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Date:
July 31st 2010
<B> ISS TRAJECTORY DATA</B>
Lift off time (UTC) : N/A
Area (sq ft) : 9149.32
Drag Coefficient (Cd) : 2.00
Monthly MSFC 50% solar flux (F10.7-jansky) : 74.8
Monthly MSFC 50% earth geomagnetic index (Kp) : 0.74
ET - UTC (sec) : 66.18
UT1 - UTC (sec) : 0.00
Maneuvers contained within the current ephemeris are as follows:
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
There are no maneuvers.
Coasting Arc #1 (Orbit 3028)
Vector Time (GMT): 2010/211/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
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
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
TWO LINE MEAN ELEMENT SET
ISS
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
Satellite: ISS
Catalog Number: 25544
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
Mean motion: 15.71333273 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3029
Checksum: 288
Coasting Arc #2 (Orbit 3044)
Vector Time (GMT): 2010/212/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
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
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
TWO LINE MEAN ELEMENT SET
ISS
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
Satellite: ISS
Catalog Number: 25544
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
Mean motion: 15.71382511 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3045
Checksum: 287
Coasting Arc #3 (Orbit 3059)
Vector Time (GMT): 2010/213/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
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
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
TWO LINE MEAN ELEMENT SET
ISS
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
Satellite: ISS
Catalog Number: 25544
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
Mean motion: 15.71370390 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3060
Checksum: 309
Coasting Arc #4 (Orbit 3075)
Vector Time (GMT): 2010/214/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
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
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
TWO LINE MEAN ELEMENT SET
ISS
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
Satellite: ISS
Catalog Number: 25544
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
Mean motion: 15.71393501 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3076
Checksum: 296
Coasting Arc #5 (Orbit 3091)
Vector Time (GMT): 2010/215/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
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
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
TWO LINE MEAN ELEMENT SET
ISS
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
Satellite: ISS
Catalog Number: 25544
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
Mean motion: 15.71367854 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3092
Checksum: 298
Coasting Arc #6 (Orbit 3107)
Vector Time (GMT): 2010/216/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
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
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
TWO LINE MEAN ELEMENT SET
ISS
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
Satellite: ISS
Catalog Number: 25544
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
Mean motion: 15.71429694 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3108
Checksum: 318
Coasting Arc #7 (Orbit 3122)
Vector Time (GMT): 2010/217/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
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
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
TWO LINE MEAN ELEMENT SET
ISS
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
Satellite: ISS
Catalog Number: 25544
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
Mean motion: 15.71451001 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3123
Checksum: 287
Coasting Arc #8 (Orbit 3138)
Vector Time (GMT): 2010/218/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
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
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
TWO LINE MEAN ELEMENT SET
ISS
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
Satellite: ISS
Catalog Number: 25544
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
Mean motion: 15.71439190 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3139
Checksum: 332
Coasting Arc #9 (Orbit 3154)
Vector Time (GMT): 2010/219/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
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
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
TWO LINE MEAN ELEMENT SET
ISS
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
Satellite: ISS
Catalog Number: 25544
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
Mean motion: 15.71494074 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3155
Checksum: 323
Coasting Arc #10 (Orbit 3169)
Vector Time (GMT): 2010/220/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
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
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
TWO LINE MEAN ELEMENT SET
ISS
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
Satellite: ISS
Catalog Number: 25544
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
Mean motion: 15.71446669 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3170
Checksum: 311
Coasting Arc #11 (Orbit 3185)
Vector Time (GMT): 2010/221/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
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
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
TWO LINE MEAN ELEMENT SET
ISS
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
Satellite: ISS
Catalog Number: 25544
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
Mean motion: 15.71473815 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3186
Checksum: 292
Coasting Arc #12 (Orbit 3201)
Vector Time (GMT): 2010/222/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
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
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
TWO LINE MEAN ELEMENT SET
ISS
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
Satellite: ISS
Catalog Number: 25544
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
Mean motion: 15.71495421 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3202
Checksum: 313
Coasting Arc #13 (Orbit 3217)
Vector Time (GMT): 2010/223/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
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
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
TWO LINE MEAN ELEMENT SET
ISS
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
Satellite: ISS
Catalog Number: 25544
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
Mean motion: 15.71531311 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3218
Checksum: 280
Coasting Arc #14 (Orbit 3232)
Vector Time (GMT): 2010/224/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
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
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
TWO LINE MEAN ELEMENT SET
ISS
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
Satellite: ISS
Catalog Number: 25544
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
Mean motion: 15.71554390 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3233
Checksum: 287
Coasting Arc #15 (Orbit 3248)
Vector Time (GMT): 2010/225/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
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
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
TWO LINE MEAN ELEMENT SET
ISS
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
Satellite: ISS
Catalog Number: 25544
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
Mean motion: 15.71532026 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3249
Checksum: 293
INTERNATIONAL SPACE STATION ORBITAL DATA:
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:
NASA Orbital Flight Dynamics
DOD C-Band Radar Network
Goddard Space Flight Center (GSFC)
NASA Johnson Space Center (JSC)
DoD/ USSTRATCOM/ US Space Command with permission
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.
David Cottle
Director Of Engineering
IDB Communications
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