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Subject:
[ISSTLE LIST] Current ISS TLEs @ 18:30 UTC
Date:
February 7th 2012
<B> ISS TRAJECTORY DATA</B>
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:
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 3748)
Vector Time (GMT): 2012/037/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 886586.8
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
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
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
Mean motion: 15.58699571 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3749
Checksum: 325
Coasting Arc #2 (Orbit 3763)
Vector Time (GMT): 2012/038/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 886586.8
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
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
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
Mean motion: 15.58734358 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3764
Checksum: 319
Coasting Arc #3 (Orbit 3779)
Vector Time (GMT): 2012/039/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 886586.8
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
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
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
Mean motion: 15.58751098 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3780
Checksum: 306
Coasting Arc #4 (Orbit 3794)
Vector Time (GMT): 2012/040/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 886586.8
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
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
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
Mean motion: 15.58751826 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3795
Checksum: 307
Coasting Arc #5 (Orbit 3810)
Vector Time (GMT): 2012/041/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 886586.8
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
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
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
Mean motion: 15.58826544 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3811
Checksum: 300
Coasting Arc #6 (Orbit 3825)
Vector Time (GMT): 2012/042/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 886586.8
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
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
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
Mean motion: 15.58862410 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3826
Checksum: 288
Coasting Arc #7 (Orbit 3841)
Vector Time (GMT): 2012/043/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 886586.8
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
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
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
Mean motion: 15.58839468 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3842
Checksum: 299
Coasting Arc #8 (Orbit 3857)
Vector Time (GMT): 2012/044/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 886586.8
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
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
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
Mean motion: 15.58868107 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3858
Checksum: 319
Coasting Arc #9 (Orbit 3872)
Vector Time (GMT): 2012/045/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 886586.8
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
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
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
Mean motion: 15.58864690 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3873
Checksum: 294
Coasting Arc #10 (Orbit 3888)
Vector Time (GMT): 2012/046/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 886586.8
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
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
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
Mean motion: 15.58922764 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3889
Checksum: 335
Coasting Arc #11 (Orbit 3903)
Vector Time (GMT): 2012/047/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 886586.8
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
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
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
Mean motion: 15.58948940 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3904
Checksum: 306
Coasting Arc #12 (Orbit 3919)
Vector Time (GMT): 2012/048/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 886586.8
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
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
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
Mean motion: 15.58972896 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3920
Checksum: 300
Coasting Arc #13 (Orbit 3935)
Vector Time (GMT): 2012/049/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 886586.8
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
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
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
Mean motion: 15.59024869 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3936
Checksum: 314
Coasting Arc #14 (Orbit 3950)
Vector Time (GMT): 2012/050/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 886586.8
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
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
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
Mean motion: 15.59002087 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3951
Checksum: 281
Coasting Arc #15 (Orbit 3966)
Vector Time (GMT): 2012/051/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 886586.8
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
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
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
Mean motion: 15.59047410 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3967
Checksum: 329
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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