LIST/example/example.com/">http://www.aus-city.com/cgi-bin/dada/mail.cgi/u/ISSTLE_LIST/example/example.com/</a>&#62; </p><p>If the above URL is inoperable, make sure that you have copied the entire address. 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subscription_form_widget.tmpl --> [ISSTLE LIST] Current ISS TLEs @ 18:30 UTC tag:www.aus-city.com,2010-07-31:%2Fcgi-bin%2Fdada%2Fmail.cgi%2Farchive%2FISSTLE_LIST%2F20100731044503%2F 2010-07-31T04:45:03Z 2010-07-31T04:45:03Z <p>&#60;B&#62; ISS TRAJECTORY DATA&#60;/B&#62; </p><p> Lift off time (UTC) : N/A<br/> Area (sq ft) : 9149.32<br/> Drag Coefficient (Cd) : 2.00<br/> Monthly MSFC 50% solar flux (F10.7-jansky) : 74.8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0.74 ET - UTC (sec) : 66.18<br/> UT1 - UTC (sec) : 0.00 </p><p> Maneuvers contained within the current ephemeris are as follows: </p><pre> IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP </pre> <hr/> There are no maneuvers. <p> Coasting Arc #1 (Orbit 3028) </p><hr/> <p> Vector Time (GMT): 2010/211/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5886772.53 A = 6736192.33 meter Y = 1453024.09 meter E = .0017697 Z = 2909467.41 I = 51.70110 XDOT = -3624.406982 Wp = 121.91121 YDOT = -4560.767225 meter/sec RA = 8.40280 deg ZDOT = -5042.500272 TA = 24.63621 MA = 24.55178 Ha = 196.145 n.mi Hp = 186.771 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -19313558.18 X = -5916716.47 Y = 4767139.42 feet Y = 1387027.14 meter Z = 9545496.75 Z = 2880797.19 XDOT = -11891.099021 XDOT = -3548.643054 YDOT = -14963.147063 feet/sec YDOT = -4600.873679 meter/sec ZDOT = -16543.636064 ZDOT = -5059.923567 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15517127.17 X = 4729620.36 Y = 12535298.83 feet Y = 3820759.08 meter Z = 9430837.90 Z = 2874519.39 XDOT = -3861.988708 XDOT = -1177.134158 YDOT = 17312.292654 feet/sec YDOT = 5276.786801 meter/sec ZDOT = -16613.263137 ZDOT = -5063.722604 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10211.53766810 .00016717 00000-0 10270-3 0 9008 2 25544 51.6422 8.7446 0007649 167.4000 192.7355 15.71333273 30296 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10211.53766810 = yrday.fracday Element set: 900 Inclination: 51.6422 deg RA of node: 8.7446 deg Eccentricity: .0007649 Arg of perigee: 167.4000 deg Mean anomaly: 192.7355 deg </pre> <p> Mean motion: 15.71333273 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3029 Checksum: 288 </pre> <p> Coasting Arc #2 (Orbit 3044) </p><hr/> <p> Vector Time (GMT): 2010/212/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4403939.30 A = 6733087.50 meter Y = 3316504.31 meter E = .0015483 Z = 3862163.07 I = 51.66218 XDOT = -5817.533868 Wp = 127.13796 YDOT = 2915.774610 meter/sec RA = 3.33999 deg ZDOT = 4109.325400 TA = 279.87419 MA = 280.04895 Ha = 195.851 n.mi Hp = 186.803 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 14448619.76 X = 4347764.73 Y = 10880919.65 feet Y = 3365437.54 meter Z = 12671138.68 Z = 3883420.89 XDOT = -19086.397205 XDOT = -5869.668385 YDOT = 9566.189665 feet/sec YDOT = 2850.427797 meter/sec ZDOT = 13482.038713 ZDOT = 4080.937582 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -345548.62 X = -105323.22 Y = -18024347.84 feet Y = -5493821.22 meter Z = 12756106.85 Z = 3888061.37 XDOT = 18060.093134 XDOT = 5504.716387 YDOT = 9162.037204 feet/sec YDOT = 2792.588940 meter/sec ZDOT = 13368.499903 ZDOT = 4074.718770 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10212.55521023 .00016717 00000-0 10270-3 0 9017 2 25544 51.6431 3.5398 0007677 171.3351 188.7945 15.71382511 30456 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10212.55521023 = yrday.fracday Element set: 901 Inclination: 51.6431 deg RA of node: 3.5398 deg Eccentricity: .0007677 Arg of perigee: 171.3351 deg Mean anomaly: 188.7945 deg </pre> <p> Mean motion: 15.71382511 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3045 Checksum: 287 </pre> <p> Coasting Arc #3 (Orbit 3059) </p><hr/> <p> Vector Time (GMT): 2010/213/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4034796.50 A = 6732241.50 meter Y = -3431398.38 meter E = .0013066 Z = -4169465.53 I = 51.62973 XDOT = 6154.530716 Wp = 140.96198 YDOT = 2735.484062 meter/sec RA = 358.17491 deg ZDOT = 3700.820262 TA = 166.95153 MA = 166.91770 Ha = 195.823 n.mi Hp = 187.068 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 13237521.32 X = 4093121.53 Y = -11257868.70 feet Y = -3385952.56 meter Z = -13679348.84 Z = -4149723.10 XDOT = 20192.029908 XDOT = 6105.506814 YDOT = 8974.685243 feet/sec YDOT = 2804.033420 meter/sec ZDOT = 12141.798759 ZDOT = 3730.599834 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -17142740.47 X = -5225107.29 Y = -3201932.10 feet Y = -975948.90 meter Z = -13600376.58 Z = -4145394.78 XDOT = -5998.832653 XDOT = -1828.444193 YDOT = -20013.019266 feet/sec YDOT = -6099.968272 meter/sec ZDOT = 12260.841561 ZDOT = 3737.104508 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10213.50914917 .00016717 00000-0 10270-3 0 9022 2 25544 51.6442 358.6609 0007609 174.0799 186.0454 15.71370390 30603 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10213.50914917 = yrday.fracday Element set: 902 Inclination: 51.6442 deg RA of node: 358.6609 deg Eccentricity: .0007609 Arg of perigee: 174.0799 deg Mean anomaly: 186.0454 deg </pre> <p> Mean motion: 15.71370390 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3060 Checksum: 309 </pre> <p> Coasting Arc #4 (Orbit 3075) </p><hr/> <p> Vector Time (GMT): 2010/214/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -6097573.56 A = 6736715.92 meter Y = -1291998.91 meter E = .0011505 Z = -2543244.12 I = 51.61493 XDOT = 3174.176473 Wp = 157.68464 YDOT = -4604.441598 meter/sec RA = 353.10498 deg ZDOT = -5289.396247 TA = 51.12935 MA = 51.02676 Ha = 195.573 n.mi Hp = 187.096 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -20005162.59 X = -6070318.44 Y = -4238841.58 feet Y = -1360033.08 meter Z = -8343976.77 Z = -2572799.88 XDOT = 10413.964808 XDOT = 3251.123090 YDOT = -15106.435690 feet/sec YDOT = -4568.515509 meter/sec ZDOT = -17353.662229 ZDOT = -5273.789536 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 9641619.94 X = 2938765.76 Y = 17978534.22 feet Y = 5479857.23 meter Z = -8462135.01 Z = -2579258.75 XDOT = -17015.707449 XDOT = -5186.387631 YDOT = 1014.413853 feet/sec YDOT = 309.193342 meter/sec ZDOT = -17291.214696 ZDOT = -5270.362239 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10214.52667404 .00016717 00000-0 10270-3 0 9032 2 25544 51.6440 353.4557 0007532 178.1212 181.9980 15.71393501 30760 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10214.52667404 = yrday.fracday Element set: 903 Inclination: 51.6440 deg RA of node: 353.4557 deg Eccentricity: .0007532 Arg of perigee: 178.1212 deg Mean anomaly: 181.9980 deg </pre> <p> Mean motion: 15.71393501 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3076 Checksum: 296 </pre> <p> Coasting Arc #5 (Orbit 3091) </p><hr/> <p> Vector Time (GMT): 2010/215/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1371872.07 A = 6729001.25 meter Y = 4322991.60 meter E = .0006436 Z = 4965333.78 I = 51.55905 XDOT = -7432.911066 Wp = 129.85057 YDOT = -47.895012 meter/sec RA = 347.94790 deg ZDOT = -2014.273460 TA = 339.64444 MA = 339.67008 Ha = 195.625 n.mi Hp = 187.310 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4500892.63 X = -1444231.20 Y = 14183043.29 feet Y = 4307245.54 meter Z = 16290465.16 Z = 4958493.82 XDOT = -24386.191162 XDOT = -7422.038122 YDOT = -157.135866 feet/sec YDOT = -130.953320 meter/sec ZDOT = -6608.508727 ZDOT = -2050.356009 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13701883.08 X = 4176333.96 Y = -5879363.79 feet Y = -1792030.08 meter Z = 16263071.30 Z = 4956984.13 XDOT = 15484.161929 XDOT = 4719.572556 YDOT = 17428.087009 feet/sec YDOT = 5312.080920 meter/sec ZDOT = -6752.773111 ZDOT = -2058.245244 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10215.54419145 .00016717 00000-0 10270-3 0 9043 2 25544 51.6444 348.2512 0007526 181.0944 179.0203 15.71367854 30921 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10215.54419145 = yrday.fracday Element set: 904 Inclination: 51.6444 deg RA of node: 348.2512 deg Eccentricity: .0007526 Arg of perigee: 181.0944 deg Mean anomaly: 179.0203 deg </pre> <p> Mean motion: 15.71367854 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3092 Checksum: 298 </pre> <p> Coasting Arc #6 (Orbit 3107) </p><hr/> <p> Vector Time (GMT): 2010/216/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6555126.59 A = 6739080.95 meter Y = -1237044.90 meter E = .0010593 Z = 945855.02 I = 51.56530 XDOT = 61.906571 Wp = 88.01616 YDOT = 4903.216536 meter/sec RA = 342.85250 deg ZDOT = 5926.981240 TA = 282.30813 MA = 282.42671 Ha = 195.373 n.mi Hp = 187.380 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 21506320.83 X = 6563877.49 Y = -4058546.25 feet Y = -1163692.71 meter Z = 3103198.89 Z = 977720.82 XDOT = 203.105548 XDOT = -21.718756 YDOT = 16086.668426 feet/sec YDOT = 4903.440688 meter/sec ZDOT = 19445.476510 ZDOT = 5927.079311 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -17432840.66 X = -5313529.83 Y = -13201615.44 feet Y = -4023852.39 meter Z = 3230618.03 Z = 984692.37 XDOT = 10901.806470 XDOT = 3322.870612 YDOT = -9593.538187 feet/sec YDOT = -2924.110439 meter/sec ZDOT = 19445.814717 ZDOT = 5927.084326 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10216.56169618 .00016717 00000-0 10270-3 0 9054 2 25544 51.6454 343.0463 0007480 185.6533 174.4545 15.71429694 31080 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10216.56169618 = yrday.fracday Element set: 905 Inclination: 51.6454 deg RA of node: 343.0463 deg Eccentricity: .0007480 Arg of perigee: 185.6533 deg Mean anomaly: 174.4545 deg </pre> <p> Mean motion: 15.71429694 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3108 Checksum: 318 </pre> <p> Coasting Arc #7 (Orbit 3122) </p><hr/> <p> Vector Time (GMT): 2010/217/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1430093.20 A = 6727390.25 meter Y = -3944958.80 meter E = .0015772 Z = -5270397.92 I = 51.49756 XDOT = 7155.643262 Wp = 118.52036 YDOT = -2803.326845 meter/sec RA = 337.71910 deg ZDOT = 149.623062 TA = 152.94608 MA = 152.86379 Ha = 195.163 n.mi Hp = 187.519 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4691906.82 X = -1360271.22 Y = -12942778.21 feet Y = -3960560.00 meter Z = -17291331.76 Z = -5277176.08 XDOT = 23476.519890 XDOT = 7185.731915 YDOT = -9197.266551 feet/sec YDOT = -2723.139946 meter/sec ZDOT = 490.889312 ZDOT = 184.457695 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -6303435.90 X = -1921287.26 Y = 12200808.82 feet Y = 3718806.53 meter Z = -17318389.39 Z = -5278645.09 XDOT = -21874.601567 XDOT = -6667.378558 YDOT = -10373.961954 feet/sec YDOT = -3161.983604 meter/sec ZDOT = 630.198039 ZDOT = 192.084362 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10217.51560057 .00016717 00000-0 10270-3 0 9063 2 25544 51.6455 338.1675 0007331 189.5309 170.5715 15.71451001 31230 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10217.51560057 = yrday.fracday Element set: 906 Inclination: 51.6455 deg RA of node: 338.1675 deg Eccentricity: .0007331 Arg of perigee: 189.5309 deg Mean anomaly: 170.5715 deg </pre> <p> Mean motion: 15.71451001 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3123 Checksum: 287 </pre> <p> Coasting Arc #8 (Orbit 3138) </p><hr/> <p> Vector Time (GMT): 2010/218/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5668315.21 A = 6739293.94 meter Y = 3558442.54 meter E = .0017708 Z = 690817.10 I = 51.51017 XDOT = -3089.554469 Wp = 149.97622 YDOT = -3751.257183 meter/sec RA = 332.58813 deg ZDOT = -5976.821625 TA = 22.48622 MA = 22.40871 Ha = 195.060 n.mi Hp = 187.805 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -18596834.68 X = -5711040.91 Y = 11674680.26 feet Y = 3494817.08 meter Z = 2266460.30 Z = 663177.38 XDOT = -10136.333561 XDOT = -3018.343645 YDOT = -12307.274222 feet/sec YDOT = -3785.407593 meter/sec ZDOT = -19608.994833 ZDOT = -5991.657951 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 21338438.78 X = 6503956.14 Y = 5224973.79 feet Y = 1592572.01 meter Z = 2155908.42 Z = 657120.89 XDOT = -1473.701921 XDOT = -449.184346 YDOT = 14206.142288 feet/sec YDOT = 4330.032169 meter/sec ZDOT = -19668.276580 ZDOT = -5994.890702 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10218.53308976 .00016717 00000-0 10270-3 0 9077 2 25544 51.6457 332.9620 0007380 193.6676 166.4287 15.71439190 31391 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10218.53308976 = yrday.fracday Element set: 907 Inclination: 51.6457 deg RA of node: 332.9620 deg Eccentricity: .0007380 Arg of perigee: 193.6676 deg Mean anomaly: 166.4287 deg </pre> <p> Mean motion: 15.71439190 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3139 Checksum: 332 </pre> <p> Coasting Arc #9 (Orbit 3154) </p><hr/> <p> Vector Time (GMT): 2010/219/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3785930.69 A = 6728196.49 meter Y = 2351004.55 meter E = .0010105 Z = 5041444.49 I = 51.44802 XDOT = -5482.734137 Wp = 168.43646 YDOT = 5120.218712 meter/sec RA = 327.48149 deg ZDOT = 1719.241985 TA = 264.90851 MA = 265.02386 Ha = 194.735 n.mi Hp = 187.911 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12421032.46 X = 3734869.96 Y = 7713269.53 feet Y = 2393055.06 meter Z = 16540172.23 Z = 5059712.45 XDOT = -17987.972890 XDOT = -5547.933489 YDOT = 16798.617821 feet/sec YDOT = 5058.542769 meter/sec ZDOT = 5640.557693 ZDOT = 1692.449509 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -3290009.02 X = -1002794.75 Y = -14160913.50 feet Y = -4316246.43 meter Z = 16613194.79 Z = 5063701.77 XDOT = 23590.558399 XDOT = 7190.402200 YDOT = 1050.430793 feet/sec YDOT = 320.171306 meter/sec ZDOT = 5533.377431 ZDOT = 1686.573441 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10219.55056819 .00016717 00000-0 10270-3 0 9087 2 25544 51.6466 327.7571 0007280 198.1513 161.9390 15.71494074 31552 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10219.55056819 = yrday.fracday Element set: 908 Inclination: 51.6466 deg RA of node: 327.7571 deg Eccentricity: .0007280 Arg of perigee: 198.1513 deg Mean anomaly: 161.9390 deg </pre> <p> Mean motion: 15.71494074 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3155 Checksum: 323 </pre> <p> Coasting Arc #10 (Orbit 3169) </p><hr/> <p> Vector Time (GMT): 2010/220/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3711722.68 A = 6737266.64 meter Y = -5148078.37 meter E = .0002595 Z = -2265936.53 I = 51.45323 XDOT = 5260.943075 Wp = 146.10152 YDOT = 1403.406083 meter/sec RA = 322.31852 deg ZDOT = 5430.112501 TA = 188.43582 MA = 188.44018 Ha = 194.686 n.mi Hp = 188.243 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12177567.86 X = 3780020.84 Y = -16890020.90 feet Y = -5106189.59 meter Z = -7434174.98 Z = -2247739.94 XDOT = 17260.311926 XDOT = 5218.481016 YDOT = 4604.350667 feet/sec YDOT = 1461.999206 meter/sec ZDOT = 17815.329729 ZDOT = 5455.566575 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -20517180.26 X = -6253636.54 Y = 3699792.73 feet Y = 1127696.83 meter Z = -7361370.16 Z = -2243745.62 XDOT = -8900.665088 XDOT = -2712.922719 YDOT = -13715.194095 feet/sec YDOT = -4180.391160 meter/sec ZDOT = 17917.100945 ZDOT = 5461.132368 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10220.50444842 .00016717 00000-0 10270-3 0 9092 2 25544 51.6467 322.8780 0007067 202.3646 157.7209 15.71446669 31705 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10220.50444842 = yrday.fracday Element set: 909 Inclination: 51.6467 deg RA of node: 322.8780 deg Eccentricity: .0007067 Arg of perigee: 202.3646 deg Mean anomaly: 157.7209 deg </pre> <p> Mean motion: 15.71446669 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3170 Checksum: 311 </pre> <p> Coasting Arc #11 (Orbit 3185) </p><hr/> <p> Vector Time (GMT): 2010/221/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5136470.09 A = 6731045.96 meter Y = 19200.35 meter E = .0006339 Z = -4352924.83 I = 51.40944 XDOT = 2836.922562 Wp = 120.34210 YDOT = -6300.690623 meter/sec RA = 317.23213 deg ZDOT = -3382.184244 TA = 115.46472 MA = 115.39913 Ha = 194.460 n.mi Hp = 188.229 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -16851935.99 X = -5115157.85 Y = 62993.27 feet Y = -38119.32 meter Z = -14281249.43 Z = -4377825.41 XDOT = 9307.488719 XDOT = 2923.596817 YDOT = -20671.557161 feet/sec YDOT = -6268.481645 meter/sec ZDOT = -11096.405000 ZDOT = -3368.192649 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 12324415.10 X = 3756481.72 Y = 11368666.12 feet Y = 3465169.43 meter Z = -14380821.37 Z = -4383274.35 XDOT = -20109.514053 XDOT = -6129.379883 YDOT = 7862.568548 feet/sec YDOT = 2396.510893 meter/sec ZDOT = -11040.415039 ZDOT = -3365.118504 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10221.52191099 .00016717 00000-0 10270-3 0 9100 2 25544 51.6466 317.6735 0007190 205.8403 154.2401 15.71473815 31868 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10221.52191099 = yrday.fracday Element set: 910 Inclination: 51.6466 deg RA of node: 317.6735 deg Eccentricity: .0007190 Arg of perigee: 205.8403 deg Mean anomaly: 154.2401 deg </pre> <p> Mean motion: 15.71473815 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3186 Checksum: 292 </pre> <p> Coasting Arc #12 (Orbit 3201) </p><hr/> <p> Vector Time (GMT): 2010/222/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1164305.44 A = 6733743.18 meter Y = 5569201.58 meter E = .0010216 Z = 3589218.91 I = 51.39680 XDOT = -6129.108029 Wp = 121.32462 YDOT = 1554.579537 meter/sec RA = 312.04998 deg ZDOT = -4396.411965 TA = 15.61791 MA = 15.58642 Ha = 194.351 n.mi Hp = 188.451 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -3819899.73 X = -1243930.08 Y = 18271658.73 feet Y = 5555736.33 meter Z = 11775652.59 Z = 3583369.59 XDOT = -20108.622144 XDOT = -6124.679645 YDOT = 5100.326564 feet/sec YDOT = 1486.065050 meter/sec ZDOT = -14423.923771 ZDOT = -4426.175647 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15101194.47 X = 4602844.08 Y = -10997726.66 feet Y = -3352107.09 meter Z = 11752237.00 Z = 3582081.84 XDOT = 17504.086811 XDOT = 5335.245660 YDOT = 8480.588989 feet/sec YDOT = 2584.883524 meter/sec ZDOT = -14542.949406 ZDOT = -4432.690979 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10222.53936499 .00016717 00000-0 10270-3 0 9114 2 25544 51.6463 312.4690 0006979 208.8906 151.1870 15.71495421 32025 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10222.53936499 = yrday.fracday Element set: 911 Inclination: 51.6463 deg RA of node: 312.4690 deg Eccentricity: .0006979 Arg of perigee: 208.8906 deg Mean anomaly: 151.1870 deg </pre> <p> Mean motion: 15.71495421 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3202 Checksum: 313 </pre> <p> Coasting Arc #13 (Orbit 3217) </p><hr/> <p> Vector Time (GMT): 2010/223/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 5258542.94 A = 6734559.54 meter Y = -2674023.07 meter E = .0010418 Z = 3246535.46 I = 51.38045 XDOT = 157.914461 Wp = 121.09529 YDOT = 6069.261879 meter/sec RA = 306.96651 deg ZDOT = 4726.693877 TA = 277.00825 MA = 277.12673 Ha = 194.122 n.mi Hp = 188.556 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 17252437.46 X = 5272282.77 Y = -8773041.57 feet Y = -2615142.07 meter Z = 10651363.05 Z = 3272114.30 XDOT = 518.092064 XDOT = 67.074181 YDOT = 19912.276505 feet/sec YDOT = 6070.519859 meter/sec ZDOT = 15507.525842 ZDOT = 4727.240360 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -18733617.04 X = -5710006.47 Y = -4634104.42 feet Y = -1412475.03 meter Z = 10753653.35 Z = 3277713.54 XDOT = 12386.302565 XDOT = 3775.345022 YDOT = -13956.911682 feet/sec YDOT = -4254.066681 meter/sec ZDOT = 15509.693915 ZDOT = 4727.354705 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10223.55680824 .00016717 00000-0 10270-3 0 9126 2 25544 51.6461 307.2636 0007007 213.6571 146.4147 15.71531311 32180 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10223.55680824 = yrday.fracday Element set: 912 Inclination: 51.6461 deg RA of node: 307.2636 deg Eccentricity: .0007007 Arg of perigee: 213.6571 deg Mean anomaly: 146.4147 deg </pre> <p> Mean motion: 15.71531311 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3218 Checksum: 280 </pre> <p> Coasting Arc #14 (Orbit 3232) </p><hr/> <p> Vector Time (GMT): 2010/224/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1361085.73 A = 6730051.23 meter Y = -4752248.11 meter E = .0010606 Z = -4576215.72 I = 51.34718 XDOT = 5535.616561 Wp = 147.89623 YDOT = -4440.417348 meter/sec RA = 301.78372 deg ZDOT = 2959.085518 TA = 151.65831 MA = 151.60058 Ha = 193.927 n.mi Hp = 188.677 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4465504.37 X = -1285613.98 Y = -15591365.17 feet Y = -4767046.65 meter Z = -15013831.09 Z = -4582644.40 XDOT = 18161.471658 XDOT = 5570.484220 YDOT = -14568.298385 feet/sec YDOT = -4378.319781 meter/sec ZDOT = 9708.285819 ZDOT = 2986.061870 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -6655967.34 X = -2028738.84 Y = 14763372.02 feet Y = 4499875.79 meter Z = -15039530.14 Z = -4584048.79 XDOT = -22156.188064 XDOT = -6753.206122 YDOT = 29.840209 feet/sec YDOT = 9.095296 meter/sec ZDOT = 9816.160431 ZDOT = 2991.965699 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10224.51065509 .00016717 00000-0 10270-3 0 9131 2 25544 51.6452 302.3844 0006843 217.1411 142.9279 15.71554390 32332 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10224.51065509 = yrday.fracday Element set: 913 Inclination: 51.6452 deg RA of node: 302.3844 deg Eccentricity: .0006843 Arg of perigee: 217.1411 deg Mean anomaly: 142.9279 deg </pre> <p> Mean motion: 15.71554390 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3233 Checksum: 287 </pre> <p> Coasting Arc #15 (Orbit 3248) </p><hr/> <p> Vector Time (GMT): 2010/225/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4165371.74 A = 6737637.36 meter Y = 4942250.42 meter E = .0010604 Z = -1878727.23 I = 51.35679 XDOT = -2778.228543 Wp = 180.16326 YDOT = -4472.865737 meter/sec RA = 296.68621 deg ZDOT = -5617.175003 TA = 20.77501 MA = 20.73194 Ha = 193.709 n.mi Hp = 188.952 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -13665917.80 X = -4211200.89 Y = 16214732.35 feet Y = 4895414.48 meter Z = -6163803.25 Z = -1899073.76 XDOT = -9114.923042 XDOT = -2700.718710 YDOT = -14674.756356 feet/sec YDOT = -4503.500214 meter/sec ZDOT = -18429.051846 ZDOT = -5630.483197 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 20793261.04 X = 6337785.97 Y = -4038016.06 feet Y = -1230787.30 meter Z = -6245161.86 Z = -1903525.33 XDOT = -2519.739768 XDOT = -768.016681 YDOT = 15557.522047 feet/sec YDOT = 4741.932720 meter/sec ZDOT = -18482.262817 ZDOT = -5633.393706 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10225.52808320 .00016717 00000-0 10270-3 0 9140 2 25544 51.6443 297.1789 0006813 221.4446 138.6200 15.71532026 32499 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10225.52808320 = yrday.fracday Element set: 914 Inclination: 51.6443 deg RA of node: 297.1789 deg Eccentricity: .0006813 Arg of perigee: 221.4446 deg Mean anomaly: 138.6200 deg </pre> <p> Mean motion: 15.71532026 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3249 Checksum: 293</pre> <hr/> <p><strong>INTERNATIONAL SPACE STATION ORBITAL DATA:</strong> </p> <p>The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability. The data normally contains past, current and predicted orbital data. Careful attention to the orbit # / epoch times! These sources include: </p><p>NASA Orbital Flight Dynamics<br/> DOD C-Band Radar Network<br/> Goddard Space Flight Center (GSFC)<br/> NASA Johnson Space Center (JSC)<br/> DoD/ USSTRATCOM/ US Space Command with permission </p> <p>By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command. </p><pre> David Cottle Director Of Engineering IDB Communications</pre> <hr/> <p>The following information is a reminder of your current mailing list subscription: </p><p>You are subscribed to the following list: </p><p><strong>[ISSTLE LIST]</strong> </p><p>using the following email: </p><p> <a href="mailto:&#x65;&#120;&#x61;&#x6D;&#112;&#108;&#x65;&#64;&#x65;&#120;&#97;&#x6D;&#112;&#x6C;&#x65;&#46;&#x63;&#111;&#109;">&#x65;&#120;&#x61;&#x6D;&#112;&#108;&#x65;&#64;&#x65;&#120;&#97;&#x6D;&#112;&#x6C;&#x65;&#46;&#x63;&#111;&#109;</a> </p><p>You may automatically unsubscribe from this list at any time by visiting the following URL: </p><p>&#60;<a href="http://www.aus-city.com/cgi-bin/dada/mail.cgi/u/ISSTLE_LIST/example/example.com/">http://www.aus-city.com/cgi-bin/dada/mail.cgi/u/ISSTLE_LIST/example/example.com/</a>&#62; </p><p>If the above URL is inoperable, make sure that you have copied the entire address. 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subscription_form_widget.tmpl --> [ISSTLE LIST] Current ISS TLEs @ 06:30 UTC tag:www.aus-city.com,2010-07-30:%2Fcgi-bin%2Fdada%2Fmail.cgi%2Farchive%2FISSTLE_LIST%2F20100730164502%2F 2010-07-30T16:45:02Z 2010-07-30T16:45:02Z <p>&#60;B&#62; ISS TRAJECTORY DATA&#60;/B&#62; </p><p> Lift off time (UTC) : N/A<br/> Area (sq ft) : 8880.23<br/> Drag Coefficient (Cd) : 2.00<br/> Monthly MSFC 50% solar flux (F10.7-jansky) : 74.8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0.74 ET - UTC (sec) : 66.18<br/> UT1 - UTC (sec) : 0.00 </p><p> Maneuvers contained within the current ephemeris are as follows: </p><pre> IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP </pre> <hr/> There are no maneuvers. <p> Coasting Arc #1 (Orbit 2996) </p><hr/> <p> Vector Time (GMT): 2010/209/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6516113.77 A = 6739113.74 meter Y = 1075697.33 meter E = .0008112 Z = -1348545.43 I = 51.76930 XDOT = 379.902553 Wp = 90.86388 YDOT = 4984.838824 meter/sec RA = 18.63083 deg ZDOT = 5841.971976 TA = 254.38104 MA = 254.47058 Ha = 196.328 n.mi Hp = 186.522 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 21378326.01 X = 6510151.69 Y = 3529190.72 feet Y = 1148531.16 meter Z = -4424361.65 Z = -1316905.21 XDOT = 1246.399451 XDOT = 295.754282 YDOT = 16354.458084 feet/sec YDOT = 4988.616247 meter/sec ZDOT = 19166.574723 ZDOT = 5843.613434 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -9477785.26 X = -2888828.95 Y = -19513152.93 feet Y = -5947609.01 meter Z = -4297840.79 Z = -1309981.87 XDOT = 11276.028065 XDOT = 3436.933354 YDOT = -9677.510145 feet/sec YDOT = -2949.705092 meter/sec ZDOT = 19173.089367 ZDOT = 5843.957639 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10209.50254265 .00016717 00000-0 10270-3 0 9008 2 25544 51.6420 19.1528 0007751 159.6876 200.4595 15.71301570 29970 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10209.50254265 = yrday.fracday Element set: 900 Inclination: 51.6420 deg RA of node: 19.1528 deg Eccentricity: .0007751 Arg of perigee: 159.6876 deg Mean anomaly: 200.4595 deg </pre> <p> Mean motion: 15.71301570 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 2997 Checksum: 302 </pre> <p> Coasting Arc #2 (Orbit 3012) </p><hr/> <p> Vector Time (GMT): 2010/210/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1774311.45 A = 6729662.15 meter Y = -4349633.23 meter E = .0014282 Z = -4829241.59 I = 51.70945 XDOT = 7278.280118 Wp = 104.82108 YDOT = -245.294757 meter/sec RA = 13.55506 deg ZDOT = -2462.799354 TA = 141.14064 MA = 141.03787 Ha = 196.197 n.mi Hp = 186.505 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -5821231.80 X = -1702082.01 Y = -14270450.24 feet Y = -4369070.55 meter Z = -15843968.46 Z = -4837685.82 XDOT = 23878.871778 XDOT = 7292.445737 YDOT = -804.772825 feet/sec YDOT = -163.825349 meter/sec ZDOT = -8080.050375 ZDOT = -2427.407688 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -8121069.96 X = -2475302.12 Y = 13057981.64 feet Y = 3980072.80 meter Z = -15877693.94 Z = -4839521.11 XDOT = -13846.353559 XDOT = -4220.368565 YDOT = -18225.826072 feet/sec YDOT = -5555.231787 meter/sec ZDOT = -7938.519472 ZDOT = -2419.660735 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10210.52011815 .00016717 00000-0 10270-3 0 9015 2 25544 51.6427 13.9486 0007709 162.3543 197.7888 15.71326345 30137 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10210.52011815 = yrday.fracday Element set: 901 Inclination: 51.6427 deg RA of node: 13.9486 deg Eccentricity: .0007709 Arg of perigee: 162.3543 deg Mean anomaly: 197.7888 deg </pre> <p> Mean motion: 15.71326345 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3013 Checksum: 296 </pre> <p> Coasting Arc #3 (Orbit 3028) </p><hr/> <p> Vector Time (GMT): 2010/211/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5881744.62 A = 6736240.36 meter Y = 1459490.95 meter E = .0017719 Z = 2916437.15 I = 51.70098 XDOT = -3635.167120 Wp = 121.99076 YDOT = -4558.045636 meter/sec RA = 8.40128 deg ZDOT = -5037.219711 TA = 24.46598 MA = 24.38199 Ha = 196.200 n.mi Hp = 186.794 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -19297062.39 X = -5911795.10 Y = 4788356.13 feet Y = 1393549.62 meter Z = 9568363.34 Z = 2887791.09 XDOT = -11926.401311 XDOT = -3559.458478 YDOT = -14954.217967 feet/sec YDOT = -4598.272726 meter/sec ZDOT = -16526.311388 ZDOT = -5054.695412 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15524118.05 X = 4731751.18 Y = 12509434.54 feet Y = 3812875.65 meter Z = 9453801.07 Z = 2881518.56 XDOT = -3835.340678 XDOT = -1169.011839 YDOT = 17334.564542 feet/sec YDOT = 5283.575272 meter/sec ZDOT = -16596.148045 ZDOT = -5058.505924 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10211.53768462 .00016717 00000-0 10270-3 0 9025 2 25544 51.6422 8.7430 0007710 167.4197 192.7159 15.71310320 30295 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10211.53768462 = yrday.fracday Element set: 902 Inclination: 51.6422 deg RA of node: 8.7430 deg Eccentricity: .0007710 Arg of perigee: 167.4197 deg Mean anomaly: 192.7159 deg </pre> <p> Mean motion: 15.71310320 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3029 Checksum: 284 </pre> <p> Coasting Arc #4 (Orbit 3044) </p><hr/> <p> Vector Time (GMT): 2010/212/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4419500.56 A = 6733190.74 meter Y = 3308687.31 meter E = .0015535 Z = 3851289.51 I = 51.66224 XDOT = -5802.149592 Wp = 127.10210 YDOT = 2927.361394 meter/sec RA = 3.33869 deg ZDOT = 4122.665932 TA = 279.73611 MA = 279.91153 Ha = 195.907 n.mi Hp = 186.827 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 14499673.74 X = 4363465.06 Y = 10855273.34 feet Y = 3357795.34 meter Z = 12635464.26 Z = 3872623.26 XDOT = -19035.923857 XDOT = -5854.479622 YDOT = 9604.204047 feet/sec YDOT = 2862.185523 meter/sec ZDOT = 13525.806862 ZDOT = 4094.352376 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -397417.09 X = -121132.73 Y = -18048750.29 feet Y = -5501259.09 meter Z = 12720736.13 Z = 3877280.37 XDOT = 18057.107948 XDOT = 5503.806503 YDOT = 9102.850259 feet/sec YDOT = 2774.548759 meter/sec ZDOT = 13412.564880 ZDOT = 4088.149775 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10212.55524169 .00016717 00000-0 10270-3 0 9033 2 25544 51.6430 3.5383 0007738 171.3522 188.7775 15.71359169 30451 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10212.55524169 = yrday.fracday Element set: 903 Inclination: 51.6430 deg RA of node: 3.5383 deg Eccentricity: .0007738 Arg of perigee: 171.3522 deg Mean anomaly: 188.7775 deg </pre> <p> Mean motion: 15.71359169 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3045 Checksum: 308 </pre> <p> Coasting Arc #5 (Orbit 3059) </p><hr/> <p> Vector Time (GMT): 2010/213/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4010554.86 A = 6732257.00 meter Y = -3442258.01 meter E = .0013189 Z = -4184015.30 I = 51.62949 XDOT = 6175.097768 Wp = 141.00469 YDOT = 2717.752384 meter/sec RA = 358.17383 deg ZDOT = 3679.377107 TA = 166.65207 MA = 166.61715 Ha = 195.878 n.mi Hp = 187.094 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 13157988.39 X = 4069073.80 Y = -11293497.41 feet Y = -3397082.19 meter Z = -13727084.32 Z = -4164390.17 XDOT = 20259.507112 XDOT = 6126.374782 YDOT = 8916.510446 feet/sec YDOT = 2786.533419 meter/sec ZDOT = 12071.447202 ZDOT = 3709.257324 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -17120247.58 X = -5218251.46 Y = -3118003.69 feet Y = -950367.52 meter Z = -13648580.95 Z = -4160087.47 XDOT = -6080.709696 XDOT = -1853.400315 YDOT = -20030.485295 feet/sec YDOT = -6105.291918 meter/sec ZDOT = 12190.892595 ZDOT = 3715.784063 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10213.50919489 .00016717 00000-0 10270-3 0 9043 2 25544 51.6441 358.6595 0007670 174.1104 186.0150 15.71346623 30600 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10213.50919489 = yrday.fracday Element set: 904 Inclination: 51.6441 deg RA of node: 358.6595 deg Eccentricity: .0007670 Arg of perigee: 174.1104 deg Mean anomaly: 186.0150 deg </pre> <p> Mean motion: 15.71346623 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3060 Checksum: 297 </pre> <p> Coasting Arc #6 (Orbit 3075) </p><hr/> <p> Vector Time (GMT): 2010/214/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -6114171.14 A = 6736845.84 meter Y = -1267695.63 meter E = .0011658 Z = -2515463.39 I = 51.61507 XDOT = 3132.189428 Wp = 157.99540 YDOT = -4613.299231 meter/sec RA = 353.10384 deg ZDOT = -5306.794511 TA = 50.47485 MA = 50.37187 Ha = 195.629 n.mi Hp = 187.123 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -20059616.60 X = -6087321.50 Y = -4159106.41 feet Y = -1335917.68 meter Z = -8252832.65 Z = -2545100.77 XDOT = 10276.212035 XDOT = 3209.322730 YDOT = -15135.496166 feet/sec YDOT = -4577.841622 meter/sec ZDOT = -17410.743147 ZDOT = -5291.391319 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 9738019.52 X = 2968148.35 Y = 17969074.85 feet Y = 5476974.01 meter Z = -8371317.45 Z = -2551577.56 XDOT = -16949.907476 XDOT = -5166.331799 YDOT = 1131.101307 feet/sec YDOT = 344.759678 meter/sec ZDOT = -17349.109246 ZDOT = -5288.008498 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10214.52673505 .00016717 00000-0 10270-3 0 9053 2 25544 51.6439 353.4544 0007593 178.1416 181.9766 15.71369601 30763 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10214.52673505 = yrday.fracday Element set: 905 Inclination: 51.6439 deg RA of node: 353.4544 deg Eccentricity: .0007593 Arg of perigee: 178.1416 deg Mean anomaly: 181.9766 deg </pre> <p> Mean motion: 15.71369601 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3076 Checksum: 320 </pre> <p> Coasting Arc #7 (Orbit 3091) </p><hr/> <p> Vector Time (GMT): 2010/215/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1322709.43 A = 6729012.82 meter Y = 4323254.72 meter E = .0006416 Z = 4978522.94 I = 51.55880 XDOT = -7444.497362 Wp = 131.13838 YDOT = -10.479641 meter/sec RA = 347.94741 deg ZDOT = -1971.283858 TA = 337.92325 MA = 337.95087 Ha = 195.679 n.mi Hp = 187.339 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4339597.86 X = -1395139.22 Y = 14183906.55 feet Y = 4308058.03 meter Z = 16333736.67 Z = 4971921.64 XDOT = -24424.203942 XDOT = -7434.250777 YDOT = -34.382024 feet/sec YDOT = -93.671020 meter/sec ZDOT = -6467.466727 ZDOT = -2007.424212 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13596498.05 X = 4144212.61 Y = -6001131.00 feet Y = -1829144.73 meter Z = 16307297.02 Z = 4970464.13 XDOT = 15593.251658 XDOT = 4752.823105 YDOT = 17384.177102 feet/sec YDOT = 5298.697181 meter/sec ZDOT = -6611.962626 ZDOT = -2015.326208 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10215.54426839 .00016717 00000-0 10270-3 0 9063 2 25544 51.6444 348.2500 0007585 181.1250 178.9896 15.71343549 30925 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10215.54426839 = yrday.fracday Element set: 906 Inclination: 51.6444 deg RA of node: 348.2500 deg Eccentricity: .0007585 Arg of perigee: 181.1250 deg Mean anomaly: 178.9896 deg </pre> <p> Mean motion: 15.71343549 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3092 Checksum: 322 </pre> <p> Coasting Arc #8 (Orbit 3107) </p><hr/> <p> Vector Time (GMT): 2010/216/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6554450.82 A = 6739193.01 meter Y = -1276112.99 meter E = .0010474 Z = 898718.08 I = 51.56537 XDOT = 129.990087 Wp = 87.88706 YDOT = 4890.130543 meter/sec RA = 342.85144 deg ZDOT = 5936.504210 TA = 281.91723 MA = 282.03464 Ha = 195.430 n.mi Hp = 187.413 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 21504103.73 X = 6563867.62 Y = -4186722.40 feet Y = -1202764.63 meter Z = 2948550.15 Z = 930582.21 XDOT = 426.476662 XDOT = 46.459769 YDOT = 16043.735376 feet/sec YDOT = 4891.116576 meter/sec ZDOT = 19476.719850 ZDOT = 5936.933259 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -17526971.96 X = -5342221.05 Y = -13114601.60 feet Y = -3997330.57 meter Z = 3075963.04 Z = 937553.54 XDOT = 10726.507000 XDOT = 3269.439334 YDOT = -9723.270816 feet/sec YDOT = -2963.652945 meter/sec ZDOT = 19478.381513 ZDOT = 5937.010685 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10216.56178918 .00016717 00000-0 10270-3 0 9079 2 25544 51.6453 343.0452 0007540 185.6751 174.4326 15.71404114 31083 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10216.56178918 = yrday.fracday Element set: 907 Inclination: 51.6453 deg RA of node: 343.0452 deg Eccentricity: .0007540 Arg of perigee: 185.6751 deg Mean anomaly: 174.4326 deg </pre> <p> Mean motion: 15.71404114 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3108 Checksum: 296 </pre> <p> Coasting Arc #9 (Orbit 3122) </p><hr/> <p> Vector Time (GMT): 2010/217/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1496796.08 A = 6727457.31 meter Y = -3918621.57 meter E = .0015736 Z = -5271540.75 I = 51.49749 XDOT = 7137.823361 Wp = 118.29976 YDOT = -2851.102041 meter/sec RA = 337.71922 deg ZDOT = 85.537640 TA = 152.55661 MA = 152.47341 Ha = 195.219 n.mi Hp = 187.552 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4910748.30 X = -1427258.10 Y = -12856369.98 feet Y = -3934970.27 meter Z = -17295081.20 Z = -5278643.64 XDOT = 23418.055646 XDOT = 7168.758882 YDOT = -9354.009320 feet/sec YDOT = -2771.109672 meter/sec ZDOT = 280.635302 ZDOT = 120.287756 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -6090738.55 X = -1856457.11 Y = 12301339.34 feet Y = 3749448.23 meter Z = -17323437.47 Z = -5280183.74 XDOT = -21942.487771 XDOT = -6688.070273 YDOT = -10240.519835 feet/sec YDOT = -3121.310446 meter/sec ZDOT = 419.606633 ZDOT = 127.896102 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10217.51570882 .00016717 00000-0 10270-3 0 9082 2 25544 51.6454 338.1665 0007393 189.5722 170.5300 15.71425065 31236 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10217.51570882 = yrday.fracday Element set: 908 Inclination: 51.6454 deg RA of node: 338.1665 deg Eccentricity: .0007393 Arg of perigee: 189.5722 deg Mean anomaly: 170.5300 deg </pre> <p> Mean motion: 15.71425065 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3123 Checksum: 302 </pre> <p> Coasting Arc #10 (Orbit 3138) </p><hr/> <p> Vector Time (GMT): 2010/218/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5634666.80 A = 6739330.60 meter Y = 3598580.54 meter E = .0017768 Z = 754981.09 I = 51.50999 XDOT = -3169.172308 Wp = 149.53391 YDOT = -3700.840956 meter/sec RA = 332.58728 deg ZDOT = -5966.615392 TA = 22.22373 MA = 22.14681 Ha = 195.121 n.mi Hp = 187.839 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -18486439.62 X = -5678155.52 Y = 11806366.61 feet Y = 3535327.09 meter Z = 2476972.09 Z = 727502.99 XDOT = -10397.546942 XDOT = -3098.568909 YDOT = -12141.866655 feet/sec YDOT = -3735.885099 meter/sec ZDOT = -19575.509815 ZDOT = -5981.839966 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 21356937.60 X = 6509594.58 Y = 5054933.03 feet Y = 1540743.59 meter Z = 2367065.97 Z = 721481.71 XDOT = -1185.350720 XDOT = -361.294899 YDOT = 14277.199512 feet/sec YDOT = 4351.690411 meter/sec ZDOT = -19636.344463 ZDOT = -5985.157792 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10218.53321460 .00016717 00000-0 10270-3 0 9092 2 25544 51.6456 332.9611 0007446 193.6726 166.4235 15.71412878 31396 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10218.53321460 = yrday.fracday Element set: 909 Inclination: 51.6456 deg RA of node: 332.9611 deg Eccentricity: .0007446 Arg of perigee: 193.6726 deg Mean anomaly: 166.4235 deg </pre> <p> Mean motion: 15.71412878 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3139 Checksum: 312 </pre> <p> Coasting Arc #11 (Orbit 3154) </p><hr/> <p> Vector Time (GMT): 2010/219/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3852425.73 A = 6728364.79 meter Y = 2288407.10 meter E = .0010291 Z = 5020088.82 I = 51.44828 XDOT = -5421.943077 Wp = 167.77085 YDOT = 5157.095545 meter/sec RA = 327.48205 deg ZDOT = 1799.375050 TA = 264.77519 MA = 264.89263 Ha = 194.794 n.mi Hp = 187.945 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12639192.01 X = 3802163.77 Y = 7507897.32 feet Y = 2331205.67 meter Z = 16470107.69 Z = 5038681.74 XDOT = -17788.527156 XDOT = -5487.948576 YDOT = 16919.604806 feet/sec YDOT = 5096.094888 meter/sec ZDOT = 5903.461449 ZDOT = 1772.875937 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -3589803.16 X = -1094172.00 Y = -14169590.19 feet Y = -4318891.09 meter Z = 16544430.22 Z = 5042742.33 XDOT = 23535.064409 XDOT = 7173.487632 YDOT = 846.928604 feet/sec YDOT = 258.143838 meter/sec ZDOT = 5797.453857 ZDOT = 1767.063936 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10219.55070986 .00016717 00000-0 10270-3 0 9101 2 25544 51.6465 327.7563 0007346 198.1419 161.9482 15.71467617 31555 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10219.55070986 = yrday.fracday Element set: 910 Inclination: 51.6465 deg RA of node: 327.7563 deg Eccentricity: .0007346 Arg of perigee: 198.1419 deg Mean anomaly: 161.9482 deg </pre> <p> Mean motion: 15.71467617 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3155 Checksum: 330 </pre> <p> Coasting Arc #12 (Orbit 3169) </p><hr/> <p> Vector Time (GMT): 2010/220/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3639647.56 A = 6737196.89 meter Y = -5166686.31 meter E = .0002833 Z = -2339622.53 I = 51.45268 XDOT = 5326.149311 Wp = 150.86546 YDOT = 1311.796888 meter/sec RA = 322.31817 deg ZDOT = 5389.064192 TA = 182.78157 MA = 182.78315 Ha = 194.744 n.mi Hp = 188.283 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 11941100.90 X = 3708517.09 Y = -16951070.57 feet Y = -5125600.32 meter Z = -7675926.94 Z = -2321774.69 XDOT = 17474.243146 XDOT = 5284.906197 YDOT = 4303.795564 feet/sec YDOT = 1371.126005 meter/sec ZDOT = 17680.656799 ZDOT = 5414.837984 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -20390127.25 X = -6214910.79 Y = 3906734.97 feet Y = 1190772.82 meter Z = -7604516.49 Z = -2317856.63 XDOT = -9248.690870 XDOT = -2819.000977 YDOT = -13656.713544 feet/sec YDOT = -4162.566288 meter/sec ZDOT = 17783.707220 ZDOT = 5420.473961 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10220.50460613 .00016717 00000-0 10270-3 0 9119 2 25544 51.6466 322.8773 0007135 202.3950 157.6901 15.71419937 31706 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10220.50460613 = yrday.fracday Element set: 911 Inclination: 51.6466 deg RA of node: 322.8773 deg Eccentricity: .0007135 Arg of perigee: 202.3950 deg Mean anomaly: 157.6901 deg </pre> <p> Mean motion: 15.71419937 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3170 Checksum: 289 </pre> <p> Coasting Arc #13 (Orbit 3185) </p><hr/> <p> Vector Time (GMT): 2010/221/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5178556.93 A = 6731316.08 meter Y = 114342.49 meter E = .0006174 Z = -4301250.23 I = 51.41004 XDOT = 2735.329701 Wp = 123.11274 YDOT = -6299.404364 meter/sec RA = 317.23280 deg ZDOT = -3467.612429 TA = 111.70513 MA = 111.63939 Ha = 194.517 n.mi Hp = 188.270 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -16990016.16 X = -5158556.47 Y = 375139.40 feet Y = 56544.84 meter Z = -14111713.37 Z = -4326358.45 XDOT = 8974.178808 XDOT = 2822.412108 YDOT = -20667.337152 feet/sec YDOT = -6268.329171 meter/sec ZDOT = -11376.681196 ZDOT = -3454.113368 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 12638795.32 X = 3852304.81 Y = 11234697.99 feet Y = 3424335.95 meter Z = -14212116.20 Z = -4331853.02 XDOT = -19873.487666 XDOT = -6057.439041 YDOT = 8062.331633 feet/sec YDOT = 2457.398682 meter/sec ZDOT = -11322.660776 ZDOT = -3451.147004 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10221.52208609 .00016717 00000-0 10270-3 0 9128 2 25544 51.6465 317.6729 0007254 205.8198 154.2602 15.71447118 31862 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10221.52208609 = yrday.fracday Element set: 912 Inclination: 51.6465 deg RA of node: 317.6729 deg Eccentricity: .0007254 Arg of perigee: 205.8198 deg Mean anomaly: 154.2602 deg </pre> <p> Mean motion: 15.71447118 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3186 Checksum: 304 </pre> <p> Coasting Arc #14 (Orbit 3201) </p><hr/> <p> Vector Time (GMT): 2010/222/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1062265.70 A = 6733589.46 meter Y = 5542441.95 meter E = .0009896 Z = 3661620.69 I = 51.39600 XDOT = -6153.257976 Wp = 120.96690 YDOT = 1675.330307 meter/sec RA = 312.05045 deg ZDOT = -4317.393796 TA = 14.88559 MA = 14.85648 Ha = 194.405 n.mi Hp = 188.494 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -3485123.70 X = -1141950.41 Y = 18183864.67 feet Y = 5530117.43 meter Z = 12013191.26 Z = 3656266.92 XDOT = -20187.854253 XDOT = -6150.561900 YDOT = 5496.490509 feet/sec YDOT = 1606.536074 meter/sec ZDOT = -14164.677810 ZDOT = -4347.279001 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 14794491.51 X = 4509361.01 Y = -11155113.70 feet Y = -3400078.65 meter Z = 11991757.39 Z = 3655087.65 XDOT = 17817.378026 XDOT = 5430.736822 YDOT = 8262.119505 feet/sec YDOT = 2518.294025 meter/sec ZDOT = -14284.189939 ZDOT = -4353.821094 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10222.53955771 .00016717 00000-0 10270-3 0 9130 2 25544 51.6463 312.4685 0007040 208.9289 151.1483 15.71468869 32020 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10222.53955771 = yrday.fracday Element set: 913 Inclination: 51.6463 deg RA of node: 312.4685 deg Eccentricity: .0007040 Arg of perigee: 208.9289 deg Mean anomaly: 151.1483 deg </pre> <p> Mean motion: 15.71468869 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3202 Checksum: 314 </pre> <p> Coasting Arc #15 (Orbit 3217) </p><hr/> <p> Vector Time (GMT): 2010/223/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 5254637.81 A = 6734882.87 meter Y = -2783503.44 meter E = .0010370 Z = 3160246.31 I = 51.38122 XDOT = 282.273681 Wp = 119.41242 YDOT = 6004.650423 meter/sec RA = 306.96700 deg ZDOT = 4802.618807 TA = 277.50424 MA = 277.62204 Ha = 194.183 n.mi Hp = 188.600 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 17239625.35 X = 5270021.33 Y = -9132229.12 feet Y = -2724656.92 meter Z = 10368262.18 Z = 3185810.18 XDOT = 926.094754 XDOT = 191.777833 YDOT = 19700.296665 feet/sec YDOT = 6007.300989 meter/sec ZDOT = 15756.623382 ZDOT = 4803.770252 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -18960539.28 X = -5779172.37 Y = -4355442.62 feet Y = -1327538.91 meter Z = 10470492.89 Z = 3191406.23 XDOT = 11960.626866 XDOT = 3645.599069 YDOT = -14046.562501 feet/sec YDOT = -4281.392250 meter/sec ZDOT = 15761.210708 ZDOT = 4804.017024 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10223.55701894 .00016717 00000-0 10270-3 0 9149 2 25544 51.6460 307.2632 0007070 213.6446 146.4268 15.71502866 32183 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10223.55701894 = yrday.fracday Element set: 914 Inclination: 51.6460 deg RA of node: 307.2632 deg Eccentricity: .0007070 Arg of perigee: 213.6446 deg Mean anomaly: 146.4268 deg </pre> <p> Mean motion: 15.71502866 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3218 Checksum: 296</pre> <hr/> <p><strong>INTERNATIONAL SPACE STATION ORBITAL DATA:</strong> </p> <p>The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability. The data normally contains past, current and predicted orbital data. Careful attention to the orbit # / epoch times! These sources include: </p><p>NASA Orbital Flight Dynamics<br/> DOD C-Band Radar Network<br/> Goddard Space Flight Center (GSFC)<br/> NASA Johnson Space Center (JSC)<br/> DoD/ USSTRATCOM/ US Space Command with permission </p> <p>By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command. </p><pre> David Cottle Director Of Engineering IDB Communications</pre> <hr/> <p>The following information is a reminder of your current mailing list subscription: </p><p>You are subscribed to the following list: </p><p><strong>[ISSTLE LIST]</strong> </p><p>using the following email: </p><p> <a href="mailto:&#101;&#x78;&#97;&#109;&#112;&#108;&#101;&#x40;&#x65;&#x78;&#x61;&#109;&#x70;&#108;&#101;&#46;&#99;&#x6F;&#109;">&#101;&#x78;&#97;&#109;&#112;&#108;&#101;&#x40;&#x65;&#x78;&#x61;&#109;&#x70;&#108;&#101;&#46;&#99;&#x6F;&#109;</a> </p><p>You may automatically unsubscribe from this list at any time by visiting the following URL: </p><p>&#60;<a href="http://www.aus-city.com/cgi-bin/dada/mail.cgi/u/ISSTLE_LIST/example/example.com/">http://www.aus-city.com/cgi-bin/dada/mail.cgi/u/ISSTLE_LIST/example/example.com/</a>&#62; </p><p>If the above URL is inoperable, make sure that you have copied the entire address. 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subscription_form_widget.tmpl --> [ISSTLE LIST] Current ISS TLEs @ 18:30 UTC tag:www.aus-city.com,2010-07-30:%2Fcgi-bin%2Fdada%2Fmail.cgi%2Farchive%2FISSTLE_LIST%2F20100730044502%2F 2010-07-30T04:45:02Z 2010-07-30T04:45:02Z <p>&#60;B&#62; ISS TRAJECTORY DATA&#60;/B&#62; </p><p> Lift off time (UTC) : N/A<br/> Area (sq ft) : 8880.23<br/> Drag Coefficient (Cd) : 2.00<br/> Monthly MSFC 50% solar flux (F10.7-jansky) : 74.8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0.74 ET - UTC (sec) : 66.18<br/> UT1 - UTC (sec) : 0.00 </p><p> Maneuvers contained within the current ephemeris are as follows: </p><pre> IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP </pre> <hr/> There are no maneuvers. <p> Coasting Arc #1 (Orbit 2996) </p><hr/> <p> Vector Time (GMT): 2010/209/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6516113.77 A = 6739113.74 meter Y = 1075697.33 meter E = .0008112 Z = -1348545.43 I = 51.76930 XDOT = 379.902553 Wp = 90.86388 YDOT = 4984.838824 meter/sec RA = 18.63083 deg ZDOT = 5841.971976 TA = 254.38104 MA = 254.47058 Ha = 196.328 n.mi Hp = 186.522 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 21378326.01 X = 6510151.69 Y = 3529190.72 feet Y = 1148531.16 meter Z = -4424361.65 Z = -1316905.21 XDOT = 1246.399451 XDOT = 295.754282 YDOT = 16354.458084 feet/sec YDOT = 4988.616247 meter/sec ZDOT = 19166.574723 ZDOT = 5843.613434 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -9477785.26 X = -2888828.95 Y = -19513152.93 feet Y = -5947609.01 meter Z = -4297840.79 Z = -1309981.87 XDOT = 11276.028065 XDOT = 3436.933354 YDOT = -9677.510145 feet/sec YDOT = -2949.705092 meter/sec ZDOT = 19173.089367 ZDOT = 5843.957639 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10209.50254265 .00016717 00000-0 10270-3 0 9008 2 25544 51.6420 19.1528 0007751 159.6876 200.4595 15.71301570 29970 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10209.50254265 = yrday.fracday Element set: 900 Inclination: 51.6420 deg RA of node: 19.1528 deg Eccentricity: .0007751 Arg of perigee: 159.6876 deg Mean anomaly: 200.4595 deg </pre> <p> Mean motion: 15.71301570 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 2997 Checksum: 302 </pre> <p> Coasting Arc #2 (Orbit 3012) </p><hr/> <p> Vector Time (GMT): 2010/210/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1774311.45 A = 6729662.15 meter Y = -4349633.23 meter E = .0014282 Z = -4829241.59 I = 51.70945 XDOT = 7278.280118 Wp = 104.82108 YDOT = -245.294757 meter/sec RA = 13.55506 deg ZDOT = -2462.799354 TA = 141.14064 MA = 141.03787 Ha = 196.197 n.mi Hp = 186.505 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -5821231.80 X = -1702082.01 Y = -14270450.24 feet Y = -4369070.55 meter Z = -15843968.46 Z = -4837685.82 XDOT = 23878.871778 XDOT = 7292.445737 YDOT = -804.772825 feet/sec YDOT = -163.825349 meter/sec ZDOT = -8080.050375 ZDOT = -2427.407688 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -8121069.96 X = -2475302.12 Y = 13057981.64 feet Y = 3980072.80 meter Z = -15877693.94 Z = -4839521.11 XDOT = -13846.353559 XDOT = -4220.368565 YDOT = -18225.826072 feet/sec YDOT = -5555.231787 meter/sec ZDOT = -7938.519472 ZDOT = -2419.660735 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10210.52011815 .00016717 00000-0 10270-3 0 9015 2 25544 51.6427 13.9486 0007709 162.3543 197.7888 15.71326345 30137 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10210.52011815 = yrday.fracday Element set: 901 Inclination: 51.6427 deg RA of node: 13.9486 deg Eccentricity: .0007709 Arg of perigee: 162.3543 deg Mean anomaly: 197.7888 deg </pre> <p> Mean motion: 15.71326345 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3013 Checksum: 296 </pre> <p> Coasting Arc #3 (Orbit 3028) </p><hr/> <p> Vector Time (GMT): 2010/211/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5881744.62 A = 6736240.36 meter Y = 1459490.95 meter E = .0017719 Z = 2916437.15 I = 51.70098 XDOT = -3635.167120 Wp = 121.99076 YDOT = -4558.045636 meter/sec RA = 8.40128 deg ZDOT = -5037.219711 TA = 24.46598 MA = 24.38199 Ha = 196.200 n.mi Hp = 186.794 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -19297062.39 X = -5911795.10 Y = 4788356.13 feet Y = 1393549.62 meter Z = 9568363.34 Z = 2887791.09 XDOT = -11926.401311 XDOT = -3559.458478 YDOT = -14954.217967 feet/sec YDOT = -4598.272726 meter/sec ZDOT = -16526.311388 ZDOT = -5054.695412 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15524118.05 X = 4731751.18 Y = 12509434.54 feet Y = 3812875.65 meter Z = 9453801.07 Z = 2881518.56 XDOT = -3835.340678 XDOT = -1169.011839 YDOT = 17334.564542 feet/sec YDOT = 5283.575272 meter/sec ZDOT = -16596.148045 ZDOT = -5058.505924 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10211.53768462 .00016717 00000-0 10270-3 0 9025 2 25544 51.6422 8.7430 0007710 167.4197 192.7159 15.71310320 30295 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10211.53768462 = yrday.fracday Element set: 902 Inclination: 51.6422 deg RA of node: 8.7430 deg Eccentricity: .0007710 Arg of perigee: 167.4197 deg Mean anomaly: 192.7159 deg </pre> <p> Mean motion: 15.71310320 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3029 Checksum: 284 </pre> <p> Coasting Arc #4 (Orbit 3044) </p><hr/> <p> Vector Time (GMT): 2010/212/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4419500.56 A = 6733190.74 meter Y = 3308687.31 meter E = .0015535 Z = 3851289.51 I = 51.66224 XDOT = -5802.149592 Wp = 127.10210 YDOT = 2927.361394 meter/sec RA = 3.33869 deg ZDOT = 4122.665932 TA = 279.73611 MA = 279.91153 Ha = 195.907 n.mi Hp = 186.827 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 14499673.74 X = 4363465.06 Y = 10855273.34 feet Y = 3357795.34 meter Z = 12635464.26 Z = 3872623.26 XDOT = -19035.923857 XDOT = -5854.479622 YDOT = 9604.204047 feet/sec YDOT = 2862.185523 meter/sec ZDOT = 13525.806862 ZDOT = 4094.352376 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -397417.09 X = -121132.73 Y = -18048750.29 feet Y = -5501259.09 meter Z = 12720736.13 Z = 3877280.37 XDOT = 18057.107948 XDOT = 5503.806503 YDOT = 9102.850259 feet/sec YDOT = 2774.548759 meter/sec ZDOT = 13412.564880 ZDOT = 4088.149775 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10212.55524169 .00016717 00000-0 10270-3 0 9033 2 25544 51.6430 3.5383 0007738 171.3522 188.7775 15.71359169 30451 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10212.55524169 = yrday.fracday Element set: 903 Inclination: 51.6430 deg RA of node: 3.5383 deg Eccentricity: .0007738 Arg of perigee: 171.3522 deg Mean anomaly: 188.7775 deg </pre> <p> Mean motion: 15.71359169 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3045 Checksum: 308 </pre> <p> Coasting Arc #5 (Orbit 3059) </p><hr/> <p> Vector Time (GMT): 2010/213/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4010554.86 A = 6732257.00 meter Y = -3442258.01 meter E = .0013189 Z = -4184015.30 I = 51.62949 XDOT = 6175.097768 Wp = 141.00469 YDOT = 2717.752384 meter/sec RA = 358.17383 deg ZDOT = 3679.377107 TA = 166.65207 MA = 166.61715 Ha = 195.878 n.mi Hp = 187.094 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 13157988.39 X = 4069073.80 Y = -11293497.41 feet Y = -3397082.19 meter Z = -13727084.32 Z = -4164390.17 XDOT = 20259.507112 XDOT = 6126.374782 YDOT = 8916.510446 feet/sec YDOT = 2786.533419 meter/sec ZDOT = 12071.447202 ZDOT = 3709.257324 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -17120247.58 X = -5218251.46 Y = -3118003.69 feet Y = -950367.52 meter Z = -13648580.95 Z = -4160087.47 XDOT = -6080.709696 XDOT = -1853.400315 YDOT = -20030.485295 feet/sec YDOT = -6105.291918 meter/sec ZDOT = 12190.892595 ZDOT = 3715.784063 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10213.50919489 .00016717 00000-0 10270-3 0 9043 2 25544 51.6441 358.6595 0007670 174.1104 186.0150 15.71346623 30600 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10213.50919489 = yrday.fracday Element set: 904 Inclination: 51.6441 deg RA of node: 358.6595 deg Eccentricity: .0007670 Arg of perigee: 174.1104 deg Mean anomaly: 186.0150 deg </pre> <p> Mean motion: 15.71346623 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3060 Checksum: 297 </pre> <p> Coasting Arc #6 (Orbit 3075) </p><hr/> <p> Vector Time (GMT): 2010/214/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -6114171.14 A = 6736845.84 meter Y = -1267695.63 meter E = .0011658 Z = -2515463.39 I = 51.61507 XDOT = 3132.189428 Wp = 157.99540 YDOT = -4613.299231 meter/sec RA = 353.10384 deg ZDOT = -5306.794511 TA = 50.47485 MA = 50.37187 Ha = 195.629 n.mi Hp = 187.123 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -20059616.60 X = -6087321.50 Y = -4159106.41 feet Y = -1335917.68 meter Z = -8252832.65 Z = -2545100.77 XDOT = 10276.212035 XDOT = 3209.322730 YDOT = -15135.496166 feet/sec YDOT = -4577.841622 meter/sec ZDOT = -17410.743147 ZDOT = -5291.391319 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 9738019.52 X = 2968148.35 Y = 17969074.85 feet Y = 5476974.01 meter Z = -8371317.45 Z = -2551577.56 XDOT = -16949.907476 XDOT = -5166.331799 YDOT = 1131.101307 feet/sec YDOT = 344.759678 meter/sec ZDOT = -17349.109246 ZDOT = -5288.008498 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10214.52673505 .00016717 00000-0 10270-3 0 9053 2 25544 51.6439 353.4544 0007593 178.1416 181.9766 15.71369601 30763 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10214.52673505 = yrday.fracday Element set: 905 Inclination: 51.6439 deg RA of node: 353.4544 deg Eccentricity: .0007593 Arg of perigee: 178.1416 deg Mean anomaly: 181.9766 deg </pre> <p> Mean motion: 15.71369601 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3076 Checksum: 320 </pre> <p> Coasting Arc #7 (Orbit 3091) </p><hr/> <p> Vector Time (GMT): 2010/215/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1322709.43 A = 6729012.82 meter Y = 4323254.72 meter E = .0006416 Z = 4978522.94 I = 51.55880 XDOT = -7444.497362 Wp = 131.13838 YDOT = -10.479641 meter/sec RA = 347.94741 deg ZDOT = -1971.283858 TA = 337.92325 MA = 337.95087 Ha = 195.679 n.mi Hp = 187.339 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4339597.86 X = -1395139.22 Y = 14183906.55 feet Y = 4308058.03 meter Z = 16333736.67 Z = 4971921.64 XDOT = -24424.203942 XDOT = -7434.250777 YDOT = -34.382024 feet/sec YDOT = -93.671020 meter/sec ZDOT = -6467.466727 ZDOT = -2007.424212 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13596498.05 X = 4144212.61 Y = -6001131.00 feet Y = -1829144.73 meter Z = 16307297.02 Z = 4970464.13 XDOT = 15593.251658 XDOT = 4752.823105 YDOT = 17384.177102 feet/sec YDOT = 5298.697181 meter/sec ZDOT = -6611.962626 ZDOT = -2015.326208 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10215.54426839 .00016717 00000-0 10270-3 0 9063 2 25544 51.6444 348.2500 0007585 181.1250 178.9896 15.71343549 30925 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10215.54426839 = yrday.fracday Element set: 906 Inclination: 51.6444 deg RA of node: 348.2500 deg Eccentricity: .0007585 Arg of perigee: 181.1250 deg Mean anomaly: 178.9896 deg </pre> <p> Mean motion: 15.71343549 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3092 Checksum: 322 </pre> <p> Coasting Arc #8 (Orbit 3107) </p><hr/> <p> Vector Time (GMT): 2010/216/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6554450.82 A = 6739193.01 meter Y = -1276112.99 meter E = .0010474 Z = 898718.08 I = 51.56537 XDOT = 129.990087 Wp = 87.88706 YDOT = 4890.130543 meter/sec RA = 342.85144 deg ZDOT = 5936.504210 TA = 281.91723 MA = 282.03464 Ha = 195.430 n.mi Hp = 187.413 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 21504103.73 X = 6563867.62 Y = -4186722.40 feet Y = -1202764.63 meter Z = 2948550.15 Z = 930582.21 XDOT = 426.476662 XDOT = 46.459769 YDOT = 16043.735376 feet/sec YDOT = 4891.116576 meter/sec ZDOT = 19476.719850 ZDOT = 5936.933259 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -17526971.96 X = -5342221.05 Y = -13114601.60 feet Y = -3997330.57 meter Z = 3075963.04 Z = 937553.54 XDOT = 10726.507000 XDOT = 3269.439334 YDOT = -9723.270816 feet/sec YDOT = -2963.652945 meter/sec ZDOT = 19478.381513 ZDOT = 5937.010685 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10216.56178918 .00016717 00000-0 10270-3 0 9079 2 25544 51.6453 343.0452 0007540 185.6751 174.4326 15.71404114 31083 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10216.56178918 = yrday.fracday Element set: 907 Inclination: 51.6453 deg RA of node: 343.0452 deg Eccentricity: .0007540 Arg of perigee: 185.6751 deg Mean anomaly: 174.4326 deg </pre> <p> Mean motion: 15.71404114 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3108 Checksum: 296 </pre> <p> Coasting Arc #9 (Orbit 3122) </p><hr/> <p> Vector Time (GMT): 2010/217/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1496796.08 A = 6727457.31 meter Y = -3918621.57 meter E = .0015736 Z = -5271540.75 I = 51.49749 XDOT = 7137.823361 Wp = 118.29976 YDOT = -2851.102041 meter/sec RA = 337.71922 deg ZDOT = 85.537640 TA = 152.55661 MA = 152.47341 Ha = 195.219 n.mi Hp = 187.552 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4910748.30 X = -1427258.10 Y = -12856369.98 feet Y = -3934970.27 meter Z = -17295081.20 Z = -5278643.64 XDOT = 23418.055646 XDOT = 7168.758882 YDOT = -9354.009320 feet/sec YDOT = -2771.109672 meter/sec ZDOT = 280.635302 ZDOT = 120.287756 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -6090738.55 X = -1856457.11 Y = 12301339.34 feet Y = 3749448.23 meter Z = -17323437.47 Z = -5280183.74 XDOT = -21942.487771 XDOT = -6688.070273 YDOT = -10240.519835 feet/sec YDOT = -3121.310446 meter/sec ZDOT = 419.606633 ZDOT = 127.896102 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10217.51570882 .00016717 00000-0 10270-3 0 9082 2 25544 51.6454 338.1665 0007393 189.5722 170.5300 15.71425065 31236 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10217.51570882 = yrday.fracday Element set: 908 Inclination: 51.6454 deg RA of node: 338.1665 deg Eccentricity: .0007393 Arg of perigee: 189.5722 deg Mean anomaly: 170.5300 deg </pre> <p> Mean motion: 15.71425065 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3123 Checksum: 302 </pre> <p> Coasting Arc #10 (Orbit 3138) </p><hr/> <p> Vector Time (GMT): 2010/218/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5634666.80 A = 6739330.60 meter Y = 3598580.54 meter E = .0017768 Z = 754981.09 I = 51.50999 XDOT = -3169.172308 Wp = 149.53391 YDOT = -3700.840956 meter/sec RA = 332.58728 deg ZDOT = -5966.615392 TA = 22.22373 MA = 22.14681 Ha = 195.121 n.mi Hp = 187.839 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -18486439.62 X = -5678155.52 Y = 11806366.61 feet Y = 3535327.09 meter Z = 2476972.09 Z = 727502.99 XDOT = -10397.546942 XDOT = -3098.568909 YDOT = -12141.866655 feet/sec YDOT = -3735.885099 meter/sec ZDOT = -19575.509815 ZDOT = -5981.839966 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 21356937.60 X = 6509594.58 Y = 5054933.03 feet Y = 1540743.59 meter Z = 2367065.97 Z = 721481.71 XDOT = -1185.350720 XDOT = -361.294899 YDOT = 14277.199512 feet/sec YDOT = 4351.690411 meter/sec ZDOT = -19636.344463 ZDOT = -5985.157792 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10218.53321460 .00016717 00000-0 10270-3 0 9092 2 25544 51.6456 332.9611 0007446 193.6726 166.4235 15.71412878 31396 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10218.53321460 = yrday.fracday Element set: 909 Inclination: 51.6456 deg RA of node: 332.9611 deg Eccentricity: .0007446 Arg of perigee: 193.6726 deg Mean anomaly: 166.4235 deg </pre> <p> Mean motion: 15.71412878 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3139 Checksum: 312 </pre> <p> Coasting Arc #11 (Orbit 3154) </p><hr/> <p> Vector Time (GMT): 2010/219/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3852425.73 A = 6728364.79 meter Y = 2288407.10 meter E = .0010291 Z = 5020088.82 I = 51.44828 XDOT = -5421.943077 Wp = 167.77085 YDOT = 5157.095545 meter/sec RA = 327.48205 deg ZDOT = 1799.375050 TA = 264.77519 MA = 264.89263 Ha = 194.794 n.mi Hp = 187.945 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12639192.01 X = 3802163.77 Y = 7507897.32 feet Y = 2331205.67 meter Z = 16470107.69 Z = 5038681.74 XDOT = -17788.527156 XDOT = -5487.948576 YDOT = 16919.604806 feet/sec YDOT = 5096.094888 meter/sec ZDOT = 5903.461449 ZDOT = 1772.875937 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -3589803.16 X = -1094172.00 Y = -14169590.19 feet Y = -4318891.09 meter Z = 16544430.22 Z = 5042742.33 XDOT = 23535.064409 XDOT = 7173.487632 YDOT = 846.928604 feet/sec YDOT = 258.143838 meter/sec ZDOT = 5797.453857 ZDOT = 1767.063936 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10219.55070986 .00016717 00000-0 10270-3 0 9101 2 25544 51.6465 327.7563 0007346 198.1419 161.9482 15.71467617 31555 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10219.55070986 = yrday.fracday Element set: 910 Inclination: 51.6465 deg RA of node: 327.7563 deg Eccentricity: .0007346 Arg of perigee: 198.1419 deg Mean anomaly: 161.9482 deg </pre> <p> Mean motion: 15.71467617 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3155 Checksum: 330 </pre> <p> Coasting Arc #12 (Orbit 3169) </p><hr/> <p> Vector Time (GMT): 2010/220/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3639647.56 A = 6737196.89 meter Y = -5166686.31 meter E = .0002833 Z = -2339622.53 I = 51.45268 XDOT = 5326.149311 Wp = 150.86546 YDOT = 1311.796888 meter/sec RA = 322.31817 deg ZDOT = 5389.064192 TA = 182.78157 MA = 182.78315 Ha = 194.744 n.mi Hp = 188.283 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 11941100.90 X = 3708517.09 Y = -16951070.57 feet Y = -5125600.32 meter Z = -7675926.94 Z = -2321774.69 XDOT = 17474.243146 XDOT = 5284.906197 YDOT = 4303.795564 feet/sec YDOT = 1371.126005 meter/sec ZDOT = 17680.656799 ZDOT = 5414.837984 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -20390127.25 X = -6214910.79 Y = 3906734.97 feet Y = 1190772.82 meter Z = -7604516.49 Z = -2317856.63 XDOT = -9248.690870 XDOT = -2819.000977 YDOT = -13656.713544 feet/sec YDOT = -4162.566288 meter/sec ZDOT = 17783.707220 ZDOT = 5420.473961 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10220.50460613 .00016717 00000-0 10270-3 0 9119 2 25544 51.6466 322.8773 0007135 202.3950 157.6901 15.71419937 31706 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10220.50460613 = yrday.fracday Element set: 911 Inclination: 51.6466 deg RA of node: 322.8773 deg Eccentricity: .0007135 Arg of perigee: 202.3950 deg Mean anomaly: 157.6901 deg </pre> <p> Mean motion: 15.71419937 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3170 Checksum: 289 </pre> <p> Coasting Arc #13 (Orbit 3185) </p><hr/> <p> Vector Time (GMT): 2010/221/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5178556.93 A = 6731316.08 meter Y = 114342.49 meter E = .0006174 Z = -4301250.23 I = 51.41004 XDOT = 2735.329701 Wp = 123.11274 YDOT = -6299.404364 meter/sec RA = 317.23280 deg ZDOT = -3467.612429 TA = 111.70513 MA = 111.63939 Ha = 194.517 n.mi Hp = 188.270 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -16990016.16 X = -5158556.47 Y = 375139.40 feet Y = 56544.84 meter Z = -14111713.37 Z = -4326358.45 XDOT = 8974.178808 XDOT = 2822.412108 YDOT = -20667.337152 feet/sec YDOT = -6268.329171 meter/sec ZDOT = -11376.681196 ZDOT = -3454.113368 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 12638795.32 X = 3852304.81 Y = 11234697.99 feet Y = 3424335.95 meter Z = -14212116.20 Z = -4331853.02 XDOT = -19873.487666 XDOT = -6057.439041 YDOT = 8062.331633 feet/sec YDOT = 2457.398682 meter/sec ZDOT = -11322.660776 ZDOT = -3451.147004 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10221.52208609 .00016717 00000-0 10270-3 0 9128 2 25544 51.6465 317.6729 0007254 205.8198 154.2602 15.71447118 31862 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10221.52208609 = yrday.fracday Element set: 912 Inclination: 51.6465 deg RA of node: 317.6729 deg Eccentricity: .0007254 Arg of perigee: 205.8198 deg Mean anomaly: 154.2602 deg </pre> <p> Mean motion: 15.71447118 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3186 Checksum: 304 </pre> <p> Coasting Arc #14 (Orbit 3201) </p><hr/> <p> Vector Time (GMT): 2010/222/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1062265.70 A = 6733589.46 meter Y = 5542441.95 meter E = .0009896 Z = 3661620.69 I = 51.39600 XDOT = -6153.257976 Wp = 120.96690 YDOT = 1675.330307 meter/sec RA = 312.05045 deg ZDOT = -4317.393796 TA = 14.88559 MA = 14.85648 Ha = 194.405 n.mi Hp = 188.494 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -3485123.70 X = -1141950.41 Y = 18183864.67 feet Y = 5530117.43 meter Z = 12013191.26 Z = 3656266.92 XDOT = -20187.854253 XDOT = -6150.561900 YDOT = 5496.490509 feet/sec YDOT = 1606.536074 meter/sec ZDOT = -14164.677810 ZDOT = -4347.279001 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 14794491.51 X = 4509361.01 Y = -11155113.70 feet Y = -3400078.65 meter Z = 11991757.39 Z = 3655087.65 XDOT = 17817.378026 XDOT = 5430.736822 YDOT = 8262.119505 feet/sec YDOT = 2518.294025 meter/sec ZDOT = -14284.189939 ZDOT = -4353.821094 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10222.53955771 .00016717 00000-0 10270-3 0 9130 2 25544 51.6463 312.4685 0007040 208.9289 151.1483 15.71468869 32020 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10222.53955771 = yrday.fracday Element set: 913 Inclination: 51.6463 deg RA of node: 312.4685 deg Eccentricity: .0007040 Arg of perigee: 208.9289 deg Mean anomaly: 151.1483 deg </pre> <p> Mean motion: 15.71468869 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3202 Checksum: 314 </pre> <p> Coasting Arc #15 (Orbit 3217) </p><hr/> <p> Vector Time (GMT): 2010/223/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 5254637.81 A = 6734882.87 meter Y = -2783503.44 meter E = .0010370 Z = 3160246.31 I = 51.38122 XDOT = 282.273681 Wp = 119.41242 YDOT = 6004.650423 meter/sec RA = 306.96700 deg ZDOT = 4802.618807 TA = 277.50424 MA = 277.62204 Ha = 194.183 n.mi Hp = 188.600 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 17239625.35 X = 5270021.33 Y = -9132229.12 feet Y = -2724656.92 meter Z = 10368262.18 Z = 3185810.18 XDOT = 926.094754 XDOT = 191.777833 YDOT = 19700.296665 feet/sec YDOT = 6007.300989 meter/sec ZDOT = 15756.623382 ZDOT = 4803.770252 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -18960539.28 X = -5779172.37 Y = -4355442.62 feet Y = -1327538.91 meter Z = 10470492.89 Z = 3191406.23 XDOT = 11960.626866 XDOT = 3645.599069 YDOT = -14046.562501 feet/sec YDOT = -4281.392250 meter/sec ZDOT = 15761.210708 ZDOT = 4804.017024 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10223.55701894 .00016717 00000-0 10270-3 0 9149 2 25544 51.6460 307.2632 0007070 213.6446 146.4268 15.71502866 32183 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10223.55701894 = yrday.fracday Element set: 914 Inclination: 51.6460 deg RA of node: 307.2632 deg Eccentricity: .0007070 Arg of perigee: 213.6446 deg Mean anomaly: 146.4268 deg </pre> <p> Mean motion: 15.71502866 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3218 Checksum: 296</pre> <hr/> <p><strong>INTERNATIONAL SPACE STATION ORBITAL DATA:</strong> </p> <p>The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability. The data normally contains past, current and predicted orbital data. Careful attention to the orbit # / epoch times! These sources include: </p><p>NASA Orbital Flight Dynamics<br/> DOD C-Band Radar Network<br/> Goddard Space Flight Center (GSFC)<br/> NASA Johnson Space Center (JSC)<br/> DoD/ USSTRATCOM/ US Space Command with permission </p> <p>By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command. </p><pre> David Cottle Director Of Engineering IDB Communications</pre> <hr/> <p>The following information is a reminder of your current mailing list subscription: </p><p>You are subscribed to the following list: </p><p><strong>[ISSTLE LIST]</strong> </p><p>using the following email: </p><p> <a href="mailto:&#x65;&#120;&#x61;&#109;&#x70;&#108;&#x65;&#64;&#x65;&#120;&#97;&#x6D;&#x70;&#108;&#101;&#46;&#x63;&#111;&#x6D;">&#x65;&#120;&#x61;&#109;&#x70;&#108;&#x65;&#64;&#x65;&#120;&#97;&#x6D;&#x70;&#108;&#101;&#46;&#x63;&#111;&#x6D;</a> </p><p>You may automatically unsubscribe from this list at any time by visiting the following URL: </p><p>&#60;<a href="http://www.aus-city.com/cgi-bin/dada/mail.cgi/u/ISSTLE_LIST/example/example.com/">http://www.aus-city.com/cgi-bin/dada/mail.cgi/u/ISSTLE_LIST/example/example.com/</a>&#62; </p><p>If the above URL is inoperable, make sure that you have copied the entire address. 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subscription_form_widget.tmpl --> [ISSTLE LIST] Current ISS TLEs @ 06:30 UTC tag:www.aus-city.com,2010-07-29:%2Fcgi-bin%2Fdada%2Fmail.cgi%2Farchive%2FISSTLE_LIST%2F20100729164502%2F 2010-07-29T16:45:02Z 2010-07-29T16:45:02Z <p>&#60;B&#62; ISS TRAJECTORY DATA&#60;/B&#62; </p><p> Lift off time (UTC) : N/A<br/> Area (sq ft) : 8880.23<br/> Drag Coefficient (Cd) : 2.00<br/> Monthly MSFC 50% solar flux (F10.7-jansky) : 74.8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0.74 ET - UTC (sec) : 66.18<br/> UT1 - UTC (sec) : 0.00 </p><p> Maneuvers contained within the current ephemeris are as follows: </p><pre> IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP </pre> <hr/> There are no maneuvers. <p> Coasting Arc #1 (Orbit 2996) </p><hr/> <p> Vector Time (GMT): 2010/209/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6516113.77 A = 6739113.74 meter Y = 1075697.33 meter E = .0008112 Z = -1348545.43 I = 51.76930 XDOT = 379.902553 Wp = 90.86388 YDOT = 4984.838824 meter/sec RA = 18.63083 deg ZDOT = 5841.971976 TA = 254.38104 MA = 254.47058 Ha = 196.328 n.mi Hp = 186.522 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 21378326.01 X = 6510151.69 Y = 3529190.72 feet Y = 1148531.16 meter Z = -4424361.65 Z = -1316905.21 XDOT = 1246.399451 XDOT = 295.754282 YDOT = 16354.458084 feet/sec YDOT = 4988.616247 meter/sec ZDOT = 19166.574723 ZDOT = 5843.613434 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -9477785.26 X = -2888828.95 Y = -19513152.93 feet Y = -5947609.01 meter Z = -4297840.79 Z = -1309981.87 XDOT = 11276.028065 XDOT = 3436.933354 YDOT = -9677.510145 feet/sec YDOT = -2949.705092 meter/sec ZDOT = 19173.089367 ZDOT = 5843.957639 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10209.50254265 .00016717 00000-0 10270-3 0 9008 2 25544 51.6420 19.1528 0007751 159.6876 200.4595 15.71301570 29970 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10209.50254265 = yrday.fracday Element set: 900 Inclination: 51.6420 deg RA of node: 19.1528 deg Eccentricity: .0007751 Arg of perigee: 159.6876 deg Mean anomaly: 200.4595 deg </pre> <p> Mean motion: 15.71301570 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 2997 Checksum: 302 </pre> <p> Coasting Arc #2 (Orbit 3012) </p><hr/> <p> Vector Time (GMT): 2010/210/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1774311.45 A = 6729662.15 meter Y = -4349633.23 meter E = .0014282 Z = -4829241.59 I = 51.70945 XDOT = 7278.280118 Wp = 104.82108 YDOT = -245.294757 meter/sec RA = 13.55506 deg ZDOT = -2462.799354 TA = 141.14064 MA = 141.03787 Ha = 196.197 n.mi Hp = 186.505 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -5821231.80 X = -1702082.01 Y = -14270450.24 feet Y = -4369070.55 meter Z = -15843968.46 Z = -4837685.82 XDOT = 23878.871778 XDOT = 7292.445737 YDOT = -804.772825 feet/sec YDOT = -163.825349 meter/sec ZDOT = -8080.050375 ZDOT = -2427.407688 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -8121069.96 X = -2475302.12 Y = 13057981.64 feet Y = 3980072.80 meter Z = -15877693.94 Z = -4839521.11 XDOT = -13846.353559 XDOT = -4220.368565 YDOT = -18225.826072 feet/sec YDOT = -5555.231787 meter/sec ZDOT = -7938.519472 ZDOT = -2419.660735 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10210.52011815 .00016717 00000-0 10270-3 0 9015 2 25544 51.6427 13.9486 0007709 162.3543 197.7888 15.71326345 30137 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10210.52011815 = yrday.fracday Element set: 901 Inclination: 51.6427 deg RA of node: 13.9486 deg Eccentricity: .0007709 Arg of perigee: 162.3543 deg Mean anomaly: 197.7888 deg </pre> <p> Mean motion: 15.71326345 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3013 Checksum: 296 </pre> <p> Coasting Arc #3 (Orbit 3028) </p><hr/> <p> Vector Time (GMT): 2010/211/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5881744.62 A = 6736240.36 meter Y = 1459490.95 meter E = .0017719 Z = 2916437.15 I = 51.70098 XDOT = -3635.167120 Wp = 121.99076 YDOT = -4558.045636 meter/sec RA = 8.40128 deg ZDOT = -5037.219711 TA = 24.46598 MA = 24.38199 Ha = 196.200 n.mi Hp = 186.794 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -19297062.39 X = -5911795.10 Y = 4788356.13 feet Y = 1393549.62 meter Z = 9568363.34 Z = 2887791.09 XDOT = -11926.401311 XDOT = -3559.458478 YDOT = -14954.217967 feet/sec YDOT = -4598.272726 meter/sec ZDOT = -16526.311388 ZDOT = -5054.695412 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15524118.05 X = 4731751.18 Y = 12509434.54 feet Y = 3812875.65 meter Z = 9453801.07 Z = 2881518.56 XDOT = -3835.340678 XDOT = -1169.011839 YDOT = 17334.564542 feet/sec YDOT = 5283.575272 meter/sec ZDOT = -16596.148045 ZDOT = -5058.505924 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10211.53768462 .00016717 00000-0 10270-3 0 9025 2 25544 51.6422 8.7430 0007710 167.4197 192.7159 15.71310320 30295 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10211.53768462 = yrday.fracday Element set: 902 Inclination: 51.6422 deg RA of node: 8.7430 deg Eccentricity: .0007710 Arg of perigee: 167.4197 deg Mean anomaly: 192.7159 deg </pre> <p> Mean motion: 15.71310320 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3029 Checksum: 284 </pre> <p> Coasting Arc #4 (Orbit 3044) </p><hr/> <p> Vector Time (GMT): 2010/212/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4419500.56 A = 6733190.74 meter Y = 3308687.31 meter E = .0015535 Z = 3851289.51 I = 51.66224 XDOT = -5802.149592 Wp = 127.10210 YDOT = 2927.361394 meter/sec RA = 3.33869 deg ZDOT = 4122.665932 TA = 279.73611 MA = 279.91153 Ha = 195.907 n.mi Hp = 186.827 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 14499673.74 X = 4363465.06 Y = 10855273.34 feet Y = 3357795.34 meter Z = 12635464.26 Z = 3872623.26 XDOT = -19035.923857 XDOT = -5854.479622 YDOT = 9604.204047 feet/sec YDOT = 2862.185523 meter/sec ZDOT = 13525.806862 ZDOT = 4094.352376 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -397417.09 X = -121132.73 Y = -18048750.29 feet Y = -5501259.09 meter Z = 12720736.13 Z = 3877280.37 XDOT = 18057.107948 XDOT = 5503.806503 YDOT = 9102.850259 feet/sec YDOT = 2774.548759 meter/sec ZDOT = 13412.564880 ZDOT = 4088.149775 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10212.55524169 .00016717 00000-0 10270-3 0 9033 2 25544 51.6430 3.5383 0007738 171.3522 188.7775 15.71359169 30451 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10212.55524169 = yrday.fracday Element set: 903 Inclination: 51.6430 deg RA of node: 3.5383 deg Eccentricity: .0007738 Arg of perigee: 171.3522 deg Mean anomaly: 188.7775 deg </pre> <p> Mean motion: 15.71359169 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3045 Checksum: 308 </pre> <p> Coasting Arc #5 (Orbit 3059) </p><hr/> <p> Vector Time (GMT): 2010/213/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4010554.86 A = 6732257.00 meter Y = -3442258.01 meter E = .0013189 Z = -4184015.30 I = 51.62949 XDOT = 6175.097768 Wp = 141.00469 YDOT = 2717.752384 meter/sec RA = 358.17383 deg ZDOT = 3679.377107 TA = 166.65207 MA = 166.61715 Ha = 195.878 n.mi Hp = 187.094 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 13157988.39 X = 4069073.80 Y = -11293497.41 feet Y = -3397082.19 meter Z = -13727084.32 Z = -4164390.17 XDOT = 20259.507112 XDOT = 6126.374782 YDOT = 8916.510446 feet/sec YDOT = 2786.533419 meter/sec ZDOT = 12071.447202 ZDOT = 3709.257324 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -17120247.58 X = -5218251.46 Y = -3118003.69 feet Y = -950367.52 meter Z = -13648580.95 Z = -4160087.47 XDOT = -6080.709696 XDOT = -1853.400315 YDOT = -20030.485295 feet/sec YDOT = -6105.291918 meter/sec ZDOT = 12190.892595 ZDOT = 3715.784063 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10213.50919489 .00016717 00000-0 10270-3 0 9043 2 25544 51.6441 358.6595 0007670 174.1104 186.0150 15.71346623 30600 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10213.50919489 = yrday.fracday Element set: 904 Inclination: 51.6441 deg RA of node: 358.6595 deg Eccentricity: .0007670 Arg of perigee: 174.1104 deg Mean anomaly: 186.0150 deg </pre> <p> Mean motion: 15.71346623 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3060 Checksum: 297 </pre> <p> Coasting Arc #6 (Orbit 3075) </p><hr/> <p> Vector Time (GMT): 2010/214/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -6114171.14 A = 6736845.84 meter Y = -1267695.63 meter E = .0011658 Z = -2515463.39 I = 51.61507 XDOT = 3132.189428 Wp = 157.99540 YDOT = -4613.299231 meter/sec RA = 353.10384 deg ZDOT = -5306.794511 TA = 50.47485 MA = 50.37187 Ha = 195.629 n.mi Hp = 187.123 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -20059616.60 X = -6087321.50 Y = -4159106.41 feet Y = -1335917.68 meter Z = -8252832.65 Z = -2545100.77 XDOT = 10276.212035 XDOT = 3209.322730 YDOT = -15135.496166 feet/sec YDOT = -4577.841622 meter/sec ZDOT = -17410.743147 ZDOT = -5291.391319 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 9738019.52 X = 2968148.35 Y = 17969074.85 feet Y = 5476974.01 meter Z = -8371317.45 Z = -2551577.56 XDOT = -16949.907476 XDOT = -5166.331799 YDOT = 1131.101307 feet/sec YDOT = 344.759678 meter/sec ZDOT = -17349.109246 ZDOT = -5288.008498 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10214.52673505 .00016717 00000-0 10270-3 0 9053 2 25544 51.6439 353.4544 0007593 178.1416 181.9766 15.71369601 30763 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10214.52673505 = yrday.fracday Element set: 905 Inclination: 51.6439 deg RA of node: 353.4544 deg Eccentricity: .0007593 Arg of perigee: 178.1416 deg Mean anomaly: 181.9766 deg </pre> <p> Mean motion: 15.71369601 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3076 Checksum: 320 </pre> <p> Coasting Arc #7 (Orbit 3091) </p><hr/> <p> Vector Time (GMT): 2010/215/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1322709.43 A = 6729012.82 meter Y = 4323254.72 meter E = .0006416 Z = 4978522.94 I = 51.55880 XDOT = -7444.497362 Wp = 131.13838 YDOT = -10.479641 meter/sec RA = 347.94741 deg ZDOT = -1971.283858 TA = 337.92325 MA = 337.95087 Ha = 195.679 n.mi Hp = 187.339 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4339597.86 X = -1395139.22 Y = 14183906.55 feet Y = 4308058.03 meter Z = 16333736.67 Z = 4971921.64 XDOT = -24424.203942 XDOT = -7434.250777 YDOT = -34.382024 feet/sec YDOT = -93.671020 meter/sec ZDOT = -6467.466727 ZDOT = -2007.424212 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13596498.05 X = 4144212.61 Y = -6001131.00 feet Y = -1829144.73 meter Z = 16307297.02 Z = 4970464.13 XDOT = 15593.251658 XDOT = 4752.823105 YDOT = 17384.177102 feet/sec YDOT = 5298.697181 meter/sec ZDOT = -6611.962626 ZDOT = -2015.326208 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10215.54426839 .00016717 00000-0 10270-3 0 9063 2 25544 51.6444 348.2500 0007585 181.1250 178.9896 15.71343549 30925 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10215.54426839 = yrday.fracday Element set: 906 Inclination: 51.6444 deg RA of node: 348.2500 deg Eccentricity: .0007585 Arg of perigee: 181.1250 deg Mean anomaly: 178.9896 deg </pre> <p> Mean motion: 15.71343549 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3092 Checksum: 322 </pre> <p> Coasting Arc #8 (Orbit 3107) </p><hr/> <p> Vector Time (GMT): 2010/216/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6554450.82 A = 6739193.01 meter Y = -1276112.99 meter E = .0010474 Z = 898718.08 I = 51.56537 XDOT = 129.990087 Wp = 87.88706 YDOT = 4890.130543 meter/sec RA = 342.85144 deg ZDOT = 5936.504210 TA = 281.91723 MA = 282.03464 Ha = 195.430 n.mi Hp = 187.413 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 21504103.73 X = 6563867.62 Y = -4186722.40 feet Y = -1202764.63 meter Z = 2948550.15 Z = 930582.21 XDOT = 426.476662 XDOT = 46.459769 YDOT = 16043.735376 feet/sec YDOT = 4891.116576 meter/sec ZDOT = 19476.719850 ZDOT = 5936.933259 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -17526971.96 X = -5342221.05 Y = -13114601.60 feet Y = -3997330.57 meter Z = 3075963.04 Z = 937553.54 XDOT = 10726.507000 XDOT = 3269.439334 YDOT = -9723.270816 feet/sec YDOT = -2963.652945 meter/sec ZDOT = 19478.381513 ZDOT = 5937.010685 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10216.56178918 .00016717 00000-0 10270-3 0 9079 2 25544 51.6453 343.0452 0007540 185.6751 174.4326 15.71404114 31083 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10216.56178918 = yrday.fracday Element set: 907 Inclination: 51.6453 deg RA of node: 343.0452 deg Eccentricity: .0007540 Arg of perigee: 185.6751 deg Mean anomaly: 174.4326 deg </pre> <p> Mean motion: 15.71404114 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3108 Checksum: 296 </pre> <p> Coasting Arc #9 (Orbit 3122) </p><hr/> <p> Vector Time (GMT): 2010/217/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1496796.08 A = 6727457.31 meter Y = -3918621.57 meter E = .0015736 Z = -5271540.75 I = 51.49749 XDOT = 7137.823361 Wp = 118.29976 YDOT = -2851.102041 meter/sec RA = 337.71922 deg ZDOT = 85.537640 TA = 152.55661 MA = 152.47341 Ha = 195.219 n.mi Hp = 187.552 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4910748.30 X = -1427258.10 Y = -12856369.98 feet Y = -3934970.27 meter Z = -17295081.20 Z = -5278643.64 XDOT = 23418.055646 XDOT = 7168.758882 YDOT = -9354.009320 feet/sec YDOT = -2771.109672 meter/sec ZDOT = 280.635302 ZDOT = 120.287756 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -6090738.55 X = -1856457.11 Y = 12301339.34 feet Y = 3749448.23 meter Z = -17323437.47 Z = -5280183.74 XDOT = -21942.487771 XDOT = -6688.070273 YDOT = -10240.519835 feet/sec YDOT = -3121.310446 meter/sec ZDOT = 419.606633 ZDOT = 127.896102 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10217.51570882 .00016717 00000-0 10270-3 0 9082 2 25544 51.6454 338.1665 0007393 189.5722 170.5300 15.71425065 31236 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10217.51570882 = yrday.fracday Element set: 908 Inclination: 51.6454 deg RA of node: 338.1665 deg Eccentricity: .0007393 Arg of perigee: 189.5722 deg Mean anomaly: 170.5300 deg </pre> <p> Mean motion: 15.71425065 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3123 Checksum: 302 </pre> <p> Coasting Arc #10 (Orbit 3138) </p><hr/> <p> Vector Time (GMT): 2010/218/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5634666.80 A = 6739330.60 meter Y = 3598580.54 meter E = .0017768 Z = 754981.09 I = 51.50999 XDOT = -3169.172308 Wp = 149.53391 YDOT = -3700.840956 meter/sec RA = 332.58728 deg ZDOT = -5966.615392 TA = 22.22373 MA = 22.14681 Ha = 195.121 n.mi Hp = 187.839 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -18486439.62 X = -5678155.52 Y = 11806366.61 feet Y = 3535327.09 meter Z = 2476972.09 Z = 727502.99 XDOT = -10397.546942 XDOT = -3098.568909 YDOT = -12141.866655 feet/sec YDOT = -3735.885099 meter/sec ZDOT = -19575.509815 ZDOT = -5981.839966 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 21356937.60 X = 6509594.58 Y = 5054933.03 feet Y = 1540743.59 meter Z = 2367065.97 Z = 721481.71 XDOT = -1185.350720 XDOT = -361.294899 YDOT = 14277.199512 feet/sec YDOT = 4351.690411 meter/sec ZDOT = -19636.344463 ZDOT = -5985.157792 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10218.53321460 .00016717 00000-0 10270-3 0 9092 2 25544 51.6456 332.9611 0007446 193.6726 166.4235 15.71412878 31396 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10218.53321460 = yrday.fracday Element set: 909 Inclination: 51.6456 deg RA of node: 332.9611 deg Eccentricity: .0007446 Arg of perigee: 193.6726 deg Mean anomaly: 166.4235 deg </pre> <p> Mean motion: 15.71412878 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3139 Checksum: 312 </pre> <p> Coasting Arc #11 (Orbit 3154) </p><hr/> <p> Vector Time (GMT): 2010/219/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3852425.73 A = 6728364.79 meter Y = 2288407.10 meter E = .0010291 Z = 5020088.82 I = 51.44828 XDOT = -5421.943077 Wp = 167.77085 YDOT = 5157.095545 meter/sec RA = 327.48205 deg ZDOT = 1799.375050 TA = 264.77519 MA = 264.89263 Ha = 194.794 n.mi Hp = 187.945 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12639192.01 X = 3802163.77 Y = 7507897.32 feet Y = 2331205.67 meter Z = 16470107.69 Z = 5038681.74 XDOT = -17788.527156 XDOT = -5487.948576 YDOT = 16919.604806 feet/sec YDOT = 5096.094888 meter/sec ZDOT = 5903.461449 ZDOT = 1772.875937 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -3589803.16 X = -1094172.00 Y = -14169590.19 feet Y = -4318891.09 meter Z = 16544430.22 Z = 5042742.33 XDOT = 23535.064409 XDOT = 7173.487632 YDOT = 846.928604 feet/sec YDOT = 258.143838 meter/sec ZDOT = 5797.453857 ZDOT = 1767.063936 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10219.55070986 .00016717 00000-0 10270-3 0 9101 2 25544 51.6465 327.7563 0007346 198.1419 161.9482 15.71467617 31555 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10219.55070986 = yrday.fracday Element set: 910 Inclination: 51.6465 deg RA of node: 327.7563 deg Eccentricity: .0007346 Arg of perigee: 198.1419 deg Mean anomaly: 161.9482 deg </pre> <p> Mean motion: 15.71467617 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3155 Checksum: 330 </pre> <p> Coasting Arc #12 (Orbit 3169) </p><hr/> <p> Vector Time (GMT): 2010/220/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3639647.56 A = 6737196.89 meter Y = -5166686.31 meter E = .0002833 Z = -2339622.53 I = 51.45268 XDOT = 5326.149311 Wp = 150.86546 YDOT = 1311.796888 meter/sec RA = 322.31817 deg ZDOT = 5389.064192 TA = 182.78157 MA = 182.78315 Ha = 194.744 n.mi Hp = 188.283 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 11941100.90 X = 3708517.09 Y = -16951070.57 feet Y = -5125600.32 meter Z = -7675926.94 Z = -2321774.69 XDOT = 17474.243146 XDOT = 5284.906197 YDOT = 4303.795564 feet/sec YDOT = 1371.126005 meter/sec ZDOT = 17680.656799 ZDOT = 5414.837984 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -20390127.25 X = -6214910.79 Y = 3906734.97 feet Y = 1190772.82 meter Z = -7604516.49 Z = -2317856.63 XDOT = -9248.690870 XDOT = -2819.000977 YDOT = -13656.713544 feet/sec YDOT = -4162.566288 meter/sec ZDOT = 17783.707220 ZDOT = 5420.473961 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10220.50460613 .00016717 00000-0 10270-3 0 9119 2 25544 51.6466 322.8773 0007135 202.3950 157.6901 15.71419937 31706 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10220.50460613 = yrday.fracday Element set: 911 Inclination: 51.6466 deg RA of node: 322.8773 deg Eccentricity: .0007135 Arg of perigee: 202.3950 deg Mean anomaly: 157.6901 deg </pre> <p> Mean motion: 15.71419937 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3170 Checksum: 289 </pre> <p> Coasting Arc #13 (Orbit 3185) </p><hr/> <p> Vector Time (GMT): 2010/221/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5178556.93 A = 6731316.08 meter Y = 114342.49 meter E = .0006174 Z = -4301250.23 I = 51.41004 XDOT = 2735.329701 Wp = 123.11274 YDOT = -6299.404364 meter/sec RA = 317.23280 deg ZDOT = -3467.612429 TA = 111.70513 MA = 111.63939 Ha = 194.517 n.mi Hp = 188.270 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -16990016.16 X = -5158556.47 Y = 375139.40 feet Y = 56544.84 meter Z = -14111713.37 Z = -4326358.45 XDOT = 8974.178808 XDOT = 2822.412108 YDOT = -20667.337152 feet/sec YDOT = -6268.329171 meter/sec ZDOT = -11376.681196 ZDOT = -3454.113368 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 12638795.32 X = 3852304.81 Y = 11234697.99 feet Y = 3424335.95 meter Z = -14212116.20 Z = -4331853.02 XDOT = -19873.487666 XDOT = -6057.439041 YDOT = 8062.331633 feet/sec YDOT = 2457.398682 meter/sec ZDOT = -11322.660776 ZDOT = -3451.147004 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10221.52208609 .00016717 00000-0 10270-3 0 9128 2 25544 51.6465 317.6729 0007254 205.8198 154.2602 15.71447118 31862 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10221.52208609 = yrday.fracday Element set: 912 Inclination: 51.6465 deg RA of node: 317.6729 deg Eccentricity: .0007254 Arg of perigee: 205.8198 deg Mean anomaly: 154.2602 deg </pre> <p> Mean motion: 15.71447118 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3186 Checksum: 304 </pre> <p> Coasting Arc #14 (Orbit 3201) </p><hr/> <p> Vector Time (GMT): 2010/222/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1062265.70 A = 6733589.46 meter Y = 5542441.95 meter E = .0009896 Z = 3661620.69 I = 51.39600 XDOT = -6153.257976 Wp = 120.96690 YDOT = 1675.330307 meter/sec RA = 312.05045 deg ZDOT = -4317.393796 TA = 14.88559 MA = 14.85648 Ha = 194.405 n.mi Hp = 188.494 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -3485123.70 X = -1141950.41 Y = 18183864.67 feet Y = 5530117.43 meter Z = 12013191.26 Z = 3656266.92 XDOT = -20187.854253 XDOT = -6150.561900 YDOT = 5496.490509 feet/sec YDOT = 1606.536074 meter/sec ZDOT = -14164.677810 ZDOT = -4347.279001 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 14794491.51 X = 4509361.01 Y = -11155113.70 feet Y = -3400078.65 meter Z = 11991757.39 Z = 3655087.65 XDOT = 17817.378026 XDOT = 5430.736822 YDOT = 8262.119505 feet/sec YDOT = 2518.294025 meter/sec ZDOT = -14284.189939 ZDOT = -4353.821094 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10222.53955771 .00016717 00000-0 10270-3 0 9130 2 25544 51.6463 312.4685 0007040 208.9289 151.1483 15.71468869 32020 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10222.53955771 = yrday.fracday Element set: 913 Inclination: 51.6463 deg RA of node: 312.4685 deg Eccentricity: .0007040 Arg of perigee: 208.9289 deg Mean anomaly: 151.1483 deg </pre> <p> Mean motion: 15.71468869 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3202 Checksum: 314 </pre> <p> Coasting Arc #15 (Orbit 3217) </p><hr/> <p> Vector Time (GMT): 2010/223/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 5254637.81 A = 6734882.87 meter Y = -2783503.44 meter E = .0010370 Z = 3160246.31 I = 51.38122 XDOT = 282.273681 Wp = 119.41242 YDOT = 6004.650423 meter/sec RA = 306.96700 deg ZDOT = 4802.618807 TA = 277.50424 MA = 277.62204 Ha = 194.183 n.mi Hp = 188.600 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 17239625.35 X = 5270021.33 Y = -9132229.12 feet Y = -2724656.92 meter Z = 10368262.18 Z = 3185810.18 XDOT = 926.094754 XDOT = 191.777833 YDOT = 19700.296665 feet/sec YDOT = 6007.300989 meter/sec ZDOT = 15756.623382 ZDOT = 4803.770252 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -18960539.28 X = -5779172.37 Y = -4355442.62 feet Y = -1327538.91 meter Z = 10470492.89 Z = 3191406.23 XDOT = 11960.626866 XDOT = 3645.599069 YDOT = -14046.562501 feet/sec YDOT = -4281.392250 meter/sec ZDOT = 15761.210708 ZDOT = 4804.017024 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10223.55701894 .00016717 00000-0 10270-3 0 9149 2 25544 51.6460 307.2632 0007070 213.6446 146.4268 15.71502866 32183 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10223.55701894 = yrday.fracday Element set: 914 Inclination: 51.6460 deg RA of node: 307.2632 deg Eccentricity: .0007070 Arg of perigee: 213.6446 deg Mean anomaly: 146.4268 deg </pre> <p> Mean motion: 15.71502866 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3218 Checksum: 296</pre> <hr/> <p><strong>INTERNATIONAL SPACE STATION ORBITAL DATA:</strong> </p> <p>The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability. The data normally contains past, current and predicted orbital data. Careful attention to the orbit # / epoch times! These sources include: </p><p>NASA Orbital Flight Dynamics<br/> DOD C-Band Radar Network<br/> Goddard Space Flight Center (GSFC)<br/> NASA Johnson Space Center (JSC)<br/> DoD/ USSTRATCOM/ US Space Command with permission </p> <p>By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command. </p><pre> David Cottle Director Of Engineering IDB Communications</pre> <hr/> <p>The following information is a reminder of your current mailing list subscription: </p><p>You are subscribed to the following list: </p><p><strong>[ISSTLE LIST]</strong> </p><p>using the following email: </p><p> <a href="mailto:&#101;&#x78;&#97;&#109;&#112;&#x6C;&#x65;&#x40;&#x65;&#x78;&#97;&#109;&#x70;&#108;&#x65;&#46;&#99;&#111;&#x6D;">&#101;&#x78;&#97;&#109;&#112;&#x6C;&#x65;&#x40;&#x65;&#x78;&#97;&#109;&#x70;&#108;&#x65;&#46;&#99;&#111;&#x6D;</a> </p><p>You may automatically unsubscribe from this list at any time by visiting the following URL: </p><p>&#60;<a href="http://www.aus-city.com/cgi-bin/dada/mail.cgi/u/ISSTLE_LIST/example/example.com/">http://www.aus-city.com/cgi-bin/dada/mail.cgi/u/ISSTLE_LIST/example/example.com/</a>&#62; </p><p>If the above URL is inoperable, make sure that you have copied the entire address. 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subscription_form_widget.tmpl --> [ISSTLE LIST] Current ISS TLEs @ 18:30 UTC tag:www.aus-city.com,2010-07-29:%2Fcgi-bin%2Fdada%2Fmail.cgi%2Farchive%2FISSTLE_LIST%2F20100729044502%2F 2010-07-29T04:45:02Z 2010-07-29T04:45:02Z <p>&#60;B&#62; ISS TRAJECTORY DATA&#60;/B&#62; </p><p> Lift off time (UTC) : N/A<br/> Area (sq ft) : 8880.23<br/> Drag Coefficient (Cd) : 2.00<br/> Monthly MSFC 50% solar flux (F10.7-jansky) : 74.8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0.74 ET - UTC (sec) : 66.18<br/> UT1 - UTC (sec) : 0.00 </p><p> Maneuvers contained within the current ephemeris are as follows: </p><pre> IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP </pre> <hr/> There are no maneuvers. <p> Coasting Arc #1 (Orbit 2996) </p><hr/> <p> Vector Time (GMT): 2010/209/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6516113.77 A = 6739113.74 meter Y = 1075697.33 meter E = .0008112 Z = -1348545.43 I = 51.76930 XDOT = 379.902553 Wp = 90.86388 YDOT = 4984.838824 meter/sec RA = 18.63083 deg ZDOT = 5841.971976 TA = 254.38104 MA = 254.47058 Ha = 196.328 n.mi Hp = 186.522 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 21378326.01 X = 6510151.69 Y = 3529190.72 feet Y = 1148531.16 meter Z = -4424361.65 Z = -1316905.21 XDOT = 1246.399451 XDOT = 295.754282 YDOT = 16354.458084 feet/sec YDOT = 4988.616247 meter/sec ZDOT = 19166.574723 ZDOT = 5843.613434 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -9477785.26 X = -2888828.95 Y = -19513152.93 feet Y = -5947609.01 meter Z = -4297840.79 Z = -1309981.87 XDOT = 11276.028065 XDOT = 3436.933354 YDOT = -9677.510145 feet/sec YDOT = -2949.705092 meter/sec ZDOT = 19173.089367 ZDOT = 5843.957639 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10209.50254265 .00016717 00000-0 10270-3 0 9008 2 25544 51.6420 19.1528 0007751 159.6876 200.4595 15.71301570 29970 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10209.50254265 = yrday.fracday Element set: 900 Inclination: 51.6420 deg RA of node: 19.1528 deg Eccentricity: .0007751 Arg of perigee: 159.6876 deg Mean anomaly: 200.4595 deg </pre> <p> Mean motion: 15.71301570 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 2997 Checksum: 302 </pre> <p> Coasting Arc #2 (Orbit 3012) </p><hr/> <p> Vector Time (GMT): 2010/210/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1774311.45 A = 6729662.15 meter Y = -4349633.23 meter E = .0014282 Z = -4829241.59 I = 51.70945 XDOT = 7278.280118 Wp = 104.82108 YDOT = -245.294757 meter/sec RA = 13.55506 deg ZDOT = -2462.799354 TA = 141.14064 MA = 141.03787 Ha = 196.197 n.mi Hp = 186.505 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -5821231.80 X = -1702082.01 Y = -14270450.24 feet Y = -4369070.55 meter Z = -15843968.46 Z = -4837685.82 XDOT = 23878.871778 XDOT = 7292.445737 YDOT = -804.772825 feet/sec YDOT = -163.825349 meter/sec ZDOT = -8080.050375 ZDOT = -2427.407688 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -8121069.96 X = -2475302.12 Y = 13057981.64 feet Y = 3980072.80 meter Z = -15877693.94 Z = -4839521.11 XDOT = -13846.353559 XDOT = -4220.368565 YDOT = -18225.826072 feet/sec YDOT = -5555.231787 meter/sec ZDOT = -7938.519472 ZDOT = -2419.660735 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10210.52011815 .00016717 00000-0 10270-3 0 9015 2 25544 51.6427 13.9486 0007709 162.3543 197.7888 15.71326345 30137 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10210.52011815 = yrday.fracday Element set: 901 Inclination: 51.6427 deg RA of node: 13.9486 deg Eccentricity: .0007709 Arg of perigee: 162.3543 deg Mean anomaly: 197.7888 deg </pre> <p> Mean motion: 15.71326345 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3013 Checksum: 296 </pre> <p> Coasting Arc #3 (Orbit 3028) </p><hr/> <p> Vector Time (GMT): 2010/211/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5881744.62 A = 6736240.36 meter Y = 1459490.95 meter E = .0017719 Z = 2916437.15 I = 51.70098 XDOT = -3635.167120 Wp = 121.99076 YDOT = -4558.045636 meter/sec RA = 8.40128 deg ZDOT = -5037.219711 TA = 24.46598 MA = 24.38199 Ha = 196.200 n.mi Hp = 186.794 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -19297062.39 X = -5911795.10 Y = 4788356.13 feet Y = 1393549.62 meter Z = 9568363.34 Z = 2887791.09 XDOT = -11926.401311 XDOT = -3559.458478 YDOT = -14954.217967 feet/sec YDOT = -4598.272726 meter/sec ZDOT = -16526.311388 ZDOT = -5054.695412 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15524118.05 X = 4731751.18 Y = 12509434.54 feet Y = 3812875.65 meter Z = 9453801.07 Z = 2881518.56 XDOT = -3835.340678 XDOT = -1169.011839 YDOT = 17334.564542 feet/sec YDOT = 5283.575272 meter/sec ZDOT = -16596.148045 ZDOT = -5058.505924 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10211.53768462 .00016717 00000-0 10270-3 0 9025 2 25544 51.6422 8.7430 0007710 167.4197 192.7159 15.71310320 30295 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10211.53768462 = yrday.fracday Element set: 902 Inclination: 51.6422 deg RA of node: 8.7430 deg Eccentricity: .0007710 Arg of perigee: 167.4197 deg Mean anomaly: 192.7159 deg </pre> <p> Mean motion: 15.71310320 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3029 Checksum: 284 </pre> <p> Coasting Arc #4 (Orbit 3044) </p><hr/> <p> Vector Time (GMT): 2010/212/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4419500.56 A = 6733190.74 meter Y = 3308687.31 meter E = .0015535 Z = 3851289.51 I = 51.66224 XDOT = -5802.149592 Wp = 127.10210 YDOT = 2927.361394 meter/sec RA = 3.33869 deg ZDOT = 4122.665932 TA = 279.73611 MA = 279.91153 Ha = 195.907 n.mi Hp = 186.827 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 14499673.74 X = 4363465.06 Y = 10855273.34 feet Y = 3357795.34 meter Z = 12635464.26 Z = 3872623.26 XDOT = -19035.923857 XDOT = -5854.479622 YDOT = 9604.204047 feet/sec YDOT = 2862.185523 meter/sec ZDOT = 13525.806862 ZDOT = 4094.352376 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -397417.09 X = -121132.73 Y = -18048750.29 feet Y = -5501259.09 meter Z = 12720736.13 Z = 3877280.37 XDOT = 18057.107948 XDOT = 5503.806503 YDOT = 9102.850259 feet/sec YDOT = 2774.548759 meter/sec ZDOT = 13412.564880 ZDOT = 4088.149775 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10212.55524169 .00016717 00000-0 10270-3 0 9033 2 25544 51.6430 3.5383 0007738 171.3522 188.7775 15.71359169 30451 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10212.55524169 = yrday.fracday Element set: 903 Inclination: 51.6430 deg RA of node: 3.5383 deg Eccentricity: .0007738 Arg of perigee: 171.3522 deg Mean anomaly: 188.7775 deg </pre> <p> Mean motion: 15.71359169 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3045 Checksum: 308 </pre> <p> Coasting Arc #5 (Orbit 3059) </p><hr/> <p> Vector Time (GMT): 2010/213/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4010554.86 A = 6732257.00 meter Y = -3442258.01 meter E = .0013189 Z = -4184015.30 I = 51.62949 XDOT = 6175.097768 Wp = 141.00469 YDOT = 2717.752384 meter/sec RA = 358.17383 deg ZDOT = 3679.377107 TA = 166.65207 MA = 166.61715 Ha = 195.878 n.mi Hp = 187.094 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 13157988.39 X = 4069073.80 Y = -11293497.41 feet Y = -3397082.19 meter Z = -13727084.32 Z = -4164390.17 XDOT = 20259.507112 XDOT = 6126.374782 YDOT = 8916.510446 feet/sec YDOT = 2786.533419 meter/sec ZDOT = 12071.447202 ZDOT = 3709.257324 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -17120247.58 X = -5218251.46 Y = -3118003.69 feet Y = -950367.52 meter Z = -13648580.95 Z = -4160087.47 XDOT = -6080.709696 XDOT = -1853.400315 YDOT = -20030.485295 feet/sec YDOT = -6105.291918 meter/sec ZDOT = 12190.892595 ZDOT = 3715.784063 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10213.50919489 .00016717 00000-0 10270-3 0 9043 2 25544 51.6441 358.6595 0007670 174.1104 186.0150 15.71346623 30600 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10213.50919489 = yrday.fracday Element set: 904 Inclination: 51.6441 deg RA of node: 358.6595 deg Eccentricity: .0007670 Arg of perigee: 174.1104 deg Mean anomaly: 186.0150 deg </pre> <p> Mean motion: 15.71346623 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3060 Checksum: 297 </pre> <p> Coasting Arc #6 (Orbit 3075) </p><hr/> <p> Vector Time (GMT): 2010/214/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -6114171.14 A = 6736845.84 meter Y = -1267695.63 meter E = .0011658 Z = -2515463.39 I = 51.61507 XDOT = 3132.189428 Wp = 157.99540 YDOT = -4613.299231 meter/sec RA = 353.10384 deg ZDOT = -5306.794511 TA = 50.47485 MA = 50.37187 Ha = 195.629 n.mi Hp = 187.123 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -20059616.60 X = -6087321.50 Y = -4159106.41 feet Y = -1335917.68 meter Z = -8252832.65 Z = -2545100.77 XDOT = 10276.212035 XDOT = 3209.322730 YDOT = -15135.496166 feet/sec YDOT = -4577.841622 meter/sec ZDOT = -17410.743147 ZDOT = -5291.391319 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 9738019.52 X = 2968148.35 Y = 17969074.85 feet Y = 5476974.01 meter Z = -8371317.45 Z = -2551577.56 XDOT = -16949.907476 XDOT = -5166.331799 YDOT = 1131.101307 feet/sec YDOT = 344.759678 meter/sec ZDOT = -17349.109246 ZDOT = -5288.008498 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10214.52673505 .00016717 00000-0 10270-3 0 9053 2 25544 51.6439 353.4544 0007593 178.1416 181.9766 15.71369601 30763 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10214.52673505 = yrday.fracday Element set: 905 Inclination: 51.6439 deg RA of node: 353.4544 deg Eccentricity: .0007593 Arg of perigee: 178.1416 deg Mean anomaly: 181.9766 deg </pre> <p> Mean motion: 15.71369601 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3076 Checksum: 320 </pre> <p> Coasting Arc #7 (Orbit 3091) </p><hr/> <p> Vector Time (GMT): 2010/215/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1322709.43 A = 6729012.82 meter Y = 4323254.72 meter E = .0006416 Z = 4978522.94 I = 51.55880 XDOT = -7444.497362 Wp = 131.13838 YDOT = -10.479641 meter/sec RA = 347.94741 deg ZDOT = -1971.283858 TA = 337.92325 MA = 337.95087 Ha = 195.679 n.mi Hp = 187.339 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4339597.86 X = -1395139.22 Y = 14183906.55 feet Y = 4308058.03 meter Z = 16333736.67 Z = 4971921.64 XDOT = -24424.203942 XDOT = -7434.250777 YDOT = -34.382024 feet/sec YDOT = -93.671020 meter/sec ZDOT = -6467.466727 ZDOT = -2007.424212 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13596498.05 X = 4144212.61 Y = -6001131.00 feet Y = -1829144.73 meter Z = 16307297.02 Z = 4970464.13 XDOT = 15593.251658 XDOT = 4752.823105 YDOT = 17384.177102 feet/sec YDOT = 5298.697181 meter/sec ZDOT = -6611.962626 ZDOT = -2015.326208 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10215.54426839 .00016717 00000-0 10270-3 0 9063 2 25544 51.6444 348.2500 0007585 181.1250 178.9896 15.71343549 30925 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10215.54426839 = yrday.fracday Element set: 906 Inclination: 51.6444 deg RA of node: 348.2500 deg Eccentricity: .0007585 Arg of perigee: 181.1250 deg Mean anomaly: 178.9896 deg </pre> <p> Mean motion: 15.71343549 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3092 Checksum: 322 </pre> <p> Coasting Arc #8 (Orbit 3107) </p><hr/> <p> Vector Time (GMT): 2010/216/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6554450.82 A = 6739193.01 meter Y = -1276112.99 meter E = .0010474 Z = 898718.08 I = 51.56537 XDOT = 129.990087 Wp = 87.88706 YDOT = 4890.130543 meter/sec RA = 342.85144 deg ZDOT = 5936.504210 TA = 281.91723 MA = 282.03464 Ha = 195.430 n.mi Hp = 187.413 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 21504103.73 X = 6563867.62 Y = -4186722.40 feet Y = -1202764.63 meter Z = 2948550.15 Z = 930582.21 XDOT = 426.476662 XDOT = 46.459769 YDOT = 16043.735376 feet/sec YDOT = 4891.116576 meter/sec ZDOT = 19476.719850 ZDOT = 5936.933259 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -17526971.96 X = -5342221.05 Y = -13114601.60 feet Y = -3997330.57 meter Z = 3075963.04 Z = 937553.54 XDOT = 10726.507000 XDOT = 3269.439334 YDOT = -9723.270816 feet/sec YDOT = -2963.652945 meter/sec ZDOT = 19478.381513 ZDOT = 5937.010685 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10216.56178918 .00016717 00000-0 10270-3 0 9079 2 25544 51.6453 343.0452 0007540 185.6751 174.4326 15.71404114 31083 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10216.56178918 = yrday.fracday Element set: 907 Inclination: 51.6453 deg RA of node: 343.0452 deg Eccentricity: .0007540 Arg of perigee: 185.6751 deg Mean anomaly: 174.4326 deg </pre> <p> Mean motion: 15.71404114 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3108 Checksum: 296 </pre> <p> Coasting Arc #9 (Orbit 3122) </p><hr/> <p> Vector Time (GMT): 2010/217/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1496796.08 A = 6727457.31 meter Y = -3918621.57 meter E = .0015736 Z = -5271540.75 I = 51.49749 XDOT = 7137.823361 Wp = 118.29976 YDOT = -2851.102041 meter/sec RA = 337.71922 deg ZDOT = 85.537640 TA = 152.55661 MA = 152.47341 Ha = 195.219 n.mi Hp = 187.552 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4910748.30 X = -1427258.10 Y = -12856369.98 feet Y = -3934970.27 meter Z = -17295081.20 Z = -5278643.64 XDOT = 23418.055646 XDOT = 7168.758882 YDOT = -9354.009320 feet/sec YDOT = -2771.109672 meter/sec ZDOT = 280.635302 ZDOT = 120.287756 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -6090738.55 X = -1856457.11 Y = 12301339.34 feet Y = 3749448.23 meter Z = -17323437.47 Z = -5280183.74 XDOT = -21942.487771 XDOT = -6688.070273 YDOT = -10240.519835 feet/sec YDOT = -3121.310446 meter/sec ZDOT = 419.606633 ZDOT = 127.896102 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10217.51570882 .00016717 00000-0 10270-3 0 9082 2 25544 51.6454 338.1665 0007393 189.5722 170.5300 15.71425065 31236 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10217.51570882 = yrday.fracday Element set: 908 Inclination: 51.6454 deg RA of node: 338.1665 deg Eccentricity: .0007393 Arg of perigee: 189.5722 deg Mean anomaly: 170.5300 deg </pre> <p> Mean motion: 15.71425065 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3123 Checksum: 302 </pre> <p> Coasting Arc #10 (Orbit 3138) </p><hr/> <p> Vector Time (GMT): 2010/218/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5634666.80 A = 6739330.60 meter Y = 3598580.54 meter E = .0017768 Z = 754981.09 I = 51.50999 XDOT = -3169.172308 Wp = 149.53391 YDOT = -3700.840956 meter/sec RA = 332.58728 deg ZDOT = -5966.615392 TA = 22.22373 MA = 22.14681 Ha = 195.121 n.mi Hp = 187.839 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -18486439.62 X = -5678155.52 Y = 11806366.61 feet Y = 3535327.09 meter Z = 2476972.09 Z = 727502.99 XDOT = -10397.546942 XDOT = -3098.568909 YDOT = -12141.866655 feet/sec YDOT = -3735.885099 meter/sec ZDOT = -19575.509815 ZDOT = -5981.839966 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 21356937.60 X = 6509594.58 Y = 5054933.03 feet Y = 1540743.59 meter Z = 2367065.97 Z = 721481.71 XDOT = -1185.350720 XDOT = -361.294899 YDOT = 14277.199512 feet/sec YDOT = 4351.690411 meter/sec ZDOT = -19636.344463 ZDOT = -5985.157792 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10218.53321460 .00016717 00000-0 10270-3 0 9092 2 25544 51.6456 332.9611 0007446 193.6726 166.4235 15.71412878 31396 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10218.53321460 = yrday.fracday Element set: 909 Inclination: 51.6456 deg RA of node: 332.9611 deg Eccentricity: .0007446 Arg of perigee: 193.6726 deg Mean anomaly: 166.4235 deg </pre> <p> Mean motion: 15.71412878 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3139 Checksum: 312 </pre> <p> Coasting Arc #11 (Orbit 3154) </p><hr/> <p> Vector Time (GMT): 2010/219/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3852425.73 A = 6728364.79 meter Y = 2288407.10 meter E = .0010291 Z = 5020088.82 I = 51.44828 XDOT = -5421.943077 Wp = 167.77085 YDOT = 5157.095545 meter/sec RA = 327.48205 deg ZDOT = 1799.375050 TA = 264.77519 MA = 264.89263 Ha = 194.794 n.mi Hp = 187.945 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12639192.01 X = 3802163.77 Y = 7507897.32 feet Y = 2331205.67 meter Z = 16470107.69 Z = 5038681.74 XDOT = -17788.527156 XDOT = -5487.948576 YDOT = 16919.604806 feet/sec YDOT = 5096.094888 meter/sec ZDOT = 5903.461449 ZDOT = 1772.875937 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -3589803.16 X = -1094172.00 Y = -14169590.19 feet Y = -4318891.09 meter Z = 16544430.22 Z = 5042742.33 XDOT = 23535.064409 XDOT = 7173.487632 YDOT = 846.928604 feet/sec YDOT = 258.143838 meter/sec ZDOT = 5797.453857 ZDOT = 1767.063936 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10219.55070986 .00016717 00000-0 10270-3 0 9101 2 25544 51.6465 327.7563 0007346 198.1419 161.9482 15.71467617 31555 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10219.55070986 = yrday.fracday Element set: 910 Inclination: 51.6465 deg RA of node: 327.7563 deg Eccentricity: .0007346 Arg of perigee: 198.1419 deg Mean anomaly: 161.9482 deg </pre> <p> Mean motion: 15.71467617 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3155 Checksum: 330 </pre> <p> Coasting Arc #12 (Orbit 3169) </p><hr/> <p> Vector Time (GMT): 2010/220/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3639647.56 A = 6737196.89 meter Y = -5166686.31 meter E = .0002833 Z = -2339622.53 I = 51.45268 XDOT = 5326.149311 Wp = 150.86546 YDOT = 1311.796888 meter/sec RA = 322.31817 deg ZDOT = 5389.064192 TA = 182.78157 MA = 182.78315 Ha = 194.744 n.mi Hp = 188.283 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 11941100.90 X = 3708517.09 Y = -16951070.57 feet Y = -5125600.32 meter Z = -7675926.94 Z = -2321774.69 XDOT = 17474.243146 XDOT = 5284.906197 YDOT = 4303.795564 feet/sec YDOT = 1371.126005 meter/sec ZDOT = 17680.656799 ZDOT = 5414.837984 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -20390127.25 X = -6214910.79 Y = 3906734.97 feet Y = 1190772.82 meter Z = -7604516.49 Z = -2317856.63 XDOT = -9248.690870 XDOT = -2819.000977 YDOT = -13656.713544 feet/sec YDOT = -4162.566288 meter/sec ZDOT = 17783.707220 ZDOT = 5420.473961 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10220.50460613 .00016717 00000-0 10270-3 0 9119 2 25544 51.6466 322.8773 0007135 202.3950 157.6901 15.71419937 31706 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10220.50460613 = yrday.fracday Element set: 911 Inclination: 51.6466 deg RA of node: 322.8773 deg Eccentricity: .0007135 Arg of perigee: 202.3950 deg Mean anomaly: 157.6901 deg </pre> <p> Mean motion: 15.71419937 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3170 Checksum: 289 </pre> <p> Coasting Arc #13 (Orbit 3185) </p><hr/> <p> Vector Time (GMT): 2010/221/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5178556.93 A = 6731316.08 meter Y = 114342.49 meter E = .0006174 Z = -4301250.23 I = 51.41004 XDOT = 2735.329701 Wp = 123.11274 YDOT = -6299.404364 meter/sec RA = 317.23280 deg ZDOT = -3467.612429 TA = 111.70513 MA = 111.63939 Ha = 194.517 n.mi Hp = 188.270 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -16990016.16 X = -5158556.47 Y = 375139.40 feet Y = 56544.84 meter Z = -14111713.37 Z = -4326358.45 XDOT = 8974.178808 XDOT = 2822.412108 YDOT = -20667.337152 feet/sec YDOT = -6268.329171 meter/sec ZDOT = -11376.681196 ZDOT = -3454.113368 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 12638795.32 X = 3852304.81 Y = 11234697.99 feet Y = 3424335.95 meter Z = -14212116.20 Z = -4331853.02 XDOT = -19873.487666 XDOT = -6057.439041 YDOT = 8062.331633 feet/sec YDOT = 2457.398682 meter/sec ZDOT = -11322.660776 ZDOT = -3451.147004 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10221.52208609 .00016717 00000-0 10270-3 0 9128 2 25544 51.6465 317.6729 0007254 205.8198 154.2602 15.71447118 31862 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10221.52208609 = yrday.fracday Element set: 912 Inclination: 51.6465 deg RA of node: 317.6729 deg Eccentricity: .0007254 Arg of perigee: 205.8198 deg Mean anomaly: 154.2602 deg </pre> <p> Mean motion: 15.71447118 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3186 Checksum: 304 </pre> <p> Coasting Arc #14 (Orbit 3201) </p><hr/> <p> Vector Time (GMT): 2010/222/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1062265.70 A = 6733589.46 meter Y = 5542441.95 meter E = .0009896 Z = 3661620.69 I = 51.39600 XDOT = -6153.257976 Wp = 120.96690 YDOT = 1675.330307 meter/sec RA = 312.05045 deg ZDOT = -4317.393796 TA = 14.88559 MA = 14.85648 Ha = 194.405 n.mi Hp = 188.494 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -3485123.70 X = -1141950.41 Y = 18183864.67 feet Y = 5530117.43 meter Z = 12013191.26 Z = 3656266.92 XDOT = -20187.854253 XDOT = -6150.561900 YDOT = 5496.490509 feet/sec YDOT = 1606.536074 meter/sec ZDOT = -14164.677810 ZDOT = -4347.279001 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 14794491.51 X = 4509361.01 Y = -11155113.70 feet Y = -3400078.65 meter Z = 11991757.39 Z = 3655087.65 XDOT = 17817.378026 XDOT = 5430.736822 YDOT = 8262.119505 feet/sec YDOT = 2518.294025 meter/sec ZDOT = -14284.189939 ZDOT = -4353.821094 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10222.53955771 .00016717 00000-0 10270-3 0 9130 2 25544 51.6463 312.4685 0007040 208.9289 151.1483 15.71468869 32020 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10222.53955771 = yrday.fracday Element set: 913 Inclination: 51.6463 deg RA of node: 312.4685 deg Eccentricity: .0007040 Arg of perigee: 208.9289 deg Mean anomaly: 151.1483 deg </pre> <p> Mean motion: 15.71468869 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3202 Checksum: 314 </pre> <p> Coasting Arc #15 (Orbit 3217) </p><hr/> <p> Vector Time (GMT): 2010/223/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 5254637.81 A = 6734882.87 meter Y = -2783503.44 meter E = .0010370 Z = 3160246.31 I = 51.38122 XDOT = 282.273681 Wp = 119.41242 YDOT = 6004.650423 meter/sec RA = 306.96700 deg ZDOT = 4802.618807 TA = 277.50424 MA = 277.62204 Ha = 194.183 n.mi Hp = 188.600 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 17239625.35 X = 5270021.33 Y = -9132229.12 feet Y = -2724656.92 meter Z = 10368262.18 Z = 3185810.18 XDOT = 926.094754 XDOT = 191.777833 YDOT = 19700.296665 feet/sec YDOT = 6007.300989 meter/sec ZDOT = 15756.623382 ZDOT = 4803.770252 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -18960539.28 X = -5779172.37 Y = -4355442.62 feet Y = -1327538.91 meter Z = 10470492.89 Z = 3191406.23 XDOT = 11960.626866 XDOT = 3645.599069 YDOT = -14046.562501 feet/sec YDOT = -4281.392250 meter/sec ZDOT = 15761.210708 ZDOT = 4804.017024 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10223.55701894 .00016717 00000-0 10270-3 0 9149 2 25544 51.6460 307.2632 0007070 213.6446 146.4268 15.71502866 32183 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10223.55701894 = yrday.fracday Element set: 914 Inclination: 51.6460 deg RA of node: 307.2632 deg Eccentricity: .0007070 Arg of perigee: 213.6446 deg Mean anomaly: 146.4268 deg </pre> <p> Mean motion: 15.71502866 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3218 Checksum: 296</pre> <hr/> <p><strong>INTERNATIONAL SPACE STATION ORBITAL DATA:</strong> </p> <p>The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability. The data normally contains past, current and predicted orbital data. Careful attention to the orbit # / epoch times! These sources include: </p><p>NASA Orbital Flight Dynamics<br/> DOD C-Band Radar Network<br/> Goddard Space Flight Center (GSFC)<br/> NASA Johnson Space Center (JSC)<br/> DoD/ USSTRATCOM/ US Space Command with permission </p> <p>By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command. </p><pre> David Cottle Director Of Engineering IDB Communications</pre> <hr/> <p>The following information is a reminder of your current mailing list subscription: </p><p>You are subscribed to the following list: </p><p><strong>[ISSTLE LIST]</strong> </p><p>using the following email: </p><p> <a href="mailto:&#101;&#120;&#x61;&#109;&#x70;&#108;&#101;&#x40;&#101;&#120;&#97;&#x6D;&#x70;&#x6C;&#x65;&#x2E;&#x63;&#111;&#x6D;">&#101;&#120;&#x61;&#109;&#x70;&#108;&#101;&#x40;&#101;&#120;&#97;&#x6D;&#x70;&#x6C;&#x65;&#x2E;&#x63;&#111;&#x6D;</a> </p><p>You may automatically unsubscribe from this list at any time by visiting the following URL: </p><p>&#60;<a href="http://www.aus-city.com/cgi-bin/dada/mail.cgi/u/ISSTLE_LIST/example/example.com/">http://www.aus-city.com/cgi-bin/dada/mail.cgi/u/ISSTLE_LIST/example/example.com/</a>&#62; </p><p>If the above URL is inoperable, make sure that you have copied the entire address. 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subscription_form_widget.tmpl --> [ISSTLE LIST] Current ISS TLEs @ 06:30 UTC tag:www.aus-city.com,2010-07-28:%2Fcgi-bin%2Fdada%2Fmail.cgi%2Farchive%2FISSTLE_LIST%2F20100728164502%2F 2010-07-28T16:45:02Z 2010-07-28T16:45:02Z <p>&#60;B&#62; ISS TRAJECTORY DATA&#60;/B&#62; </p><p> Lift off time (UTC) : N/A<br/> Area (sq ft) : 8880.23<br/> Drag Coefficient (Cd) : 2.00<br/> Monthly MSFC 50% solar flux (F10.7-jansky) : 74.8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0.74 ET - UTC (sec) : 66.18<br/> UT1 - UTC (sec) : 0.00 </p><p> Maneuvers contained within the current ephemeris are as follows: </p><pre> IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP </pre> <hr/> There are no maneuvers. <p> Coasting Arc #1 (Orbit 2979) </p><hr/> <p> Vector Time (GMT): 2010/208/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5593976.34 A = 6734057.59 meter Y = 646179.01 meter E = .0015774 Z = 3675431.36 I = 51.78783 XDOT = -3477.261292 Wp = 109.99564 YDOT = -5327.330457 meter/sec RA = 24.33098 deg ZDOT = -4346.054904 TA = 25.92703 MA = 25.84808 Ha = 196.274 n.mi Hp = 186.497 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -18352940.75 X = -5618640.45 Y = 2120009.87 feet Y = 583485.61 meter Z = 12058501.84 Z = 3648196.59 XDOT = -11408.337572 XDOT = -3396.319810 YDOT = -17478.118298 feet/sec YDOT = -5365.762334 meter/sec ZDOT = -14258.710314 ZDOT = -4362.750903 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -588585.71 X = -179400.92 Y = 18536274.98 feet Y = 5649856.61 meter Z = 11949578.21 Z = 3642231.44 XDOT = -17591.172354 XDOT = -5361.789334 YDOT = 8697.160616 feet/sec YDOT = 2650.894556 meter/sec ZDOT = -14325.425943 ZDOT = -4366.389827 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10208.42135606 .00016717 00000-0 10270-3 0 9005 2 25544 51.6461 24.6869 0007109 156.0301 204.1193 15.71318315 29807 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10208.42135606 = yrday.fracday Element set: 900 Inclination: 51.6461 deg RA of node: 24.6869 deg Eccentricity: .0007109 Arg of perigee: 156.0301 deg Mean anomaly: 204.1193 deg </pre> <p> Mean motion: 15.71318315 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 2980 Checksum: 276 </pre> <p> Coasting Arc #2 (Orbit 2995) </p><hr/> <p> Vector Time (GMT): 2010/209/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4323530.30 A = 6735628.52 meter Y = 4113538.89 meter E = .0016416 Z = 3116620.96 I = 51.76403 XDOT = -5559.592175 Wp = 110.12131 YDOT = 2127.643949 meter/sec RA = 19.27540 deg ZDOT = 4878.099003 TA = 285.98971 MA = 286.17049 Ha = 196.088 n.mi Hp = 186.653 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 14184810.69 X = 4262070.96 Y = 13495862.51 feet Y = 4161543.35 meter Z = 10225134.38 Z = 3137475.22 XDOT = -18240.131807 XDOT = -5606.667103 YDOT = 6980.459149 feet/sec YDOT = 2065.209731 meter/sec ZDOT = 16004.261820 ZDOT = 4850.976866 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15202542.06 X = 4633734.82 Y = -12268588.04 feet Y = -3739465.64 meter Z = 10308491.39 Z = 3142028.17 XDOT = 3667.337869 XDOT = 1117.804583 YDOT = 17972.248025 feet/sec YDOT = 5477.941198 meter/sec ZDOT = 15895.776677 ZDOT = 4845.032731 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10209.43894824 .00016717 00000-0 10270-3 0 9012 2 25544 51.6451 19.4817 0007132 160.5853 199.5582 15.71289510 29969 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10209.43894824 = yrday.fracday Element set: 901 Inclination: 51.6451 deg RA of node: 19.4817 deg Eccentricity: .0007132 Arg of perigee: 160.5853 deg Mean anomaly: 199.5582 deg </pre> <p> Mean motion: 15.71289510 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 2996 Checksum: 325 </pre> <p> Coasting Arc #3 (Orbit 3010) </p><hr/> <p> Vector Time (GMT): 2010/210/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3852262.72 A = 6730298.20 meter Y = -2876537.27 meter E = .0016302 Z = -4725089.92 I = 51.71634 XDOT = 6132.831492 Wp = 129.83370 YDOT = 3750.621062 meter/sec RA = 14.12118 deg ZDOT = 2712.611111 TA = 166.91581 MA = 166.87347 Ha = 196.032 n.mi Hp = 186.862 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12638657.22 X = 3907095.60 Y = -9437458.24 feet Y = -2833152.13 meter Z = -15502263.53 Z = -4706242.93 XDOT = 20120.838229 XDOT = 6077.258418 YDOT = 12305.187210 feet/sec YDOT = 3818.891184 meter/sec ZDOT = 8899.642752 ZDOT = 2742.269086 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -7957073.02 X = -2425315.86 Y = -13704677.99 feet Y = -4177185.85 meter Z = -15426867.43 Z = -4702109.19 XDOT = 13470.483680 XDOT = 4105.803426 YDOT = -17987.608328 feet/sec YDOT = -5482.623018 meter/sec ZDOT = 9018.206619 ZDOT = 2748.749377 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10210.39293210 .00016717 00000-0 10270-3 0 9022 2 25544 51.6444 14.6014 0007186 164.0441 196.0948 15.71307656 30117 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10210.39293210 = yrday.fracday Element set: 902 Inclination: 51.6444 deg RA of node: 14.6014 deg Eccentricity: .0007186 Arg of perigee: 164.0441 deg Mean anomaly: 196.0948 deg </pre> <p> Mean motion: 15.71307656 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3011 Checksum: 273 </pre> <p> Coasting Arc #4 (Orbit 3026) </p><hr/> <p> Vector Time (GMT): 2010/211/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -6149261.14 A = 6738741.61 meter Y = -2239238.65 meter E = .0014770 Z = -1576435.39 I = 51.71527 XDOT = 2977.419840 Wp = 154.19670 YDOT = -4137.640630 meter/sec RA = 9.04818 deg ZDOT = -5770.027550 TA = 43.16194 MA = 43.04625 Ha = 195.880 n.mi Hp = 186.928 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -20174741.26 X = -6116106.60 Y = -7346583.49 feet Y = -2307817.92 meter Z = -5172032.11 Z = -1606227.64 XDOT = 9768.437795 XDOT = 3051.495761 YDOT = -13574.936450 feet/sec YDOT = -4103.930913 meter/sec ZDOT = -18930.536581 ZDOT = -5755.383696 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -9219001.35 X = -2809951.61 Y = 19358621.18 feet Y = 5900507.74 meter Z = -5291142.64 Z = -1612740.28 XDOT = -11168.560027 XDOT = -3404.177096 YDOT = -10447.750805 feet/sec YDOT = -3184.474445 meter/sec ZDOT = -18871.939189 ZDOT = -5752.167065 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10211.41050696 .00016717 00000-0 10270-3 0 9036 2 25544 51.6443 9.3977 0007166 168.2313 191.9018 15.71300350 30270 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10211.41050696 = yrday.fracday Element set: 903 Inclination: 51.6443 deg RA of node: 9.3977 deg Eccentricity: .0007166 Arg of perigee: 168.2313 deg Mean anomaly: 191.9018 deg </pre> <p> Mean motion: 15.71300350 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3027 Checksum: 280 </pre> <p> Coasting Arc #5 (Orbit 3042) </p><hr/> <p> Vector Time (GMT): 2010/212/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1184044.76 A = 6728017.60 meter Y = 4063459.05 meter E = .0006664 Z = 5225971.16 I = 51.64887 XDOT = -7568.456691 Wp = 143.90256 YDOT = -1163.824886 meter/sec RA = 3.91381 deg ZDOT = -814.609073 TA = 313.82223 MA = 313.87731 Ha = 195.858 n.mi Hp = 187.078 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -3884661.28 X = -1254781.66 Y = 13331558.55 feet Y = 4049822.62 meter Z = 17145574.66 Z = 5220047.47 XDOT = -24830.894657 XDOT = -7550.922900 YDOT = -3818.323116 feet/sec YDOT = -1248.361824 meter/sec ZDOT = -2672.601945 ZDOT = -851.333721 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 12983383.03 X = 3957335.15 Y = 5006579.44 feet Y = 1526005.41 meter Z = 17121848.74 Z = 5218739.50 XDOT = -5363.530457 XDOT = -1634.804083 YDOT = 23497.652406 feet/sec YDOT = 7162.084453 meter/sec ZDOT = -2819.436920 ZDOT = -859.364373 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10212.42807305 .00016717 00000-0 10270-3 0 9046 2 25544 51.6442 4.1925 0007175 171.9126 188.2153 15.71307487 30433 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10212.42807305 = yrday.fracday Element set: 904 Inclination: 51.6442 deg RA of node: 4.1925 deg Eccentricity: .0007175 Arg of perigee: 171.9126 deg Mean anomaly: 188.2153 deg </pre> <p> Mean motion: 15.71307487 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3043 Checksum: 283 </pre> <p> Coasting Arc #6 (Orbit 3057) </p><hr/> <p> Vector Time (GMT): 2010/213/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6731837.90 A = 6739769.80 meter Y = -265371.59 meter E = .0009054 Z = -157855.97 I = 51.65758 XDOT = 322.280996 Wp = 80.29205 YDOT = 4763.703897 meter/sec RA = 358.80446 deg ZDOT = 6029.911767 TA = 277.99649 MA = 278.09922 Ha = 195.703 n.mi Hp = 187.190 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 22086082.34 X = 6735071.83 Y = -870641.69 feet Y = -190074.06 meter Z = -517900.17 Z = -125145.08 XDOT = 1057.352350 XDOT = 239.696414 YDOT = 15628.949793 feet/sec YDOT = 4766.845799 meter/sec ZDOT = 19783.175087 ZDOT = 6031.277023 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 462435.97 X = 140950.48 Y = -22101076.27 feet Y = -6736408.05 meter Z = -387106.09 Z = -117989.94 XDOT = 14046.203067 XDOT = 4281.282695 YDOT = -30.073606 feet/sec YDOT = -9.166435 meter/sec ZDOT = 19788.586276 ZDOT = 6031.561097 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10213.38203262 .00016717 00000-0 10270-3 0 9055 2 25544 51.6433 359.3122 0007151 175.6075 184.5151 15.71330643 30588 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10213.38203262 = yrday.fracday Element set: 905 Inclination: 51.6433 deg RA of node: 359.3122 deg Eccentricity: .0007151 Arg of perigee: 175.6075 deg Mean anomaly: 184.5151 deg </pre> <p> Mean motion: 15.71330643 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3058 Checksum: 277 </pre> <p> Coasting Arc #7 (Orbit 3073) </p><hr/> <p> Vector Time (GMT): 2010/214/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1712233.94 A = 6728046.28 meter Y = -3946824.50 meter E = .0015346 Z = -5184402.89 I = 51.58777 XDOT = 7403.464701 Wp = 108.94118 YDOT = -1725.985859 meter/sec RA = 353.69868 deg ZDOT = -1138.770211 TA = 150.20420 MA = 150.11673 Ha = 195.593 n.mi Hp = 187.195 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -5617565.44 X = -1642787.79 Y = -12948899.29 feet Y = -3965583.13 meter Z = -17009195.85 Z = -5192552.44 XDOT = 24289.582354 XDOT = 7427.746662 YDOT = -5662.683266 feet/sec YDOT = -1643.060056 meter/sec ZDOT = -3736.122739 ZDOT = -1102.745455 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13175192.30 X = -4015798.61 Y = 4953504.95 feet Y = 1509828.31 meter Z = -17041739.17 Z = -5194322.10 XDOT = -4248.484509 XDOT = -1294.938078 YDOT = -23572.005877 feet/sec YDOT = -7184.747391 meter/sec ZDOT = -3592.068103 ZDOT = -1094.862358 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10214.39958184 .00016717 00000-0 10270-3 0 9068 2 25544 51.6429 354.1072 0007200 178.3150 181.8037 15.71354547 30749 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10214.39958184 = yrday.fracday Element set: 906 Inclination: 51.6429 deg RA of node: 354.1072 deg Eccentricity: .0007200 Arg of perigee: 178.3150 deg Mean anomaly: 181.8037 deg </pre> <p> Mean motion: 15.71354547 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3074 Checksum: 301 </pre> <p> Coasting Arc #8 (Orbit 3089) </p><hr/> <p> Vector Time (GMT): 2010/215/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5903272.77 A = 6738203.55 meter Y = 2665364.26 meter E = .0017808 Z = 1817445.51 I = 51.59266 XDOT = -3499.597939 Wp = 135.68222 YDOT = -3873.878546 meter/sec RA = 348.55385 deg ZDOT = -5665.141610 TA = 24.15040 MA = 24.06701 Ha = 195.343 n.mi Hp = 187.478 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -19367692.82 X = -5941467.41 Y = 8744633.38 feet Y = 2599136.64 meter Z = 5962747.75 Z = 1788674.94 XDOT = -11481.620536 XDOT = -3428.499288 YDOT = -12709.575282 feet/sec YDOT = -3912.615189 meter/sec ZDOT = -18586.422606 ZDOT = -5681.970187 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 8239180.98 X = 2511302.36 Y = 19622714.67 feet Y = 5981003.43 meter Z = 5847688.85 Z = 1782375.56 XDOT = -11569.624076 XDOT = -3526.421418 YDOT = 10437.436060 feet/sec YDOT = 3181.330511 meter/sec ZDOT = -18653.665050 ZDOT = -5685.637107 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10215.41712003 .00016717 00000-0 10270-3 0 9071 2 25544 51.6433 348.9021 0006997 184.0724 176.0382 15.71403577 30907 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10215.41712003 = yrday.fracday Element set: 907 Inclination: 51.6433 deg RA of node: 348.9021 deg Eccentricity: .0006997 Arg of perigee: 184.0724 deg Mean anomaly: 176.0382 deg </pre> <p> Mean motion: 15.71403577 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3090 Checksum: 292 </pre> <p> Coasting Arc #9 (Orbit 3105) </p><hr/> <p> Vector Time (GMT): 2010/216/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4222549.98 A = 6730429.50 meter Y = 2543591.15 meter E = .0012606 Z = 4581813.69 I = 51.53649 XDOT = -5748.476504 Wp = 147.51871 YDOT = 4167.082658 meter/sec RA = 343.47134 deg ZDOT = 2970.148885 TA = 272.87933 MA = 273.02360 Ha = 195.237 n.mi Hp = 187.562 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 13853510.44 X = 4171535.73 Y = 8345115.33 feet Y = 2590524.58 meter Z = 15032197.15 Z = 4602203.07 XDOT = -18859.831051 XDOT = -5809.074723 YDOT = 13671.531031 feet/sec YDOT = 4102.460665 meter/sec ZDOT = 9744.582956 ZDOT = 2942.076097 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 8465173.65 X = 2580184.93 Y = -13691050.62 feet Y = -4173032.23 meter Z = 15113689.84 Z = 4606652.66 XDOT = 12508.194554 XDOT = 3812.497700 YDOT = 18418.269414 feet/sec YDOT = 5613.888517 meter/sec ZDOT = 9632.296976 ZDOT = 2935.924118 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10216.43465247 .00016717 00000-0 10270-3 0 9080 2 25544 51.6426 343.6967 0007157 186.8343 173.2723 15.71385075 31064 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10216.43465247 = yrday.fracday Element set: 908 Inclination: 51.6426 deg RA of node: 343.6967 deg Eccentricity: .0007157 Arg of perigee: 186.8343 deg Mean anomaly: 173.2723 deg </pre> <p> Mean motion: 15.71385075 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3106 Checksum: 318 </pre> <p> Coasting Arc #10 (Orbit 3120) </p><hr/> <p> Vector Time (GMT): 2010/217/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3920692.73 A = 6734961.48 meter Y = -4380230.15 meter E = .0007570 Z = -3296820.05 I = 51.52370 XDOT = 5844.185912 Wp = 151.74716 YDOT = 1693.201433 meter/sec RA = 338.30035 deg ZDOT = 4698.330260 TA = 169.58441 MA = 169.56872 Ha = 195.249 n.mi Hp = 187.715 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12863165.12 X = 3985397.10 Y = -14370833.81 feet Y = -4336024.49 meter Z = -10816338.73 Z = -3277616.75 XDOT = 19173.838294 XDOT = 5801.994402 YDOT = 5555.122812 feet/sec YDOT = 1758.318214 meter/sec ZDOT = 15414.469356 ZDOT = 4726.618804 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -14480444.91 X = -4413639.61 Y = -12804479.00 feet Y = -3902805.20 meter Z = -10739511.06 Z = -3273402.97 XDOT = 4459.661443 XDOT = 1359.304808 YDOT = -18072.786406 feet/sec YDOT = -5508.585296 meter/sec ZDOT = 15527.555388 ZDOT = 4732.798882 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10217.38858027 .00016717 00000-0 10270-3 0 9098 2 25544 51.6434 338.8166 0007234 188.8703 171.2332 15.71394693 31215 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10217.38858027 = yrday.fracday Element set: 909 Inclination: 51.6434 deg RA of node: 338.8166 deg Eccentricity: .0007234 Arg of perigee: 188.8703 deg Mean anomaly: 171.2332 deg </pre> <p> Mean motion: 15.71394693 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3121 Checksum: 317 </pre> <p> Coasting Arc #11 (Orbit 3136) </p><hr/> <p> Vector Time (GMT): 2010/218/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5716327.37 A = 6733965.97 meter Y = -276100.67 meter E = .0007238 Z = -3546276.52 I = 51.49356 XDOT = 3023.711564 Wp = 147.81110 YDOT = -5496.799273 meter/sec RA = 333.22671 deg ZDOT = -4456.218989 TA = 74.49577 MA = 74.41585 Ha = 194.952 n.mi Hp = 187.729 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -18754354.89 X = -5695588.15 Y = -905842.10 feet Y = -339907.70 meter Z = -11634765.47 Z = -3573995.77 XDOT = 9920.313530 XDOT = 3106.600299 YDOT = -18034.118350 feet/sec YDOT = -5462.522366 meter/sec ZDOT = -14620.141039 ZDOT = -4441.329253 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -425874.49 X = -129806.54 Y = 18702240.17 feet Y = 5700442.80 meter Z = -11745594.42 Z = -3580057.18 XDOT = -16921.941489 XDOT = -5157.807766 YDOT = -9509.022259 feet/sec YDOT = -2898.349985 meter/sec ZDOT = -14560.547886 ZDOT = -4438.054996 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10218.40609386 .00016717 00000-0 10270-3 0 9106 2 25544 51.6437 333.6119 0007067 192.6133 167.4853 15.71420869 31370 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10218.40609386 = yrday.fracday Element set: 910 Inclination: 51.6437 deg RA of node: 333.6119 deg Eccentricity: .0007067 Arg of perigee: 192.6133 deg Mean anomaly: 167.4853 deg </pre> <p> Mean motion: 15.71420869 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3137 Checksum: 310 </pre> <p> Coasting Arc #12 (Orbit 3152) </p><hr/> <p> Vector Time (GMT): 2010/219/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1259750.03 A = 6731199.22 meter Y = 4922980.85 meter E = .0007642 Z = 4406516.97 I = 51.45678 XDOT = -6860.617672 Wp = 117.91068 YDOT = 1189.880333 meter/sec RA = 328.04947 deg ZDOT = -3289.862997 TA = 5.19906 MA = 5.19113 Ha = 195.006 n.mi Hp = 188.007 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4133038.16 X = -1336111.77 Y = 16151511.99 feet Y = 4908466.14 meter Z = 14457076.68 Z = 4400212.26 XDOT = -22508.588164 XDOT = -6857.431949 YDOT = 3903.806867 feet/sec YDOT = 1113.178973 meter/sec ZDOT = -10793.513770 ZDOT = -3323.183448 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 16318031.61 X = 4973736.03 Y = 3522052.51 feet Y = 1073521.60 meter Z = 14431819.04 Z = 4398818.44 XDOT = 5119.181452 XDOT = 1560.326507 YDOT = 21066.298842 feet/sec YDOT = 6421.007887 meter/sec ZDOT = -10926.758020 ZDOT = -3330.475844 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10219.42359981 .00016717 00000-0 10270-3 0 9113 2 25544 51.6433 328.4063 0007182 196.3063 163.7869 15.71393771 31532 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10219.42359981 = yrday.fracday Element set: 911 Inclination: 51.6433 deg RA of node: 328.4063 deg Eccentricity: .0007182 Arg of perigee: 196.3063 deg Mean anomaly: 163.7869 deg </pre> <p> Mean motion: 15.71393771 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3153 Checksum: 319 </pre> <p> Coasting Arc #13 (Orbit 3168) </p><hr/> <p> Vector Time (GMT): 2010/220/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 5940203.61 A = 6737365.17 meter Y = -2344850.96 meter E = .0010970 Z = 2141388.60 I = 51.45464 XDOT = 134.638995 Wp = 101.16436 YDOT = 5383.033809 meter/sec RA = 322.96383 deg ZDOT = 5495.129930 TA = 282.81965 MA = 282.94220 Ha = 194.774 n.mi Hp = 188.032 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 19488856.98 X = 5955580.42 Y = -7693080.56 feet Y = -2278338.26 meter Z = 7025553.16 Z = 2170282.62 XDOT = 441.728986 XDOT = 47.741160 YDOT = 17660.872078 feet/sec YDOT = 5384.053058 meter/sec ZDOT = 18028.641502 ZDOT = 5495.573404 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -8846993.87 X = -2696563.73 Y = -18949740.66 feet Y = -5775880.95 meter Z = 7141110.58 Z = 2176610.50 XDOT = 16227.616144 XDOT = 4946.177401 YDOT = -749.995457 feet/sec YDOT = -228.598615 meter/sec ZDOT = 18030.369416 ZDOT = 5495.656598 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10220.44109451 .00016717 00000-0 10270-3 0 9123 2 25544 51.6446 323.2014 0007239 200.4868 159.6005 15.71459969 31693 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10220.44109451 = yrday.fracday Element set: 912 Inclination: 51.6446 deg RA of node: 323.2014 deg Eccentricity: .0007239 Arg of perigee: 200.4868 deg Mean anomaly: 159.6005 deg </pre> <p> Mean motion: 15.71459969 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3169 Checksum: 300 </pre> <p> Coasting Arc #14 (Orbit 3183) </p><hr/> <p> Vector Time (GMT): 2010/221/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1418836.85 A = 6728221.07 meter Y = -4189111.30 meter E = .0014095 Z = -5081508.90 I = 51.40065 XDOT = 6338.354010 Wp = 131.38497 YDOT = -4056.965989 meter/sec RA = 317.80152 deg ZDOT = 1568.373613 TA = 153.78354 MA = 153.71212 Ha = 194.625 n.mi Hp = 188.192 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4654976.56 X = -1347203.56 Y = -13743803.48 feet Y = -4204576.75 meter Z = -16671617.12 Z = -5088227.70 XDOT = 20795.124706 XDOT = 6375.629982 YDOT = -13310.255870 feet/sec YDOT = -3985.878397 meter/sec ZDOT = 5145.582721 ZDOT = 1599.254866 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13351452.19 X = -4069522.63 Y = 5603931.44 feet Y = 1708078.30 meter Z = -16698456.07 Z = -5089689.41 XDOT = -14465.196792 XDOT = -4408.991982 YDOT = -18700.811340 feet/sec YDOT = -5700.007296 meter/sec ZDOT = 5269.096759 ZDOT = 1606.020692 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10221.39499044 .00016717 00000-0 10270-3 0 9139 2 25544 51.6450 318.3229 0007091 203.7352 156.3483 15.71456210 31848 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10221.39499044 = yrday.fracday Element set: 913 Inclination: 51.6450 deg RA of node: 318.3229 deg Eccentricity: .0007091 Arg of perigee: 203.7352 deg Mean anomaly: 156.3483 deg </pre> <p> Mean motion: 15.71456210 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3184 Checksum: 291 </pre> <p> Coasting Arc #15 (Orbit 3199) </p><hr/> <p> Vector Time (GMT): 2010/222/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4871358.78 A = 6739227.99 meter Y = 4607941.10 meter E = .0014927 Z = -572290.44 I = 51.41592 XDOT = -2944.572606 Wp = 165.12510 YDOT = -3850.145630 meter/sec RA = 312.68732 deg ZDOT = -5984.746134 TA = 21.12026 MA = 21.05869 Ha = 194.364 n.mi Hp = 188.464 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -15982148.23 X = -4919743.56 Y = 15117917.00 feet Y = 4553196.14 meter Z = -1877593.31 Z = -596072.31 XDOT = -9660.671278 XDOT = -2872.228633 YDOT = -12631.711386 feet/sec YDOT = -3882.668940 meter/sec ZDOT = -19634.993879 ZDOT = -5998.874902 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 16557438.05 X = 5046707.12 Y = 14472922.23 feet Y = 4411346.70 meter Z = -1972714.03 Z = -601283.24 XDOT = -10619.974550 XDOT = -3236.968243 YDOT = 9486.237269 feet/sec YDOT = 2891.405120 meter/sec ZDOT = -19691.473356 ZDOT = -6001.961079 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10222.41246952 .00016717 00000-0 10270-3 0 9142 2 25544 51.6446 313.1171 0007006 208.4305 151.6476 15.71471886 32003 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10222.41246952 = yrday.fracday Element set: 914 Inclination: 51.6446 deg RA of node: 313.1171 deg Eccentricity: .0007006 Arg of perigee: 208.4305 deg Mean anomaly: 151.6476 deg </pre> <p> Mean motion: 15.71471886 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3200 Checksum: 279</pre> <hr/> <p><strong>INTERNATIONAL SPACE STATION ORBITAL DATA:</strong> </p> <p>The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability. The data normally contains past, current and predicted orbital data. Careful attention to the orbit # / epoch times! These sources include: </p><p>NASA Orbital Flight Dynamics<br/> DOD C-Band Radar Network<br/> Goddard Space Flight Center (GSFC)<br/> NASA Johnson Space Center (JSC)<br/> DoD/ USSTRATCOM/ US Space Command with permission </p> <p>By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command. </p><pre> David Cottle Director Of Engineering IDB Communications</pre> <hr/> <p>The following information is a reminder of your current mailing list subscription: </p><p>You are subscribed to the following list: </p><p><strong>[ISSTLE LIST]</strong> </p><p>using the following email: </p><p> <a href="mailto:&#x65;&#120;&#x61;&#x6D;&#112;&#x6C;&#101;&#x40;&#x65;&#120;&#97;&#x6D;&#112;&#x6C;&#x65;&#x2E;&#99;&#111;&#x6D;">&#x65;&#120;&#x61;&#x6D;&#112;&#x6C;&#101;&#x40;&#x65;&#120;&#97;&#x6D;&#112;&#x6C;&#x65;&#x2E;&#99;&#111;&#x6D;</a> </p><p>You may automatically unsubscribe from this list at any time by visiting the following URL: </p><p>&#60;<a href="http://www.aus-city.com/cgi-bin/dada/mail.cgi/u/ISSTLE_LIST/example/example.com/">http://www.aus-city.com/cgi-bin/dada/mail.cgi/u/ISSTLE_LIST/example/example.com/</a>&#62; </p><p>If the above URL is inoperable, make sure that you have copied the entire address. 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subscription_form_widget.tmpl --> [ISSTLE LIST] Current ISS TLEs @ 18:30 UTC tag:www.aus-city.com,2010-07-28:%2Fcgi-bin%2Fdada%2Fmail.cgi%2Farchive%2FISSTLE_LIST%2F20100728044502%2F 2010-07-28T04:45:02Z 2010-07-28T04:45:02Z <p>&#60;B&#62; ISS TRAJECTORY DATA&#60;/B&#62; </p><p> Lift off time (UTC) : N/A<br/> Area (sq ft) : 8880.23<br/> Drag Coefficient (Cd) : 2.00<br/> Monthly MSFC 50% solar flux (F10.7-jansky) : 74.8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0.74 ET - UTC (sec) : 66.18<br/> UT1 - UTC (sec) : 0.00 </p><p> Maneuvers contained within the current ephemeris are as follows: </p><pre> IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP </pre> <hr/> There are no maneuvers. <p> Coasting Arc #1 (Orbit 2979) </p><hr/> <p> Vector Time (GMT): 2010/208/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5593976.34 A = 6734057.59 meter Y = 646179.01 meter E = .0015774 Z = 3675431.36 I = 51.78783 XDOT = -3477.261292 Wp = 109.99564 YDOT = -5327.330457 meter/sec RA = 24.33098 deg ZDOT = -4346.054904 TA = 25.92703 MA = 25.84808 Ha = 196.274 n.mi Hp = 186.497 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -18352940.75 X = -5618640.45 Y = 2120009.87 feet Y = 583485.61 meter Z = 12058501.84 Z = 3648196.59 XDOT = -11408.337572 XDOT = -3396.319810 YDOT = -17478.118298 feet/sec YDOT = -5365.762334 meter/sec ZDOT = -14258.710314 ZDOT = -4362.750903 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -588585.71 X = -179400.92 Y = 18536274.98 feet Y = 5649856.61 meter Z = 11949578.21 Z = 3642231.44 XDOT = -17591.172354 XDOT = -5361.789334 YDOT = 8697.160616 feet/sec YDOT = 2650.894556 meter/sec ZDOT = -14325.425943 ZDOT = -4366.389827 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10208.42135606 .00016717 00000-0 10270-3 0 9005 2 25544 51.6461 24.6869 0007109 156.0301 204.1193 15.71318315 29807 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10208.42135606 = yrday.fracday Element set: 900 Inclination: 51.6461 deg RA of node: 24.6869 deg Eccentricity: .0007109 Arg of perigee: 156.0301 deg Mean anomaly: 204.1193 deg </pre> <p> Mean motion: 15.71318315 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 2980 Checksum: 276 </pre> <p> Coasting Arc #2 (Orbit 2995) </p><hr/> <p> Vector Time (GMT): 2010/209/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4323530.30 A = 6735628.52 meter Y = 4113538.89 meter E = .0016416 Z = 3116620.96 I = 51.76403 XDOT = -5559.592175 Wp = 110.12131 YDOT = 2127.643949 meter/sec RA = 19.27540 deg ZDOT = 4878.099003 TA = 285.98971 MA = 286.17049 Ha = 196.088 n.mi Hp = 186.653 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 14184810.69 X = 4262070.96 Y = 13495862.51 feet Y = 4161543.35 meter Z = 10225134.38 Z = 3137475.22 XDOT = -18240.131807 XDOT = -5606.667103 YDOT = 6980.459149 feet/sec YDOT = 2065.209731 meter/sec ZDOT = 16004.261820 ZDOT = 4850.976866 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15202542.06 X = 4633734.82 Y = -12268588.04 feet Y = -3739465.64 meter Z = 10308491.39 Z = 3142028.17 XDOT = 3667.337869 XDOT = 1117.804583 YDOT = 17972.248025 feet/sec YDOT = 5477.941198 meter/sec ZDOT = 15895.776677 ZDOT = 4845.032731 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10209.43894824 .00016717 00000-0 10270-3 0 9012 2 25544 51.6451 19.4817 0007132 160.5853 199.5582 15.71289510 29969 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10209.43894824 = yrday.fracday Element set: 901 Inclination: 51.6451 deg RA of node: 19.4817 deg Eccentricity: .0007132 Arg of perigee: 160.5853 deg Mean anomaly: 199.5582 deg </pre> <p> Mean motion: 15.71289510 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 2996 Checksum: 325 </pre> <p> Coasting Arc #3 (Orbit 3010) </p><hr/> <p> Vector Time (GMT): 2010/210/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3852262.72 A = 6730298.20 meter Y = -2876537.27 meter E = .0016302 Z = -4725089.92 I = 51.71634 XDOT = 6132.831492 Wp = 129.83370 YDOT = 3750.621062 meter/sec RA = 14.12118 deg ZDOT = 2712.611111 TA = 166.91581 MA = 166.87347 Ha = 196.032 n.mi Hp = 186.862 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12638657.22 X = 3907095.60 Y = -9437458.24 feet Y = -2833152.13 meter Z = -15502263.53 Z = -4706242.93 XDOT = 20120.838229 XDOT = 6077.258418 YDOT = 12305.187210 feet/sec YDOT = 3818.891184 meter/sec ZDOT = 8899.642752 ZDOT = 2742.269086 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -7957073.02 X = -2425315.86 Y = -13704677.99 feet Y = -4177185.85 meter Z = -15426867.43 Z = -4702109.19 XDOT = 13470.483680 XDOT = 4105.803426 YDOT = -17987.608328 feet/sec YDOT = -5482.623018 meter/sec ZDOT = 9018.206619 ZDOT = 2748.749377 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10210.39293210 .00016717 00000-0 10270-3 0 9022 2 25544 51.6444 14.6014 0007186 164.0441 196.0948 15.71307656 30117 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10210.39293210 = yrday.fracday Element set: 902 Inclination: 51.6444 deg RA of node: 14.6014 deg Eccentricity: .0007186 Arg of perigee: 164.0441 deg Mean anomaly: 196.0948 deg </pre> <p> Mean motion: 15.71307656 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3011 Checksum: 273 </pre> <p> Coasting Arc #4 (Orbit 3026) </p><hr/> <p> Vector Time (GMT): 2010/211/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -6149261.14 A = 6738741.61 meter Y = -2239238.65 meter E = .0014770 Z = -1576435.39 I = 51.71527 XDOT = 2977.419840 Wp = 154.19670 YDOT = -4137.640630 meter/sec RA = 9.04818 deg ZDOT = -5770.027550 TA = 43.16194 MA = 43.04625 Ha = 195.880 n.mi Hp = 186.928 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -20174741.26 X = -6116106.60 Y = -7346583.49 feet Y = -2307817.92 meter Z = -5172032.11 Z = -1606227.64 XDOT = 9768.437795 XDOT = 3051.495761 YDOT = -13574.936450 feet/sec YDOT = -4103.930913 meter/sec ZDOT = -18930.536581 ZDOT = -5755.383696 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -9219001.35 X = -2809951.61 Y = 19358621.18 feet Y = 5900507.74 meter Z = -5291142.64 Z = -1612740.28 XDOT = -11168.560027 XDOT = -3404.177096 YDOT = -10447.750805 feet/sec YDOT = -3184.474445 meter/sec ZDOT = -18871.939189 ZDOT = -5752.167065 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10211.41050696 .00016717 00000-0 10270-3 0 9036 2 25544 51.6443 9.3977 0007166 168.2313 191.9018 15.71300350 30270 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10211.41050696 = yrday.fracday Element set: 903 Inclination: 51.6443 deg RA of node: 9.3977 deg Eccentricity: .0007166 Arg of perigee: 168.2313 deg Mean anomaly: 191.9018 deg </pre> <p> Mean motion: 15.71300350 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3027 Checksum: 280 </pre> <p> Coasting Arc #5 (Orbit 3042) </p><hr/> <p> Vector Time (GMT): 2010/212/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1184044.76 A = 6728017.60 meter Y = 4063459.05 meter E = .0006664 Z = 5225971.16 I = 51.64887 XDOT = -7568.456691 Wp = 143.90256 YDOT = -1163.824886 meter/sec RA = 3.91381 deg ZDOT = -814.609073 TA = 313.82223 MA = 313.87731 Ha = 195.858 n.mi Hp = 187.078 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -3884661.28 X = -1254781.66 Y = 13331558.55 feet Y = 4049822.62 meter Z = 17145574.66 Z = 5220047.47 XDOT = -24830.894657 XDOT = -7550.922900 YDOT = -3818.323116 feet/sec YDOT = -1248.361824 meter/sec ZDOT = -2672.601945 ZDOT = -851.333721 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 12983383.03 X = 3957335.15 Y = 5006579.44 feet Y = 1526005.41 meter Z = 17121848.74 Z = 5218739.50 XDOT = -5363.530457 XDOT = -1634.804083 YDOT = 23497.652406 feet/sec YDOT = 7162.084453 meter/sec ZDOT = -2819.436920 ZDOT = -859.364373 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10212.42807305 .00016717 00000-0 10270-3 0 9046 2 25544 51.6442 4.1925 0007175 171.9126 188.2153 15.71307487 30433 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10212.42807305 = yrday.fracday Element set: 904 Inclination: 51.6442 deg RA of node: 4.1925 deg Eccentricity: .0007175 Arg of perigee: 171.9126 deg Mean anomaly: 188.2153 deg </pre> <p> Mean motion: 15.71307487 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3043 Checksum: 283 </pre> <p> Coasting Arc #6 (Orbit 3057) </p><hr/> <p> Vector Time (GMT): 2010/213/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6731837.90 A = 6739769.80 meter Y = -265371.59 meter E = .0009054 Z = -157855.97 I = 51.65758 XDOT = 322.280996 Wp = 80.29205 YDOT = 4763.703897 meter/sec RA = 358.80446 deg ZDOT = 6029.911767 TA = 277.99649 MA = 278.09922 Ha = 195.703 n.mi Hp = 187.190 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 22086082.34 X = 6735071.83 Y = -870641.69 feet Y = -190074.06 meter Z = -517900.17 Z = -125145.08 XDOT = 1057.352350 XDOT = 239.696414 YDOT = 15628.949793 feet/sec YDOT = 4766.845799 meter/sec ZDOT = 19783.175087 ZDOT = 6031.277023 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 462435.97 X = 140950.48 Y = -22101076.27 feet Y = -6736408.05 meter Z = -387106.09 Z = -117989.94 XDOT = 14046.203067 XDOT = 4281.282695 YDOT = -30.073606 feet/sec YDOT = -9.166435 meter/sec ZDOT = 19788.586276 ZDOT = 6031.561097 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10213.38203262 .00016717 00000-0 10270-3 0 9055 2 25544 51.6433 359.3122 0007151 175.6075 184.5151 15.71330643 30588 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10213.38203262 = yrday.fracday Element set: 905 Inclination: 51.6433 deg RA of node: 359.3122 deg Eccentricity: .0007151 Arg of perigee: 175.6075 deg Mean anomaly: 184.5151 deg </pre> <p> Mean motion: 15.71330643 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3058 Checksum: 277 </pre> <p> Coasting Arc #7 (Orbit 3073) </p><hr/> <p> Vector Time (GMT): 2010/214/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1712233.94 A = 6728046.28 meter Y = -3946824.50 meter E = .0015346 Z = -5184402.89 I = 51.58777 XDOT = 7403.464701 Wp = 108.94118 YDOT = -1725.985859 meter/sec RA = 353.69868 deg ZDOT = -1138.770211 TA = 150.20420 MA = 150.11673 Ha = 195.593 n.mi Hp = 187.195 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -5617565.44 X = -1642787.79 Y = -12948899.29 feet Y = -3965583.13 meter Z = -17009195.85 Z = -5192552.44 XDOT = 24289.582354 XDOT = 7427.746662 YDOT = -5662.683266 feet/sec YDOT = -1643.060056 meter/sec ZDOT = -3736.122739 ZDOT = -1102.745455 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13175192.30 X = -4015798.61 Y = 4953504.95 feet Y = 1509828.31 meter Z = -17041739.17 Z = -5194322.10 XDOT = -4248.484509 XDOT = -1294.938078 YDOT = -23572.005877 feet/sec YDOT = -7184.747391 meter/sec ZDOT = -3592.068103 ZDOT = -1094.862358 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10214.39958184 .00016717 00000-0 10270-3 0 9068 2 25544 51.6429 354.1072 0007200 178.3150 181.8037 15.71354547 30749 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10214.39958184 = yrday.fracday Element set: 906 Inclination: 51.6429 deg RA of node: 354.1072 deg Eccentricity: .0007200 Arg of perigee: 178.3150 deg Mean anomaly: 181.8037 deg </pre> <p> Mean motion: 15.71354547 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3074 Checksum: 301 </pre> <p> Coasting Arc #8 (Orbit 3089) </p><hr/> <p> Vector Time (GMT): 2010/215/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5903272.77 A = 6738203.55 meter Y = 2665364.26 meter E = .0017808 Z = 1817445.51 I = 51.59266 XDOT = -3499.597939 Wp = 135.68222 YDOT = -3873.878546 meter/sec RA = 348.55385 deg ZDOT = -5665.141610 TA = 24.15040 MA = 24.06701 Ha = 195.343 n.mi Hp = 187.478 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -19367692.82 X = -5941467.41 Y = 8744633.38 feet Y = 2599136.64 meter Z = 5962747.75 Z = 1788674.94 XDOT = -11481.620536 XDOT = -3428.499288 YDOT = -12709.575282 feet/sec YDOT = -3912.615189 meter/sec ZDOT = -18586.422606 ZDOT = -5681.970187 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 8239180.98 X = 2511302.36 Y = 19622714.67 feet Y = 5981003.43 meter Z = 5847688.85 Z = 1782375.56 XDOT = -11569.624076 XDOT = -3526.421418 YDOT = 10437.436060 feet/sec YDOT = 3181.330511 meter/sec ZDOT = -18653.665050 ZDOT = -5685.637107 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10215.41712003 .00016717 00000-0 10270-3 0 9071 2 25544 51.6433 348.9021 0006997 184.0724 176.0382 15.71403577 30907 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10215.41712003 = yrday.fracday Element set: 907 Inclination: 51.6433 deg RA of node: 348.9021 deg Eccentricity: .0006997 Arg of perigee: 184.0724 deg Mean anomaly: 176.0382 deg </pre> <p> Mean motion: 15.71403577 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3090 Checksum: 292 </pre> <p> Coasting Arc #9 (Orbit 3105) </p><hr/> <p> Vector Time (GMT): 2010/216/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4222549.98 A = 6730429.50 meter Y = 2543591.15 meter E = .0012606 Z = 4581813.69 I = 51.53649 XDOT = -5748.476504 Wp = 147.51871 YDOT = 4167.082658 meter/sec RA = 343.47134 deg ZDOT = 2970.148885 TA = 272.87933 MA = 273.02360 Ha = 195.237 n.mi Hp = 187.562 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 13853510.44 X = 4171535.73 Y = 8345115.33 feet Y = 2590524.58 meter Z = 15032197.15 Z = 4602203.07 XDOT = -18859.831051 XDOT = -5809.074723 YDOT = 13671.531031 feet/sec YDOT = 4102.460665 meter/sec ZDOT = 9744.582956 ZDOT = 2942.076097 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 8465173.65 X = 2580184.93 Y = -13691050.62 feet Y = -4173032.23 meter Z = 15113689.84 Z = 4606652.66 XDOT = 12508.194554 XDOT = 3812.497700 YDOT = 18418.269414 feet/sec YDOT = 5613.888517 meter/sec ZDOT = 9632.296976 ZDOT = 2935.924118 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10216.43465247 .00016717 00000-0 10270-3 0 9080 2 25544 51.6426 343.6967 0007157 186.8343 173.2723 15.71385075 31064 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10216.43465247 = yrday.fracday Element set: 908 Inclination: 51.6426 deg RA of node: 343.6967 deg Eccentricity: .0007157 Arg of perigee: 186.8343 deg Mean anomaly: 173.2723 deg </pre> <p> Mean motion: 15.71385075 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3106 Checksum: 318 </pre> <p> Coasting Arc #10 (Orbit 3120) </p><hr/> <p> Vector Time (GMT): 2010/217/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3920692.73 A = 6734961.48 meter Y = -4380230.15 meter E = .0007570 Z = -3296820.05 I = 51.52370 XDOT = 5844.185912 Wp = 151.74716 YDOT = 1693.201433 meter/sec RA = 338.30035 deg ZDOT = 4698.330260 TA = 169.58441 MA = 169.56872 Ha = 195.249 n.mi Hp = 187.715 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12863165.12 X = 3985397.10 Y = -14370833.81 feet Y = -4336024.49 meter Z = -10816338.73 Z = -3277616.75 XDOT = 19173.838294 XDOT = 5801.994402 YDOT = 5555.122812 feet/sec YDOT = 1758.318214 meter/sec ZDOT = 15414.469356 ZDOT = 4726.618804 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -14480444.91 X = -4413639.61 Y = -12804479.00 feet Y = -3902805.20 meter Z = -10739511.06 Z = -3273402.97 XDOT = 4459.661443 XDOT = 1359.304808 YDOT = -18072.786406 feet/sec YDOT = -5508.585296 meter/sec ZDOT = 15527.555388 ZDOT = 4732.798882 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10217.38858027 .00016717 00000-0 10270-3 0 9098 2 25544 51.6434 338.8166 0007234 188.8703 171.2332 15.71394693 31215 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10217.38858027 = yrday.fracday Element set: 909 Inclination: 51.6434 deg RA of node: 338.8166 deg Eccentricity: .0007234 Arg of perigee: 188.8703 deg Mean anomaly: 171.2332 deg </pre> <p> Mean motion: 15.71394693 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3121 Checksum: 317 </pre> <p> Coasting Arc #11 (Orbit 3136) </p><hr/> <p> Vector Time (GMT): 2010/218/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5716327.37 A = 6733965.97 meter Y = -276100.67 meter E = .0007238 Z = -3546276.52 I = 51.49356 XDOT = 3023.711564 Wp = 147.81110 YDOT = -5496.799273 meter/sec RA = 333.22671 deg ZDOT = -4456.218989 TA = 74.49577 MA = 74.41585 Ha = 194.952 n.mi Hp = 187.729 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -18754354.89 X = -5695588.15 Y = -905842.10 feet Y = -339907.70 meter Z = -11634765.47 Z = -3573995.77 XDOT = 9920.313530 XDOT = 3106.600299 YDOT = -18034.118350 feet/sec YDOT = -5462.522366 meter/sec ZDOT = -14620.141039 ZDOT = -4441.329253 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -425874.49 X = -129806.54 Y = 18702240.17 feet Y = 5700442.80 meter Z = -11745594.42 Z = -3580057.18 XDOT = -16921.941489 XDOT = -5157.807766 YDOT = -9509.022259 feet/sec YDOT = -2898.349985 meter/sec ZDOT = -14560.547886 ZDOT = -4438.054996 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10218.40609386 .00016717 00000-0 10270-3 0 9106 2 25544 51.6437 333.6119 0007067 192.6133 167.4853 15.71420869 31370 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10218.40609386 = yrday.fracday Element set: 910 Inclination: 51.6437 deg RA of node: 333.6119 deg Eccentricity: .0007067 Arg of perigee: 192.6133 deg Mean anomaly: 167.4853 deg </pre> <p> Mean motion: 15.71420869 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3137 Checksum: 310 </pre> <p> Coasting Arc #12 (Orbit 3152) </p><hr/> <p> Vector Time (GMT): 2010/219/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1259750.03 A = 6731199.22 meter Y = 4922980.85 meter E = .0007642 Z = 4406516.97 I = 51.45678 XDOT = -6860.617672 Wp = 117.91068 YDOT = 1189.880333 meter/sec RA = 328.04947 deg ZDOT = -3289.862997 TA = 5.19906 MA = 5.19113 Ha = 195.006 n.mi Hp = 188.007 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4133038.16 X = -1336111.77 Y = 16151511.99 feet Y = 4908466.14 meter Z = 14457076.68 Z = 4400212.26 XDOT = -22508.588164 XDOT = -6857.431949 YDOT = 3903.806867 feet/sec YDOT = 1113.178973 meter/sec ZDOT = -10793.513770 ZDOT = -3323.183448 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 16318031.61 X = 4973736.03 Y = 3522052.51 feet Y = 1073521.60 meter Z = 14431819.04 Z = 4398818.44 XDOT = 5119.181452 XDOT = 1560.326507 YDOT = 21066.298842 feet/sec YDOT = 6421.007887 meter/sec ZDOT = -10926.758020 ZDOT = -3330.475844 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10219.42359981 .00016717 00000-0 10270-3 0 9113 2 25544 51.6433 328.4063 0007182 196.3063 163.7869 15.71393771 31532 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10219.42359981 = yrday.fracday Element set: 911 Inclination: 51.6433 deg RA of node: 328.4063 deg Eccentricity: .0007182 Arg of perigee: 196.3063 deg Mean anomaly: 163.7869 deg </pre> <p> Mean motion: 15.71393771 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3153 Checksum: 319 </pre> <p> Coasting Arc #13 (Orbit 3168) </p><hr/> <p> Vector Time (GMT): 2010/220/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 5940203.61 A = 6737365.17 meter Y = -2344850.96 meter E = .0010970 Z = 2141388.60 I = 51.45464 XDOT = 134.638995 Wp = 101.16436 YDOT = 5383.033809 meter/sec RA = 322.96383 deg ZDOT = 5495.129930 TA = 282.81965 MA = 282.94220 Ha = 194.774 n.mi Hp = 188.032 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 19488856.98 X = 5955580.42 Y = -7693080.56 feet Y = -2278338.26 meter Z = 7025553.16 Z = 2170282.62 XDOT = 441.728986 XDOT = 47.741160 YDOT = 17660.872078 feet/sec YDOT = 5384.053058 meter/sec ZDOT = 18028.641502 ZDOT = 5495.573404 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -8846993.87 X = -2696563.73 Y = -18949740.66 feet Y = -5775880.95 meter Z = 7141110.58 Z = 2176610.50 XDOT = 16227.616144 XDOT = 4946.177401 YDOT = -749.995457 feet/sec YDOT = -228.598615 meter/sec ZDOT = 18030.369416 ZDOT = 5495.656598 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10220.44109451 .00016717 00000-0 10270-3 0 9123 2 25544 51.6446 323.2014 0007239 200.4868 159.6005 15.71459969 31693 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10220.44109451 = yrday.fracday Element set: 912 Inclination: 51.6446 deg RA of node: 323.2014 deg Eccentricity: .0007239 Arg of perigee: 200.4868 deg Mean anomaly: 159.6005 deg </pre> <p> Mean motion: 15.71459969 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3169 Checksum: 300 </pre> <p> Coasting Arc #14 (Orbit 3183) </p><hr/> <p> Vector Time (GMT): 2010/221/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1418836.85 A = 6728221.07 meter Y = -4189111.30 meter E = .0014095 Z = -5081508.90 I = 51.40065 XDOT = 6338.354010 Wp = 131.38497 YDOT = -4056.965989 meter/sec RA = 317.80152 deg ZDOT = 1568.373613 TA = 153.78354 MA = 153.71212 Ha = 194.625 n.mi Hp = 188.192 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4654976.56 X = -1347203.56 Y = -13743803.48 feet Y = -4204576.75 meter Z = -16671617.12 Z = -5088227.70 XDOT = 20795.124706 XDOT = 6375.629982 YDOT = -13310.255870 feet/sec YDOT = -3985.878397 meter/sec ZDOT = 5145.582721 ZDOT = 1599.254866 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13351452.19 X = -4069522.63 Y = 5603931.44 feet Y = 1708078.30 meter Z = -16698456.07 Z = -5089689.41 XDOT = -14465.196792 XDOT = -4408.991982 YDOT = -18700.811340 feet/sec YDOT = -5700.007296 meter/sec ZDOT = 5269.096759 ZDOT = 1606.020692 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10221.39499044 .00016717 00000-0 10270-3 0 9139 2 25544 51.6450 318.3229 0007091 203.7352 156.3483 15.71456210 31848 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10221.39499044 = yrday.fracday Element set: 913 Inclination: 51.6450 deg RA of node: 318.3229 deg Eccentricity: .0007091 Arg of perigee: 203.7352 deg Mean anomaly: 156.3483 deg </pre> <p> Mean motion: 15.71456210 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3184 Checksum: 291 </pre> <p> Coasting Arc #15 (Orbit 3199) </p><hr/> <p> Vector Time (GMT): 2010/222/09:09:47.811 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4871358.78 A = 6739227.99 meter Y = 4607941.10 meter E = .0014927 Z = -572290.44 I = 51.41592 XDOT = -2944.572606 Wp = 165.12510 YDOT = -3850.145630 meter/sec RA = 312.68732 deg ZDOT = -5984.746134 TA = 21.12026 MA = 21.05869 Ha = 194.364 n.mi Hp = 188.464 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -15982148.23 X = -4919743.56 Y = 15117917.00 feet Y = 4553196.14 meter Z = -1877593.31 Z = -596072.31 XDOT = -9660.671278 XDOT = -2872.228633 YDOT = -12631.711386 feet/sec YDOT = -3882.668940 meter/sec ZDOT = -19634.993879 ZDOT = -5998.874902 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 16557438.05 X = 5046707.12 Y = 14472922.23 feet Y = 4411346.70 meter Z = -1972714.03 Z = -601283.24 XDOT = -10619.974550 XDOT = -3236.968243 YDOT = 9486.237269 feet/sec YDOT = 2891.405120 meter/sec ZDOT = -19691.473356 ZDOT = -6001.961079 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10222.41246952 .00016717 00000-0 10270-3 0 9142 2 25544 51.6446 313.1171 0007006 208.4305 151.6476 15.71471886 32003 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10222.41246952 = yrday.fracday Element set: 914 Inclination: 51.6446 deg RA of node: 313.1171 deg Eccentricity: .0007006 Arg of perigee: 208.4305 deg Mean anomaly: 151.6476 deg </pre> <p> Mean motion: 15.71471886 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3200 Checksum: 279</pre> <hr/> <p><strong>INTERNATIONAL SPACE STATION ORBITAL DATA:</strong> </p> <p>The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability. The data normally contains past, current and predicted orbital data. Careful attention to the orbit # / epoch times! These sources include: </p><p>NASA Orbital Flight Dynamics<br/> DOD C-Band Radar Network<br/> Goddard Space Flight Center (GSFC)<br/> NASA Johnson Space Center (JSC)<br/> DoD/ USSTRATCOM/ US Space Command with permission </p> <p>By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command. </p><pre> David Cottle Director Of Engineering IDB Communications</pre> <hr/> <p>The following information is a reminder of your current mailing list subscription: </p><p>You are subscribed to the following list: </p><p><strong>[ISSTLE LIST]</strong> </p><p>using the following email: </p><p> <a href="mailto:&#101;&#120;&#x61;&#109;&#112;&#108;&#x65;&#x40;&#101;&#120;&#97;&#x6D;&#112;&#108;&#101;&#x2E;&#x63;&#x6F;&#109;">&#101;&#120;&#x61;&#109;&#112;&#108;&#x65;&#x40;&#101;&#120;&#97;&#x6D;&#112;&#108;&#101;&#x2E;&#x63;&#x6F;&#109;</a> </p><p>You may automatically unsubscribe from this list at any time by visiting the following URL: </p><p>&#60;<a href="http://www.aus-city.com/cgi-bin/dada/mail.cgi/u/ISSTLE_LIST/example/example.com/">http://www.aus-city.com/cgi-bin/dada/mail.cgi/u/ISSTLE_LIST/example/example.com/</a>&#62; </p><p>If the above URL is inoperable, make sure that you have copied the entire address. 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subscription_form_widget.tmpl --> [ISSTLE LIST] Current ISS TLEs @ 06:30 UTC tag:www.aus-city.com,2010-07-27:%2Fcgi-bin%2Fdada%2Fmail.cgi%2Farchive%2FISSTLE_LIST%2F20100727164502%2F 2010-07-27T16:45:02Z 2010-07-27T16:45:02Z <p>&#60;B&#62; ISS TRAJECTORY DATA&#60;/B&#62; </p><p> Lift off time (UTC) : N/A<br/> Area (sq ft) : 8880.23<br/> Drag Coefficient (Cd) : 2.00<br/> Monthly MSFC 50% solar flux (F10.7-jansky) : 74.8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0.74 ET - UTC (sec) : 66.18<br/> UT1 - UTC (sec) : 0.00 </p><p> Maneuvers contained within the current ephemeris are as follows: </p><pre> IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP </pre> <hr/> There are no maneuvers. <p> Coasting Arc #1 (Orbit 2965) </p><hr/> <p> Vector Time (GMT): 2010/207/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5717102.70 A = 6739607.78 meter Y = -3526312.96 meter E = .0018564 Z = -418678.88 I = 51.82705 XDOT = 2815.697421 Wp = 143.30493 YDOT = -3866.323319 meter/sec RA = 28.85763 deg ZDOT = -6035.887764 TA = 41.23371 MA = 41.09364 Ha = 196.258 n.mi Hp = 186.203 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -18756898.62 X = -5675212.10 Y = -11569268.23 feet Y = -3590010.75 meter Z = -1373618.38 Z = -446350.53 XDOT = 9237.852431 XDOT = 2888.042646 YDOT = -12684.787793 feet/sec YDOT = -3834.431385 meter/sec ZDOT = -19802.781379 ZDOT = -6022.034101 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 622730.00 X = 189808.10 Y = 22021926.81 feet Y = 6712283.29 meter Z = -1484246.41 Z = -452398.31 XDOT = -14132.740932 XDOT = -4307.659436 YDOT = -900.344301 feet/sec YDOT = -274.424943 meter/sec ZDOT = -19747.336617 ZDOT = -6018.988201 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10207.53098269 .00016717 00000-0 10270-3 0 9009 2 25544 51.6423 29.2368 0007425 151.8329 208.3235 15.71362563 29665 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10207.53098269 = yrday.fracday Element set: 900 Inclination: 51.6423 deg RA of node: 29.2368 deg Eccentricity: .0007425 Arg of perigee: 151.8329 deg Mean anomaly: 208.3235 deg </pre> <p> Mean motion: 15.71362563 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 2966 Checksum: 308 </pre> <p> Coasting Arc #2 (Orbit 2981) </p><hr/> <p> Vector Time (GMT): 2010/208/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1123075.04 A = 6727891.37 meter Y = 4035216.39 meter E = .0009794 Z = 5260631.19 I = 51.75928 XDOT = -7190.339566 Wp = 143.68097 YDOT = -2705.907320 meter/sec RA = 23.75270 deg ZDOT = 532.308459 TA = 301.22216 MA = 301.31810 Ha = 196.414 n.mi Hp = 186.365 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -3684629.38 X = -1193668.71 Y = 13238898.91 feet Y = 4022262.35 meter Z = 17259288.68 Z = 5255004.28 XDOT = -23590.352906 XDOT = -7162.133015 YDOT = -8877.648689 feet/sec YDOT = -2786.156327 meter/sec ZDOT = 1746.418828 ZDOT = 497.446870 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13072276.65 X = 3984429.92 Y = -4328765.63 feet Y = -1319407.76 meter Z = 17236744.33 Z = 5253759.67 XDOT = 5642.824603 XDOT = 1719.932939 YDOT = 23547.393545 feet/sec YDOT = 7177.245553 meter/sec ZDOT = 1607.028774 ZDOT = 489.822370 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10208.54854054 .00016717 00000-0 10270-3 0 9014 2 25544 51.6416 24.0311 0007644 155.3537 204.7991 15.71295665 29826 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10208.54854054 = yrday.fracday Element set: 901 Inclination: 51.6416 deg RA of node: 24.0311 deg Eccentricity: .0007644 Arg of perigee: 155.3537 deg Mean anomaly: 204.7991 deg </pre> <p> Mean motion: 15.71295665 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 2982 Checksum: 304 </pre> <p> Coasting Arc #3 (Orbit 2996) </p><hr/> <p> Vector Time (GMT): 2010/209/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6517634.00 A = 6738981.46 meter Y = 1098314.22 meter E = .0008177 Z = -1321691.16 I = 51.76954 XDOT = 341.100511 Wp = 90.28639 YDOT = 4978.381138 meter/sec RA = 18.62891 deg ZDOT = 5850.071472 TA = 255.25843 MA = 255.34906 Ha = 196.238 n.mi Hp = 186.432 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 21383313.65 X = 6511288.45 Y = 3603393.10 feet Y = 1171162.90 meter Z = -4336257.10 Z = -1290044.49 XDOT = 1119.096165 XDOT = 256.987990 YDOT = 16333.271451 feet/sec YDOT = 4981.724853 meter/sec ZDOT = 19193.147874 ZDOT = 5851.524520 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -9419779.08 X = -2871148.66 Y = -19559646.42 feet Y = -5961780.23 meter Z = -4209710.65 Z = -1283119.81 XDOT = 11328.936970 XDOT = 3453.059988 YDOT = -9565.443565 feet/sec YDOT = -2915.547199 meter/sec ZDOT = 19198.909115 ZDOT = 5851.827498 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10209.50248946 .00016717 00000-0 10270-3 0 9029 2 25544 51.6422 19.1509 0007736 159.5539 200.5934 15.71358465 29972 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10209.50248946 = yrday.fracday Element set: 902 Inclination: 51.6422 deg RA of node: 19.1509 deg Eccentricity: .0007736 Arg of perigee: 159.5539 deg Mean anomaly: 200.5934 deg </pre> <p> Mean motion: 15.71358465 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 2997 Checksum: 325 </pre> <p> Coasting Arc #4 (Orbit 3012) </p><hr/> <p> Vector Time (GMT): 2010/210/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1718202.59 A = 6729422.56 meter Y = -4351186.72 meter E = .0014425 Z = -4847961.29 I = 51.70932 XDOT = 7295.871754 Wp = 104.67117 YDOT = -201.893970 meter/sec RA = 13.55218 deg ZDOT = -2414.120677 TA = 141.79554 MA = 141.69323 Ha = 196.109 n.mi Hp = 186.416 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -5637147.59 X = -1645869.01 Y = -14275546.98 feet Y = -4369996.01 meter Z = -15905384.81 Z = -4856132.70 XDOT = 23936.587121 XDOT = 7309.314282 YDOT = -662.381790 feet/sec YDOT = -120.231887 meter/sec ZDOT = -7920.343428 ZDOT = -2378.645306 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -8234257.24 X = -2509801.61 Y = 12912261.24 feet Y = 3935657.23 meter Z = -15938019.26 Z = -4857908.27 XDOT = -13775.723376 XDOT = -4198.840485 YDOT = -18347.559987 feet/sec YDOT = -5592.336284 meter/sec ZDOT = -7778.478224 ZDOT = -2370.880163 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10210.52002812 .00016717 00000-0 10270-3 0 9034 2 25544 51.6428 13.9464 0007696 162.2144 197.9288 15.71383182 30133 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10210.52002812 = yrday.fracday Element set: 903 Inclination: 51.6428 deg RA of node: 13.9464 deg Eccentricity: .0007696 Arg of perigee: 162.2144 deg Mean anomaly: 197.9288 deg </pre> <p> Mean motion: 15.71383182 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3013 Checksum: 291 </pre> <p> Coasting Arc #5 (Orbit 3028) </p><hr/> <p> Vector Time (GMT): 2010/211/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5920550.09 A = 6736212.59 meter Y = 1410107.92 meter E = .0017867 Z = 2861476.45 I = 51.70158 XDOT = -3551.465572 Wp = 122.42921 YDOT = -4578.343086 meter/sec RA = 8.39855 deg ZDOT = -5078.493356 TA = 24.74023 MA = 24.65466 Ha = 196.106 n.mi Hp = 186.705 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -19424376.95 X = -5949778.50 Y = 4626338.30 feet Y = 1343737.24 meter Z = 9388046.10 Z = 2832643.88 XDOT = -11651.789934 XDOT = -3475.335684 YDOT = -15020.810649 feet/sec YDOT = -4617.631818 meter/sec ZDOT = -16661.723610 ZDOT = -5095.561418 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15471528.13 X = 4715721.77 Y = 12707988.60 feet Y = 3873394.92 meter Z = 9272738.47 Z = 2826330.68 XDOT = -4040.545496 XDOT = -1231.558267 YDOT = 17159.447071 feet/sec YDOT = 5230.199467 meter/sec ZDOT = -16729.930024 ZDOT = -5099.282671 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10211.53755768 .00016717 00000-0 10270-3 0 9042 2 25544 51.6423 8.7406 0007692 167.3042 192.8315 15.71368007 30296 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10211.53755768 = yrday.fracday Element set: 904 Inclination: 51.6423 deg RA of node: 8.7406 deg Eccentricity: .0007692 Arg of perigee: 167.3042 deg Mean anomaly: 192.8315 deg </pre> <p> Mean motion: 15.71368007 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3029 Checksum: 302 </pre> <p> Coasting Arc #6 (Orbit 3044) </p><hr/> <p> Vector Time (GMT): 2010/212/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4337835.94 A = 6732834.31 meter Y = 3348907.03 meter E = .0015483 Z = 3908350.50 I = 51.66173 XDOT = -5882.049451 Wp = 128.05631 YDOT = 2866.879436 meter/sec RA = 3.33521 deg ZDOT = 4051.686861 TA = 279.69856 MA = 279.87341 Ha = 195.814 n.mi Hp = 186.738 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 14231745.20 X = 4281079.57 Y = 10987227.80 feet Y = 3397097.81 meter Z = 12822672.23 Z = 3929285.78 XDOT = -19298.062504 XDOT = -5933.352423 YDOT = 9405.772428 feet/sec YDOT = 2800.815824 meter/sec ZDOT = 13292.935896 ZDOT = 4022.987648 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -127284.93 X = -38796.45 Y = -17919056.55 feet Y = -5461728.44 meter Z = 12906350.39 Z = 3933855.60 XDOT = 18072.021443 XDOT = 5508.352136 YDOT = 9410.782346 feet/sec YDOT = 2868.406459 meter/sec ZDOT = 13178.152437 ZDOT = 4016.700863 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10212.55507786 .00016717 00000-0 10270-3 0 9051 2 25544 51.6432 3.5357 0007722 171.2386 188.8912 15.71416642 30458 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10212.55507786 = yrday.fracday Element set: 905 Inclination: 51.6432 deg RA of node: 3.5357 deg Eccentricity: .0007722 Arg of perigee: 171.2386 deg Mean anomaly: 188.8912 deg </pre> <p> Mean motion: 15.71416642 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3045 Checksum: 303 </pre> <p> Coasting Arc #7 (Orbit 3059) </p><hr/> <p> Vector Time (GMT): 2010/213/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4115211.54 A = 6732322.12 meter Y = -3395199.69 meter E = .0012864 Z = -4120154.45 I = 51.63041 XDOT = 6084.912859 Wp = 141.38263 YDOT = 2793.534815 meter/sec RA = 358.16976 deg ZDOT = 3772.075210 TA = 167.39289 MA = 167.36068 Ha = 195.789 n.mi Hp = 187.003 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 13501350.20 X = 4172886.27 Y = -11139106.59 feet Y = -3348858.26 meter Z = -13517567.10 Z = -4100022.95 XDOT = 19963.624867 XDOT = 6034.898856 YDOT = 9165.140469 feet/sec YDOT = 2861.300125 meter/sec ZDOT = 12375.574837 ZDOT = 3801.514179 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -17216897.16 X = -5247710.26 Y = -3480688.69 feet Y = -1060913.91 meter Z = -13437039.53 Z = -4095609.65 XDOT = -5726.319508 XDOT = -1745.382186 YDOT = -19949.977308 feet/sec YDOT = -6080.753084 meter/sec ZDOT = 12493.255185 ZDOT = 3807.944180 </pre> <p> The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time </p><p><strong>TWO LINE MEAN ELEMENT SET</strong> </p><p><strong>ISS</strong><br/> 1 25544U 98067A 10213.50899645 .00016717 00000-0 10270-3 0 9066 2 25544 51.6443 358.6566 0007655 173.9550 186.1705 15.71404052 30603 </p><p> Satellite: ISS<br/> Catalog Number: 25544 </p><pre> Epoch time: 10213.50899645 = yrday.fracday Element set: 906 Inclination: 51.6443 deg RA of node: 358.6566 deg Eccentricity: .0007655 Arg of perigee: 173.9550 deg Mean anomaly: 186.1705 deg </pre> <p> Mean motion: 15.71404052 rev/day Decay rate: 1.67170E-04 rev/day^2 </p><pre> Epoch rev: 3060 Checksum: 313 </pre> <p> Coasting Arc #8 (Orbit 3075) </p><hr/> <p> Vector Time (GMT): 2010/214/12:00:00.000 Vector Time (MET): N/A<br/> Weight (LBS) : 828730.9 </p><pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -6049016.24 A = 6736444.56 meter Y = -1360457.74 meter E = .0011284 Z = -2622243.02 I = 51.61443 XDOT = 3293.031267