[ISSTLE LIST]

[ISSTLE LIST] Current ISS TLEs @ 18:30 UTC

Tue, 07 Feb 2012 18:30:00 GMT

ISS TRAJECTORY DATA Lift off time (UTC) : N/A Area (sq ft) : 10494.81 Drag Coefficient (Cd) : 2.00 Monthly MSFC 50% solar flux (F10.7-jansky) : 119.7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2.152 ET - UTC (sec) : 66.18 UT1 - UTC (sec) : 0.00 Maneuvers contained within the current ephemeris are as follows: <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. Coasting Arc #1 (Orbit 3748) <hr/> Vector Time (GMT): 2012/037/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 2984041.49 A = 6776056.96 meter Y = 6055296.30 meter E = .0031779 Z = 274415.38 I = 51.96907 XDOT = -4367.366738 Wp = 25.87687 YDOT = 1867.440426 meter/sec RA = 61.94397 deg ZDOT = 6050.552461 TA = 337.07891 MA = 337.22042 Ha = 220.217 n.mi Hp = 202.634 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 9790162.36 X = 2914775.16 Y = 19866457.69 feet Y = 6088278.40 meter Z = 900312.93 Z = 288743.08 XDOT = -14328.631030 XDOT = -4417.315635 YDOT = 6126.773050 feet/sec YDOT = 1818.322550 meter/sec ZDOT = 19850.893900 ZDOT = 6029.215267 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -7040933.36 X = -2146076.49 Y = 20996198.94 feet Y = 6399641.44 meter Z = 958577.63 Z = 292174.46 XDOT = -13043.440210 XDOT = -3975.640576 YDOT = -5309.195515 feet/sec YDOT = -1618.242793 meter/sec ZDOT = 19763.242165 ZDOT = 6023.836212 </pre> 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 12037.56355562 .00016717 00000-0 10270-3 0 9007 2 25544 51.6409 62.2910 0020603 12.8885 347.2793 15.58699571 37494 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12037.56355562 = yrday.fracday Element set: 900 Inclination: 51.6409 deg RA of node: 62.2910 deg Eccentricity: .0020603 Arg of perigee: 12.8885 deg Mean anomaly: 347.2793 deg </pre> Mean motion: 15.58699571 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3749 Checksum: 325 </pre> Coasting Arc #2 (Orbit 3763) <hr/> Vector Time (GMT): 2012/038/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -740031.31 A = 6771328.82 meter Y = -5881766.55 meter E = .0021950 Z = -3302506.74 I = 51.93808 XDOT = 5690.498137 Wp = 28.26123 YDOT = 1947.107631 meter/sec RA = 56.96611 deg ZDOT = -4736.976557 TA = 189.91713 MA = 189.96052 Ha = 220.246 n.mi Hp = 202.414 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -2427924.24 X = -658162.84 Y = -19297134.35 feet Y = -5889584.36 meter Z = -10834995.86 Z = -3305902.68 XDOT = 18669.613310 XDOT = 5691.312762 YDOT = 6388.148396 feet/sec YDOT = 2010.746729 meter/sec ZDOT = -15541.261671 ZDOT = -4709.331239 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 11644782.05 X = 3549329.57 Y = -15568611.29 feet Y = -4745312.72 meter Z = -10848444.09 Z = -3306605.76 XDOT = 7994.660364 XDOT = 2436.772479 YDOT = 16743.835614 feet/sec YDOT = 5103.521095 meter/sec ZDOT = -15428.049453 ZDOT = -4702.469473 </pre> 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 12038.52524298 .00016717 00000-0 10270-3 0 9019 2 25544 51.6405 57.4626 0020537 16.5385 343.6436 15.58734358 37646 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12038.52524298 = yrday.fracday Element set: 901 Inclination: 51.6405 deg RA of node: 57.4626 deg Eccentricity: .0020537 Arg of perigee: 16.5385 deg Mean anomaly: 343.6436 deg </pre> Mean motion: 15.58734358 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3764 Checksum: 319 </pre> Coasting Arc #3 (Orbit 3779) <hr/> Vector Time (GMT): 2012/039/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1968227.37 A = 6764839.28 meter Y = 3970583.54 meter E = .0019903 Z = 5097275.01 I = 51.89790 XDOT = -5605.302539 Wp = 34.42936 YDOT = -4972.121843 meter/sec RA = 51.95345 deg ZDOT = 1721.471175 TA = 39.11039 MA = 38.96669 Ha = 220.447 n.mi Hp = 202.116 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -6457438.86 X = -2037241.68 Y = 13026848.88 feet Y = 3948187.97 meter Z = 16723343.20 Z = 5087545.89 XDOT = -18390.100192 XDOT = -5557.648969 YDOT = -16312.735705 feet/sec YDOT = -5034.537262 meter/sec ZDOT = 5647.871309 ZDOT = 1694.357600 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13662945.44 X = -4164465.77 Y = 5105377.93 feet Y = 1556119.19 meter Z = 16683121.84 Z = 5085015.54 XDOT = -2067.697746 XDOT = -630.234273 YDOT = -23490.141875 feet/sec YDOT = -7159.795244 meter/sec ZDOT = 5537.087500 ZDOT = 1687.704270 </pre> 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 12039.55102962 .00016717 00000-0 10270-3 0 9024 2 25544 51.6394 52.3119 0020593 20.4942 339.7035 15.58751098 37808 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12039.55102962 = yrday.fracday Element set: 902 Inclination: 51.6394 deg RA of node: 52.3119 deg Eccentricity: .0020593 Arg of perigee: 20.4942 deg Mean anomaly: 339.7035 deg </pre> Mean motion: 15.58751098 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3780 Checksum: 306 </pre> Coasting Arc #4 (Orbit 3794) <hr/> Vector Time (GMT): 2012/040/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4358646.89 A = 6765151.27 meter Y = -1149495.45 meter E = .0026059 Z = -5057919.79 I = 51.87979 XDOT = 3866.666804 Wp = 52.78496 YDOT = 6334.873846 meter/sec RA = 46.92298 deg ZDOT = 1914.492512 TA = 235.60339 MA = 235.85006 Ha = 220.497 n.mi Hp = 202.019 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 14300022.61 X = 4395746.49 Y = -3771310.54 feet Y = -1100547.27 meter Z = -16594225.04 Z = -5036656.00 XDOT = 12685.914710 XDOT = 3786.241644 YDOT = 20783.706845 feet/sec YDOT = 6377.663742 meter/sec ZDOT = 6281.143413 ZDOT = 1933.080391 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13249207.76 X = 4038358.53 Y = 6786853.15 feet Y = 2068632.84 meter Z = -16506933.46 Z = -5031313.32 XDOT = -3930.953729 XDOT = -1198.154697 YDOT = 22957.688028 feet/sec YDOT = 6997.503311 meter/sec ZDOT = 6356.849244 ZDOT = 1937.567650 </pre> 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 12040.51269074 .00016717 00000-0 10270-3 0 9031 2 25544 51.6400 47.4847 0020604 23.6687 336.5412 15.58751826 37952 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12040.51269074 = yrday.fracday Element set: 903 Inclination: 51.6400 deg RA of node: 47.4847 deg Eccentricity: .0020604 Arg of perigee: 23.6687 deg Mean anomaly: 336.5412 deg </pre> Mean motion: 15.58751826 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3795 Checksum: 307 </pre> Coasting Arc #5 (Orbit 3810) <hr/> Vector Time (GMT): 2012/041/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5722341.80 A = 6771687.31 meter Y = -1857799.81 meter E = .0028274 Z = 3109194.49 I = 51.88002 XDOT = -781.284515 Wp = 52.37763 YDOT = -5858.259960 meter/sec RA = 41.90924 deg ZDOT = -4891.113989 TA = 91.92031 MA = 91.59647 Ha = 220.512 n.mi Hp = 201.651 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -18774087.28 X = -5716245.69 Y = -6095143.74 feet Y = -1921756.25 meter Z = 10200769.34 Z = 3081411.10 XDOT = -2563.269407 XDOT = -691.958739 YDOT = -19220.012992 feet/sec YDOT = -5866.497677 meter/sec ZDOT = -16046.961905 ZDOT = -4894.691963 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -10271161.07 X = -3130649.89 Y = -16924202.25 feet Y = -5158496.84 meter Z = 10086994.30 Z = 3074515.86 XDOT = 9463.348985 XDOT = 2884.428771 YDOT = -15409.219424 feet/sec YDOT = -4696.730081 meter/sec ZDOT = -16061.150736 ZDOT = -4895.438744 </pre> 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 12041.53844747 .00016717 00000-0 10270-3 0 9041 2 25544 51.6392 42.3334 0020720 27.4046 332.8197 15.58826544 38115 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12041.53844747 = yrday.fracday Element set: 904 Inclination: 51.6392 deg RA of node: 42.3334 deg Eccentricity: .0020720 Arg of perigee: 27.4046 deg Mean anomaly: 332.8197 deg </pre> Mean motion: 15.58826544 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3811 Checksum: 300 </pre> Coasting Arc #6 (Orbit 3825) <hr/> Vector Time (GMT): 2012/042/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 5436669.17 A = 6775615.50 meter Y = 4013555.28 meter E = .0032384 Z = -73994.74 I = 51.87052 XDOT = -2778.896938 Wp = 36.20674 YDOT = 3850.569800 meter/sec RA = 36.92860 deg ZDOT = 6048.558173 TA = 322.99572 MA = 323.21863 Ha = 220.457 n.mi Hp = 201.342 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 17836841.12 X = 5391744.17 Y = 13167832.27 feet Y = 4074100.27 meter Z = -242764.89 Z = -47693.44 XDOT = -9117.115938 XDOT = -2851.130347 YDOT = 12633.103020 feet/sec YDOT = 3819.091005 meter/sec ZDOT = 19844.350962 ZDOT = 6034.882898 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 5264004.57 X = 1604468.59 Y = 21537771.59 feet Y = 6564712.78 meter Z = -135253.47 Z = -41225.26 XDOT = -13615.709710 XDOT = -4150.068319 YDOT = 3401.562184 feet/sec YDOT = 1036.796154 meter/sec ZDOT = 19787.955909 ZDOT = 6031.368961 </pre> 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 12042.50008200 .00016717 00000-0 10270-3 0 9056 2 25544 51.6395 37.5064 0020526 31.5183 328.7197 15.58862410 38268 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12042.50008200 = yrday.fracday Element set: 905 Inclination: 51.6395 deg RA of node: 37.5064 deg Eccentricity: .0020526 Arg of perigee: 31.5183 deg Mean anomaly: 328.7197 deg </pre> Mean motion: 15.58862410 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3826 Checksum: 288 </pre> Coasting Arc #7 (Orbit 3841) <hr/> Vector Time (GMT): 2012/043/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3443914.52 A = 6771630.11 meter Y = -4982816.19 meter E = .0022574 Z = -3061001.50 I = 51.83187 XDOT = 5775.182720 Wp = 45.51565 YDOT = -966.652534 meter/sec RA = 31.94493 deg ZDOT = -4931.072248 TA = 169.49200 MA = 169.44475 Ha = 220.629 n.mi Hp = 201.127 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -11298932.17 X = -3373070.23 Y = -16347822.15 feet Y = -5020932.22 meter Z = -10042655.83 Z = -3077559.33 XDOT = 18947.449869 XDOT = 5809.516561 YDOT = -3171.432197 feet/sec YDOT = -901.879183 meter/sec ZDOT = -16178.058555 ZDOT = -4902.933545 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 1501714.35 X = 457722.53 Y = -19781362.48 feet Y = -6029359.28 meter Z = -10110125.90 Z = -3081566.37 XDOT = 15380.467160 XDOT = 4687.966390 YDOT = 9365.444842 feet/sec YDOT = 2854.587588 meter/sec ZDOT = -16062.601527 ZDOT = -4895.880945 </pre> 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 12043.52581012 .00016717 00000-0 10270-3 0 9067 2 25544 51.6392 32.3551 0020735 35.0625 325.1891 15.58839468 38428 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12043.52581012 = yrday.fracday Element set: 906 Inclination: 51.6392 deg RA of node: 32.3551 deg Eccentricity: .0020735 Arg of perigee: 35.0625 deg Mean anomaly: 325.1891 deg </pre> Mean motion: 15.58839468 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3842 Checksum: 299 </pre> Coasting Arc #8 (Orbit 3857) <hr/> Vector Time (GMT): 2012/044/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 212081.97 A = 6764834.62 meter Y = 4526723.30 meter E = .0021864 Z = 5003610.14 I = 51.78289 XDOT = -7184.518763 Wp = 53.11009 YDOT = -1875.703037 meter/sec RA = 26.92800 deg ZDOT = 2008.270040 TA = 17.51890 MA = 17.44360 Ha = 220.664 n.mi Hp = 200.965 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 695806.98 X = 137141.32 Y = 14851454.41 feet Y = 4528676.09 meter Z = 16416043.76 Z = 5004458.23 XDOT = -23571.255784 XDOT = -7172.765929 YDOT = -6153.881356 feet/sec YDOT = -1955.978971 meter/sec ZDOT = 6588.812466 ZDOT = 1973.396942 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -8644745.39 X = -2634918.40 Y = 12092013.44 feet Y = 3685645.70 meter Z = 16419132.94 Z = 5004551.72 XDOT = -13982.610393 XDOT = -4261.899648 YDOT = -18718.682701 feet/sec YDOT = -5705.454487 meter/sec ZDOT = 6445.989410 ZDOT = 1964.737572 </pre> 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 12044.55152172 .00016717 00000-0 10270-3 0 9073 2 25544 51.6391 27.2052 0020674 38.3649 321.8972 15.58868107 38582 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12044.55152172 = yrday.fracday Element set: 907 Inclination: 51.6391 deg RA of node: 27.2052 deg Eccentricity: .0020674 Arg of perigee: 38.3649 deg Mean anomaly: 321.8972 deg </pre> Mean motion: 15.58868107 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3858 Checksum: 319 </pre> Coasting Arc #9 (Orbit 3872) <hr/> Vector Time (GMT): 2012/045/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3237277.26 A = 6764556.30 meter Y = -3047231.10 meter E = .0029675 Z = -5118396.60 I = 51.75431 XDOT = 6337.813193 Wp = 64.83263 YDOT = 3963.628183 meter/sec RA = 21.88767 deg ZDOT = 1668.650175 TA = 221.16059 MA = 221.38477 Ha = 220.745 n.mi Hp = 200.855 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 10620988.39 X = 3295975.14 Y = -9997477.36 feet Y = -3010701.74 meter Z = -16792639.76 Z = -5102527.62 XDOT = 20793.350371 XDOT = 6284.914233 YDOT = 13004.029471 feet/sec YDOT = 4034.205764 meter/sec ZDOT = 5474.574065 ZDOT = 1699.310092 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 14577340.20 X = 4443173.29 Y = -1563941.61 feet Y = -476689.40 meter Z = -16727311.12 Z = -5098484.43 XDOT = 8689.312574 XDOT = 2648.502472 YDOT = 21797.029204 feet/sec YDOT = 6643.734501 meter/sec ZDOT = 5599.937214 ZDOT = 1706.860863 </pre> 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 12045.51311243 .00016717 00000-0 10270-3 0 9087 2 25544 51.6393 22.3771 0020727 42.0422 318.2319 15.58864690 38733 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12045.51311243 = yrday.fracday Element set: 908 Inclination: 51.6393 deg RA of node: 22.3771 deg Eccentricity: .0020727 Arg of perigee: 42.0422 deg Mean anomaly: 318.2319 deg </pre> Mean motion: 15.58864690 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3873 Checksum: 294 </pre> Coasting Arc #10 (Orbit 3888) <hr/> Vector Time (GMT): 2012/046/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5869052.12 A = 6771037.83 meter Y = 896200.56 meter E = .0030844 Z = 3247307.30 I = 51.74778 XDOT = -3418.196247 Wp = 62.96398 YDOT = -4958.345009 meter/sec RA = 16.86289 deg ZDOT = -4761.022185 TA = 79.36945 MA = 79.02222 Ha = 220.762 n.mi Hp = 200.602 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -19255420.34 X = -5894411.87 Y = 2940290.54 feet Y = 830427.40 meter Z = 10653895.34 Z = 3218734.53 XDOT = -11214.554615 XDOT = -3339.369360 YDOT = -16267.536118 feet/sec YDOT = -4996.128632 meter/sec ZDOT = -15620.151527 ZDOT = -4777.435926 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -17375973.28 X = -5296196.65 Y = -8942942.36 feet Y = -2725808.83 meter Z = 10536666.52 Z = 3211575.96 XDOT = -123.897987 XDOT = -37.764106 YDOT = -18431.316772 feet/sec YDOT = -5617.865352 meter/sec ZDOT = -15687.013566 ZDOT = -4781.401735 </pre> 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 12046.53879267 .00016717 00000-0 10270-3 0 9096 2 25544 51.6392 17.2261 0020740 45.5461 314.7387 15.58922764 38895 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12046.53879267 = yrday.fracday Element set: 909 Inclination: 51.6392 deg RA of node: 17.2261 deg Eccentricity: .0020740 Arg of perigee: 45.5461 deg Mean anomaly: 314.7387 deg </pre> Mean motion: 15.58922764 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3889 Checksum: 335 </pre> Coasting Arc #11 (Orbit 3903) <hr/> Vector Time (GMT): 2012/047/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6646760.26 A = 6775347.32 meter Y = 1217517.98 meter E = .0032460 Z = -222896.44 I = 51.73324 XDOT = -681.150152 Wp = 47.09993 YDOT = 4717.401696 meter/sec RA = 11.87104 deg ZDOT = 6030.127622 TA = 310.49352 MA = 310.77594 Ha = 220.733 n.mi Hp = 200.328 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 21806956.25 X = 6633734.49 Y = 3994481.56 feet Y = 1291773.32 meter Z = -731287.54 Z = -190639.04 XDOT = -2234.744592 XDOT = -763.142891 YDOT = 15477.039685 feet/sec YDOT = 4709.326175 meter/sec ZDOT = 19783.883275 ZDOT = 6026.619561 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15602023.26 X = 4755496.69 Y = 15756011.89 feet Y = 4802432.42 meter Z = -599136.59 Z = -182616.83 XDOT = -9638.742679 XDOT = -2937.888769 YDOT = 10208.822806 feet/sec YDOT = 3111.649191 meter/sec ZDOT = 19769.083511 ZDOT = 6025.616654 </pre> 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 12047.50035354 .00016717 00000-0 10270-3 0 9107 2 25544 51.6393 12.3983 0020711 49.5775 310.7183 15.58948940 39045 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12047.50035354 = yrday.fracday Element set: 910 Inclination: 51.6393 deg RA of node: 12.3983 deg Eccentricity: .0020711 Arg of perigee: 49.5775 deg Mean anomaly: 310.7183 deg </pre> Mean motion: 15.58948940 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3904 Checksum: 306 </pre> Coasting Arc #12 (Orbit 3919) <hr/> Vector Time (GMT): 2012/048/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5304433.97 A = 6771429.60 meter Y = -3008078.23 meter E = .0023512 Z = -2976179.95 I = 51.69150 XDOT = 4713.591638 Wp = 61.71191 YDOT = -3398.360938 meter/sec RA = 6.87832 deg ZDOT = -4985.367833 TA = 152.27206 MA = 152.14651 Ha = 220.736 n.mi Hp = 200.112 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -17402998.58 X = -5255945.53 Y = -9869023.05 feet Y = -3067124.57 meter Z = -9764369.92 Z = -3001830.25 XDOT = 15464.539496 XDOT = 4775.459678 YDOT = -11149.478143 feet/sec YDOT = -3345.304738 meter/sec ZDOT = -16356.193678 ZDOT = -4962.319689 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -8885028.32 X = -2708156.63 Y = -17867809.01 feet Y = -5446108.19 meter Z = -9869273.95 Z = -3008154.70 XDOT = 17834.240293 XDOT = 5435.876441 YDOT = 79.326650 feet/sec YDOT = 24.178763 meter/sec ZDOT = -16261.393468 ZDOT = -4956.472729 </pre> 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 12048.52600190 .00016717 00000-0 10270-3 0 9117 2 25544 51.6402 7.2467 0020762 52.9217 307.3832 15.58972896 39209 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12048.52600190 = yrday.fracday Element set: 911 Inclination: 51.6402 deg RA of node: 7.2467 deg Eccentricity: .0020762 Arg of perigee: 52.9217 deg Mean anomaly: 307.3832 deg </pre> Mean motion: 15.58972896 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3920 Checksum: 300 </pre> Coasting Arc #13 (Orbit 3935) <hr/> Vector Time (GMT): 2012/049/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 2190247.08 A = 6764468.30 meter Y = 4006220.12 meter E = .0023484 Z = 4969545.83 I = 51.63874 XDOT = -7275.200294 Wp = 69.56063 YDOT = 1406.290118 meter/sec RA = 1.85196 deg ZDOT = 2072.887892 TA = .34518 MA = .34356 Ha = 220.592 n.mi Hp = 200.043 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 7185850.00 X = 2121145.67 Y = 13143766.80 feet Y = 4030326.54 meter Z = 16304284.23 Z = 4980017.74 XDOT = -23868.767370 XDOT = -7300.454349 YDOT = 4613.812723 feet/sec YDOT = 1324.793179 meter/sec ZDOT = 6800.813294 ZDOT = 2037.484909 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -1198010.22 X = -365153.51 Y = 14885206.93 feet Y = 4537011.07 meter Z = 16346868.70 Z = 4982525.58 XDOT = -21490.747719 XDOT = -6550.379905 YDOT = -9038.192936 feet/sec YDOT = -2754.841207 meter/sec ZDOT = 6655.533130 ZDOT = 2028.606498 </pre> 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 12049.55163226 .00016717 00000-0 10270-3 0 9126 2 25544 51.6407 2.0969 0020527 56.6661 303.6456 15.59024869 39364 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12049.55163226 = yrday.fracday Element set: 912 Inclination: 51.6407 deg RA of node: 2.0969 deg Eccentricity: .0020527 Arg of perigee: 56.6661 deg Mean anomaly: 303.6456 deg </pre> Mean motion: 15.59024869 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3936 Checksum: 314 </pre> Coasting Arc #14 (Orbit 3950) <hr/> Vector Time (GMT): 2012/050/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 1622704.49 A = 6764149.17 meter Y = -4149548.00 meter E = .0031849 Z = -5114224.55 I = 51.60694 XDOT = 7422.527745 Wp = 76.23003 YDOT = 892.217175 meter/sec RA = 356.79939 deg ZDOT = 1647.213404 TA = 209.61397 MA = 209.79469 Ha = 220.744 n.mi Hp = 199.953 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 5323833.62 X = 1693827.98 Y = -13614002.63 feet Y = -4131004.45 meter Z = -16778951.93 Z = -5106168.84 XDOT = 24352.125147 XDOT = 7403.997581 YDOT = 2927.221704 feet/sec YDOT = 975.116915 meter/sec ZDOT = 5404.243453 ZDOT = 1683.225604 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 11807873.00 X = 3599039.69 Y = -8682038.41 feet Y = -2646285.31 meter Z = -16745561.92 Z = -5104047.27 XDOT = 18453.473291 XDOT = 5624.618659 YDOT = 14490.840352 feet/sec YDOT = 4416.808139 meter/sec ZDOT = 5551.818421 ZDOT = 1692.194255 </pre> 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 12050.51314791 .00016717 00000-0 10270-3 0 9130 2 25544 51.6409 357.2676 0020643 60.1038 300.2164 15.59002087 39517 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12050.51314791 = yrday.fracday Element set: 913 Inclination: 51.6409 deg RA of node: 357.2676 deg Eccentricity: .0020643 Arg of perigee: 60.1038 deg Mean anomaly: 300.2164 deg </pre> Mean motion: 15.59002087 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3951 Checksum: 281 </pre> Coasting Arc #15 (Orbit 3966) <hr/> Vector Time (GMT): 2012/051/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4951127.82 A = 6770734.91 meter Y = 3294616.64 meter E = .0032453 Z = 3218989.23 I = 51.59969 XDOT = -5177.937394 Wp = 74.71733 YDOT = -3071.918160 meter/sec RA = 351.76382 deg ZDOT = -4771.635423 TA = 67.88098 MA = 67.53678 Ha = 220.775 n.mi Hp = 199.789 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -16243857.68 X = -5003237.58 Y = 10809109.70 feet Y = 3238958.91 meter Z = 10560988.30 Z = 3194810.81 XDOT = -16987.983577 XDOT = -5120.022901 YDOT = -10078.471655 feet/sec YDOT = -3129.497526 meter/sec ZDOT = -15654.971859 ZDOT = -4796.648015 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -19545211.27 X = -5957380.40 Y = 880009.00 feet Y = 268226.74 meter Z = 10461574.42 Z = 3188687.88 XDOT = -9236.246307 XDOT = -2815.207874 YDOT = -15908.418138 feet/sec YDOT = -4848.885848 meter/sec ZDOT = -15757.258004 ZDOT = -4802.812240 </pre> 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 12051.53874666 .00016717 00000-0 10270-3 0 9146 2 25544 51.6416 352.1166 0020661 63.8897 296.4381 15.59047410 39679 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12051.53874666 = yrday.fracday Element set: 914 Inclination: 51.6416 deg RA of node: 352.1166 deg Eccentricity: .0020661 Arg of perigee: 63.8897 deg Mean anomaly: 296.4381 deg </pre> Mean motion: 15.59047410 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3967 Checksum: 329</pre> <hr/> 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. <pre> David Cottle Director Of Engineering IDB Communications</pre> <hr/> The following information is a reminder of your current mailing list subscription: You are subscribed to the following list: [ISSTLE LIST] using the following email: <a href="mailto:example@example.com">example@example.com</a> You may automatically unsubscribe from this list at any time by visiting the following URL: <<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>> If the above URL is inoperable, make sure that you have copied the entire address. Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism. You may also change your subscription by visiting this list's main screen: <<a href="http://www.aus-city.com/cgi-bin/dada/mail.cgi/list/ISSTLE_LIST">http://www.aus-city.com/cgi-bin/dada/mail.cgi/list/ISSTLE_LIST</a>> If you're still having trouble, please contact the list owner at: <mailto:<a href="mailto:list.admin@aus-city.com">list.admin@aus-city.com</a>> The following physical address is associated with this mailing list: <a href="http://www.aus-city.com">http://www.aus-city.com</a>

[ISSTLE LIST] Current ISS TLEs @ 06:30 UTC

Tue, 07 Feb 2012 06:30:00 GMT

[ISSTLE LIST] Current ISS TLEs @ 18:30 UTC

Mon, 06 Feb 2012 18:30:00 GMT

[ISSTLE LIST] Current ISS TLEs @ 06:30 UTC

Mon, 06 Feb 2012 06:30:00 GMT

ISS TRAJECTORY DATA Lift off time (UTC) : N/A Area (sq ft) : 10979.19 Drag Coefficient (Cd) : 2.00 Monthly MSFC 50% solar flux (F10.7-jansky) : 119.7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2.152 ET - UTC (sec) : 66.18 UT1 - UTC (sec) : 0.00 Maneuvers contained within the current ephemeris are as follows: <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. Coasting Arc #1 (Orbit 3701) <hr/> Vector Time (GMT): 2012/034/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3667057.92 A = 6764650.21 meter Y = 2247285.80 meter E = .0018467 Z = 5214974.97 I = 51.96161 XDOT = -2635.417598 Wp = 11.62583 YDOT = -7110.375691 meter/sec RA = 76.94051 deg ZDOT = 1227.785041 TA = 66.76277 MA = 66.56842 Ha = 219.888 n.mi Hp = 203.505 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -12031029.93 X = -3717247.70 Y = 7372984.89 feet Y = 2205997.67 meter Z = 17109497.92 Z = 5197039.06 XDOT = -8646.383194 XDOT = -2561.676280 YDOT = -23328.004235 feet/sec YDOT = -7139.434290 meter/sec ZDOT = 4028.166145 ZDOT = 1215.161362 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13619608.08 X = -4151256.54 Y = -4016221.84 feet Y = -1224144.42 meter Z = 17035778.37 Z = 5192505.25 XDOT = 11131.879492 XDOT = 3392.996869 YDOT = -21116.585630 feet/sec YDOT = -6436.335300 meter/sec ZDOT = 3976.966266 ZDOT = 1212.179318 </pre> 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 12034.55019472 .00016717 00000-0 10270-3 0 9000 2 25544 51.6407 77.4144 0020358 1.3772 358.7436 15.58661152 37028 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12034.55019472 = yrday.fracday Element set: 900 Inclination: 51.6407 deg RA of node: 77.4144 deg Eccentricity: .0020358 Arg of perigee: 1.3772 deg Mean anomaly: 358.7436 deg </pre> Mean motion: 15.58661152 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3702 Checksum: 292 </pre> Coasting Arc #2 (Orbit 3716) <hr/> Vector Time (GMT): 2012/035/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4470246.89 A = 6766011.83 meter Y = 1302198.87 meter E = .0021464 Z = -4914404.46 I = 51.95903 XDOT = 441.595210 Wp = 38.06095 YDOT = 7287.467865 meter/sec RA = 71.91611 deg ZDOT = 2354.583594 TA = 254.75811 MA = 254.99552 Ha = 220.038 n.mi Hp = 203.303 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 14666164.35 X = 4479225.76 Y = 4272306.00 feet Y = 1352238.30 meter Z = -16123374.20 Z = -4892666.81 XDOT = 1448.803182 XDOT = 348.634676 YDOT = 23909.015304 feet/sec YDOT = 7291.886198 meter/sec ZDOT = 7725.011792 ZDOT = 2356.503266 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 7009313.80 X = 2136438.85 Y = 13677775.36 feet Y = 4168985.93 meter Z = -16034342.90 Z = -4887267.72 XDOT = -15451.097658 XDOT = -4709.494566 YDOT = 16897.902741 feet/sec YDOT = 5150.480755 meter/sec ZDOT = 7732.301048 ZDOT = 2356.805359 </pre> 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 12035.51191994 .00016717 00000-0 10270-3 0 9018 2 25544 51.6416 72.5874 0020468 4.9178 355.2174 15.58656749 37178 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12035.51191994 = yrday.fracday Element set: 901 Inclination: 51.6416 deg RA of node: 72.5874 deg Eccentricity: .0020468 Arg of perigee: 4.9178 deg Mean anomaly: 355.2174 deg </pre> Mean motion: 15.58656749 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3717 Checksum: 330 </pre> Coasting Arc #3 (Orbit 3732) <hr/> Vector Time (GMT): 2012/036/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4279558.50 A = 6772736.16 meter Y = -4443199.80 meter E = .0024256 Z = 2805988.85 I = 51.97057 XDOT = 2104.812043 Wp = 42.44820 YDOT = -5294.300381 meter/sec RA = 66.91394 deg ZDOT = -5129.971998 TA = 105.84124 MA = 105.57371 Ha = 220.044 n.mi Hp = 202.953 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -14040546.26 X = -4243186.20 Y = -14577427.16 feet Y = -4490853.15 meter Z = 9206000.16 Z = 2785287.71 XDOT = 6905.551323 XDOT = 2188.777150 YDOT = -17369.751907 feet/sec YDOT = -5270.293483 meter/sec ZDOT = -16830.616791 ZDOT = -5119.543354 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 603545.30 X = 183960.61 Y = -20268776.27 feet Y = -6177923.01 meter Z = 9121469.31 Z = 2780223.84 XDOT = 15853.820029 XDOT = 4832.244345 YDOT = -7147.121373 feet/sec YDOT = -2178.442595 meter/sec ZDOT = -16787.425129 ZDOT = -5116.807179 </pre> 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 12036.53774461 .00016717 00000-0 10270-3 0 9028 2 25544 51.6405 67.4376 0020524 9.0384 351.1137 15.58717680 37338 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12036.53774461 = yrday.fracday Element set: 902 Inclination: 51.6405 deg RA of node: 67.4376 deg Eccentricity: .0020524 Arg of perigee: 9.0384 deg Mean anomaly: 351.1137 deg </pre> Mean motion: 15.58717680 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3733 Checksum: 300 </pre> Coasting Arc #4 (Orbit 3748) <hr/> Vector Time (GMT): 2012/037/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 2984581.37 A = 6776036.27 meter Y = 6055034.40 meter E = .0031771 Z = 274009.07 I = 51.96900 XDOT = -4367.040814 Wp = 25.89243 YDOT = 1868.149002 meter/sec RA = 61.94157 deg ZDOT = 6050.572517 TA = 337.05897 MA = 337.20057 Ha = 220.203 n.mi Hp = 202.625 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 9791933.63 X = 2915319.90 Y = 19865598.44 feet Y = 6088022.57 meter Z = 898979.90 Z = 288339.41 XDOT = -14327.561725 XDOT = -4416.997755 YDOT = 6129.097775 feet/sec YDOT = 1819.034726 meter/sec ZDOT = 19850.959703 ZDOT = 6029.236887 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -7039064.84 X = -2145506.96 Y = 20996841.63 feet Y = 6399837.33 meter Z = 957255.42 Z = 291771.45 XDOT = -13044.271274 XDOT = -3975.893884 YDOT = -5306.928413 feet/sec YDOT = -1617.551780 meter/sec ZDOT = 19763.314324 ZDOT = 6023.858206 </pre> 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 12037.56355610 .00016717 00000-0 10270-3 0 9034 2 25544 51.6409 62.2885 0020593 12.9097 347.2581 15.58706756 37498 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12037.56355610 = yrday.fracday Element set: 903 Inclination: 51.6409 deg RA of node: 62.2885 deg Eccentricity: .0020593 Arg of perigee: 12.9097 deg Mean anomaly: 347.2581 deg </pre> Mean motion: 15.58706756 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3749 Checksum: 326 </pre> Coasting Arc #5 (Orbit 3763) <hr/> Vector Time (GMT): 2012/038/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -738219.26 A = 6771300.47 meter Y = -5881009.26 meter E = .0021949 Z = -3304200.45 I = 51.93799 XDOT = 5690.939333 Wp = 28.28723 YDOT = 1949.568289 meter/sec RA = 56.96365 deg ZDOT = -4735.461607 TA = 189.91449 MA = 189.95786 Ha = 220.230 n.mi Hp = 202.404 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -2421979.20 X = -656351.17 Y = -19294649.80 feet Y = -5888806.81 meter Z = -10840552.65 Z = -3307587.59 XDOT = 18671.060804 XDOT = 5691.719050 YDOT = 6396.221419 feet/sec YDOT = 2013.212125 meter/sec ZDOT = -15536.291362 ZDOT = -4707.814231 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 11647380.47 X = 3550121.57 Y = -15562681.37 feet Y = -4743505.28 meter Z = -10853964.84 Z = -3308288.48 XDOT = 7990.530972 XDOT = 2435.513840 YDOT = 16750.456193 feet/sec YDOT = 5105.539047 meter/sec ZDOT = -15423.070906 ZDOT = -4700.952012 </pre> 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 12038.52523870 .00016717 00000-0 10270-3 0 9047 2 25544 51.6405 57.4601 0020526 16.5619 343.6203 15.58742510 37648 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12038.52523870 = yrday.fracday Element set: 904 Inclination: 51.6405 deg RA of node: 57.4601 deg Eccentricity: .0020526 Arg of perigee: 16.5619 deg Mean anomaly: 343.6203 deg </pre> Mean motion: 15.58742510 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3764 Checksum: 289 </pre> Coasting Arc #6 (Orbit 3779) <hr/> Vector Time (GMT): 2012/039/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1972743.38 A = 6764806.53 meter Y = 3966493.71 meter E = .0019893 Z = 5098688.28 I = 51.89781 XDOT = -5603.399780 Wp = 34.42564 YDOT = -4976.179932 meter/sec RA = 51.95088 deg ZDOT = 1715.943704 TA = 39.16875 MA = 39.02494 Ha = 220.429 n.mi Hp = 202.104 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -6472255.18 X = -2041718.49 Y = 13013430.82 feet Y = 3944047.87 meter Z = 16727979.94 Z = 5088937.32 XDOT = -18383.857545 XDOT = -5555.674123 YDOT = -16326.049647 feet/sec YDOT = -5038.573670 meter/sec ZDOT = 5629.736563 ZDOT = 1688.839548 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13664724.56 X = -4165008.05 Y = 5085447.50 feet Y = 1550044.40 meter Z = 16687669.34 Z = 5086401.61 XDOT = -2055.444418 XDOT = -626.499459 YDOT = -23495.468350 feet/sec YDOT = -7161.418753 meter/sec ZDOT = 5518.991714 ZDOT = 1682.188674 </pre> 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 12039.55101961 .00016717 00000-0 10270-3 0 9055 2 25544 51.6393 52.3093 0020581 20.5198 339.6779 15.58760295 37802 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12039.55101961 = yrday.fracday Element set: 905 Inclination: 51.6393 deg RA of node: 52.3093 deg Eccentricity: .0020581 Arg of perigee: 20.5198 deg Mean anomaly: 339.6779 deg </pre> Mean motion: 15.58760295 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3780 Checksum: 321 </pre> Coasting Arc #7 (Orbit 3794) <hr/> Vector Time (GMT): 2012/040/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4363911.42 A = 6765133.12 meter Y = -1140952.82 meter E = .0026031 Z = -5055252.10 I = 51.87976 XDOT = 3859.268835 Wp = 52.80560 YDOT = 6336.730021 meter/sec RA = 46.92031 deg ZDOT = 1923.424079 TA = 235.67220 MA = 235.91882 Ha = 220.478 n.mi Hp = 202.006 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 14317294.69 X = 4400902.14 Y = -3743283.51 feet Y = -1091946.37 meter Z = -16585472.77 Z = -5033963.00 XDOT = 12661.643161 XDOT = 3778.780083 YDOT = 20789.796658 feet/sec YDOT = 6379.436834 meter/sec ZDOT = 6310.446454 ZDOT = 1941.975866 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13243361.16 X = 4036576.48 Y = 6819223.53 feet Y = 2078499.33 meter Z = -16498078.11 Z = -5028614.21 XDOT = -3950.878946 XDOT = -1204.227903 YDOT = 22946.358401 feet/sec YDOT = 6994.050041 meter/sec ZDOT = 6386.004121 ZDOT = 1946.454056 </pre> 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 12040.51267474 .00016717 00000-0 10270-3 0 9066 2 25544 51.6399 47.4821 0020592 23.6966 336.5132 15.58762003 37955 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12040.51267474 = yrday.fracday Element set: 906 Inclination: 51.6399 deg RA of node: 47.4821 deg Eccentricity: .0020592 Arg of perigee: 23.6966 deg Mean anomaly: 336.5132 deg </pre> Mean motion: 15.58762003 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3795 Checksum: 315 </pre> Coasting Arc #8 (Orbit 3810) <hr/> Vector Time (GMT): 2012/041/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5723915.45 A = 6771680.01 meter Y = -1869057.54 meter E = .0028254 Z = 3099534.06 I = 51.88004 XDOT = -767.083063 Wp = 52.48478 YDOT = -5853.543066 meter/sec RA = 41.90659 deg ZDOT = -4898.997722 TA = 91.94099 MA = 91.61740 Ha = 220.490 n.mi Hp = 201.636 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -18779250.17 X = -5717646.41 Y = -6132078.54 feet Y = -1933030.61 meter Z = 10169075.00 Z = 3071743.44 XDOT = -2516.676717 XDOT = -677.772791 YDOT = -19204.537618 feet/sec YDOT = -5861.622061 meter/sec ZDOT = -16072.827171 ZDOT = -4902.506745 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -10250779.35 X = -3124437.54 Y = -16955404.83 feet Y = -5168007.39 meter Z = 10055271.27 Z = 3064846.68 XDOT = 9486.338769 XDOT = 2891.436057 YDOT = -15368.437887 feet/sec YDOT = -4684.299868 meter/sec ZDOT = -16086.733649 ZDOT = -4903.236416 </pre> 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 12041.53842440 .00016717 00000-0 10270-3 0 9072 2 25544 51.6392 42.3307 0020707 27.4356 332.7888 15.58837787 38111 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12041.53842440 = yrday.fracday Element set: 907 Inclination: 51.6392 deg RA of node: 42.3307 deg Eccentricity: .0020707 Arg of perigee: 27.4356 deg Mean anomaly: 332.7888 deg </pre> Mean motion: 15.58837787 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3811 Checksum: 317 </pre> Coasting Arc #9 (Orbit 3825) <hr/> Vector Time (GMT): 2012/042/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 5429526.21 A = 6775580.33 meter Y = 4023369.71 meter E = .0032395 Z = -58136.44 I = 51.87047 XDOT = -2797.148948 Wp = 36.28916 YDOT = 3837.079506 meter/sec RA = 36.92597 deg ZDOT = 6048.781924 TA = 323.08423 MA = 323.30677 Ha = 220.433 n.mi Hp = 201.327 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 17813406.20 X = 5384414.96 Y = 13200031.85 feet Y = 4083833.78 meter Z = -190736.35 Z = -31870.29 XDOT = -9176.997860 XDOT = -2869.231236 YDOT = 12588.843522 feet/sec YDOT = 3805.397449 meter/sec ZDOT = 19845.085052 ZDOT = 6035.018351 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 5225139.35 X = 1592622.47 Y = 21547288.22 feet Y = 6567613.45 meter Z = -83369.90 Z = -25411.15 XDOT = -13632.654146 XDOT = -4155.232984 YDOT = 3332.049656 feet/sec YDOT = 1015.608735 meter/sec ZDOT = 19788.329066 ZDOT = 6031.482699 </pre> 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 12042.50005166 .00016717 00000-0 10270-3 0 9087 2 25544 51.6395 37.5037 0020510 31.5497 328.6883 15.58874755 38265 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12042.50005166 = yrday.fracday Element set: 908 Inclination: 51.6395 deg RA of node: 37.5037 deg Eccentricity: .0020510 Arg of perigee: 31.5497 deg Mean anomaly: 328.6883 deg </pre> Mean motion: 15.58874755 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3826 Checksum: 316 </pre> Coasting Arc #10 (Orbit 3841) <hr/> Vector Time (GMT): 2012/043/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3424833.98 A = 6771549.30 meter Y = -4985810.32 meter E = .0022618 Z = -3077403.01 I = 51.83167 XDOT = 5789.768862 Wp = 45.47633 YDOT = -945.740271 meter/sec RA = 31.94211 deg ZDOT = -4918.003162 TA = 169.74697 MA = 169.70076 Ha = 220.603 n.mi Hp = 201.110 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -11236331.95 X = -3353877.95 Y = -16357645.41 feet Y = -5023712.36 meter Z = -10096466.56 Z = -3093867.88 XDOT = 18995.304665 XDOT = 5823.804288 YDOT = -3102.822412 feet/sec YDOT = -880.805478 meter/sec ZDOT = -16135.180977 ZDOT = -4889.794327 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 1556886.46 X = 474538.99 Y = -19749546.99 feet Y = -6019661.92 meter Z = -10163555.21 Z = -3097851.63 XDOT = 15376.819657 XDOT = 4686.854631 YDOT = 9444.711383 feet/sec YDOT = 2878.748029 meter/sec ZDOT = -16019.438162 ZDOT = -4882.724752 </pre> 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 12043.52577132 .00016717 00000-0 10270-3 0 9098 2 25544 51.6391 32.3523 0020718 35.0986 325.1530 15.58852682 38420 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12043.52577132 = yrday.fracday Element set: 909 Inclination: 51.6391 deg RA of node: 32.3523 deg Eccentricity: .0020718 Arg of perigee: 35.0986 deg Mean anomaly: 325.1530 deg </pre> Mean motion: 15.58852682 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3842 Checksum: 302 </pre> Coasting Arc #11 (Orbit 3857) <hr/> Vector Time (GMT): 2012/044/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 182833.19 A = 6764759.23 meter Y = 4518953.07 meter E = .0021817 Z = 5011759.93 I = 51.78272 XDOT = -7185.675265 Wp = 53.00818 YDOT = -1899.339844 meter/sec RA = 26.92482 deg ZDOT = 1981.646021 TA = 17.88879 MA = 17.81212 Ha = 220.638 n.mi Hp = 200.947 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 599846.44 X = 107942.02 Y = 14825961.51 feet Y = 4520579.06 meter Z = 16442781.91 Z = 5012466.05 XDOT = -23575.050083 XDOT = -7173.528701 YDOT = -6231.429935 feet/sec YDOT = -1979.626510 meter/sec ZDOT = 6501.463322 ZDOT = 1946.768262 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -8704989.08 X = -2653280.67 Y = 12012894.75 feet Y = 3661530.32 meter Z = 16445289.67 Z = 5012524.29 XDOT = -13943.359574 XDOT = -4249.935998 YDOT = -18777.522348 feet/sec YDOT = -5723.388812 meter/sec ZDOT = 6358.623188 ZDOT = 1938.108348 </pre> 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 12044.55147375 .00016717 00000-0 10270-3 0 9106 2 25544 51.6391 27.2023 0020657 38.4048 321.8573 15.58882279 38588 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12044.55147375 = yrday.fracday Element set: 910 Inclination: 51.6391 deg RA of node: 27.2023 deg Eccentricity: .0020657 Arg of perigee: 38.4048 deg Mean anomaly: 321.8573 deg </pre> Mean motion: 15.58882279 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3858 Checksum: 318 </pre> Coasting Arc #12 (Orbit 3872) <hr/> Vector Time (GMT): 2012/045/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3268371.49 A = 6764547.95 meter Y = -3027747.60 meter E = .0029586 Z = -5110038.34 I = 51.75438 XDOT = 6317.531843 Wp = 64.88478 YDOT = 3982.466969 meter/sec RA = 21.88432 deg ZDOT = 1700.969135 TA = 221.42856 MA = 221.65327 Ha = 220.715 n.mi Hp = 200.837 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 10723003.59 X = 3326808.59 Y = -9933555.12 feet Y = -2990871.98 meter Z = -16765217.66 Z = -5094018.94 XDOT = 20726.810507 XDOT = 6264.266734 YDOT = 13065.836514 feet/sec YDOT = 4052.815705 meter/sec ZDOT = 5580.607398 ZDOT = 1731.529637 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 14620454.44 X = 4456314.51 Y = -1451690.96 feet Y = -442475.41 meter Z = -16699273.98 Z = -5089938.71 XDOT = 8606.663786 XDOT = 2623.311122 YDOT = 21803.019077 feet/sec YDOT = 6645.560215 meter/sec ZDOT = 5705.561298 ZDOT = 1739.055084 </pre> 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 12045.51305516 .00016717 00000-0 10270-3 0 9117 2 25544 51.6393 22.3742 0020708 42.0817 318.1924 15.58880110 38734 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12045.51305516 = yrday.fracday Element set: 911 Inclination: 51.6393 deg RA of node: 22.3742 deg Eccentricity: .0020708 Arg of perigee: 42.0817 deg Mean anomaly: 318.1924 deg </pre> Mean motion: 15.58880110 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3873 Checksum: 285 </pre> Coasting Arc #13 (Orbit 3888) <hr/> Vector Time (GMT): 2012/046/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5888745.64 A = 6771065.80 meter Y = 867580.96 meter E = .0030820 Z = 3219463.07 I = 51.74800 XDOT = -3374.399094 Wp = 63.22076 YDOT = -4964.813347 meter/sec RA = 16.85974 deg ZDOT = -4785.351025 TA = 79.49157 MA = 79.14447 Ha = 220.729 n.mi Hp = 200.581 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -19320031.63 X = -5913648.63 Y = 2846394.23 feet Y = 801590.13 meter Z = 10562542.89 Z = 3190795.75 XDOT = -11070.863170 XDOT = -3295.384950 YDOT = -16288.757700 feet/sec YDOT = -5002.106157 meter/sec ZDOT = -15699.970555 ZDOT = -4801.551549 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -17372821.86 X = -5295236.10 Y = -9056567.54 feet Y = -2760441.79 meter Z = 10444928.90 Z = 3183614.33 XDOT = -2.937906 XDOT = -.895474 YDOT = -18364.226430 feet/sec YDOT = -5597.416216 meter/sec ZDOT = -15765.957821 ZDOT = -4805.463944 </pre> 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 12046.53872478 .00016717 00000-0 10270-3 0 9127 2 25544 51.6392 17.2231 0020720 45.5902 314.6945 15.58939476 38897 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12046.53872478 = yrday.fracday Element set: 912 Inclination: 51.6392 deg RA of node: 17.2231 deg Eccentricity: .0020720 Arg of perigee: 45.5902 deg Mean anomaly: 314.6945 deg </pre> Mean motion: 15.58939476 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3889 Checksum: 328 </pre> Coasting Arc #14 (Orbit 3903) <hr/> Vector Time (GMT): 2012/047/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6641971.55 A = 6775300.56 meter Y = 1249150.33 meter E = .0032526 Z = -181959.10 I = 51.73323 XDOT = -739.153778 Wp = 47.24701 YDOT = 4706.634740 meter/sec RA = 11.86806 deg ZDOT = 6031.909672 TA = 310.78857 MA = 311.07031 Ha = 220.695 n.mi Hp = 200.305 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 21791245.24 X = 6628393.55 Y = 4098262.24 feet Y = 1323349.03 meter Z = -596978.67 Z = -149726.30 XDOT = -2425.045205 XDOT = -821.030465 YDOT = 15441.715027 feet/sec YDOT = 4697.911236 meter/sec ZDOT = 19789.729896 ZDOT = 6028.120120 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15529083.17 X = 4733264.55 Y = 15831674.60 feet Y = 4825494.42 meter Z = -464931.39 Z = -141711.09 XDOT = -9769.108347 XDOT = -2977.624224 YDOT = 10076.264569 feet/sec YDOT = 3071.245441 meter/sec ZDOT = 19773.776939 ZDOT = 6027.047211 </pre> 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 12047.50027498 .00016717 00000-0 10270-3 0 9130 2 25544 51.6393 12.3952 0020688 49.6279 310.6678 15.58967174 39042 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12047.50027498 = yrday.fracday Element set: 913 Inclination: 51.6393 deg RA of node: 12.3952 deg Eccentricity: .0020688 Arg of perigee: 49.6279 deg Mean anomaly: 310.6678 deg </pre> Mean motion: 15.58967174 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3904 Checksum: 336 </pre> Coasting Arc #15 (Orbit 3919) <hr/> Vector Time (GMT): 2012/048/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 <pre> M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5267528.82 A = 6771276.02 meter Y = -3034183.04 meter E = .0023598 Z = -3014955.08 I = 51.69113 XDOT = 4766.095186 Wp = 61.49256 YDOT = -3368.547531 meter/sec RA = 6.87498 deg ZDOT = -4955.475633 TA = 152.99637 MA = 152.87339 Ha = 220.699 n.mi Hp = 200.087 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -17281918.69 X = -5218562.86 Y = -9954668.75 feet Y = -3092814.01 meter Z = -9891584.91 Z = -3040424.94 XDOT = 15636.795229 XDOT = 4827.480738 YDOT = -11051.665127 feet/sec YDOT = -3314.906902 meter/sec ZDOT = -16258.122155 ZDOT = -4932.173607 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -8736118.03 X = -2662768.78 Y = -17870894.86 feet Y = -5447048.75 meter Z = -9995746.81 Z = -3046703.63 XDOT = 17921.880551 XDOT = 5462.589192 YDOT = 245.426637 feet/sec YDOT = 74.806039 meter/sec ZDOT = -16162.283633 ZDOT = -4926.264051 </pre> 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 12048.52591123 .00016717 00000-0 10270-3 0 9145 2 25544 51.6402 7.2436 0020738 52.9742 307.3307 15.58991853 39202 Satellite: ISS Catalog Number: 25544 <pre> Epoch time: 12048.52591123 = yrday.fracday Element set: 914 Inclination: 51.6402 deg RA of node: 7.2436 deg Eccentricity: .0020738 Arg of perigee: 52.9742 deg Mean anomaly: 307.3307 deg </pre> Mean motion: 15.58991853 rev/day Decay rate: 1.67170E-04 rev/day^2 <pre> Epoch rev: 3920 Checksum: 301</pre> <hr/> 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. <pre> David Cottle Director Of Engineering IDB Communications</pre> <hr/> The following information is a reminder of your current mailing list subscription: You are subscribed to the following list: [ISSTLE LIST] using the following email: <a href="mailto:example@example.com">example@example.com</a> You may automatically unsubscribe from this list at any time by visiting the following URL: <<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>> If the above URL is inoperable, make sure that you have copied the entire address. Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism. You may also change your subscription by visiting this list's main screen: <<a href="http://www.aus-city.com/cgi-bin/dada/mail.cgi/list/ISSTLE_LIST">http://www.aus-city.com/cgi-bin/dada/mail.cgi/list/ISSTLE_LIST</a>> If you're still having trouble, please contact the list owner at: <mailto:<a href="mailto:list.admin@aus-city.com">list.admin@aus-city.com</a>> The following physical address is associated with this mailing list: <a href="http://www.aus-city.com">http://www.aus-city.com</a>

[ISSTLE LIST] Current ISS TLEs @ 18:30 UTC

Sun, 05 Feb 2012 18:30:00 GMT

[ISSTLE LIST] Current ISS TLEs @ 06:30 UTC

Sun, 05 Feb 2012 06:30:00 GMT

[ISSTLE LIST] Current ISS TLEs @ 18:30 UTC

Sat, 04 Feb 2012 18:30:00 GMT

[ISSTLE LIST] Current ISS TLEs @ 06:30 UTC

Sat, 04 Feb 2012 06:30:00 GMT

[ISSTLE LIST] Current ISS TLEs @ 18:30 UTC

Fri, 03 Feb 2012 18:30:00 GMT