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Date:
March 8th 2010
<B> ISS TRAJECTORY DATA</B>
Lift off time (UTC) : N/A
Area (sq ft) : 20989.63
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 714)
Vector Time (GMT): 2010/064/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3538470.99 A = 6731290.76 meter
Y = 5350909.38 meter E = .0019407
Z = 2000265.91 I = 51.88616
XDOT = -5126.245037 Wp = 49.53740
YDOT = 1283.412060 meter/sec RA = 42.36518 deg
ZDOT = 5612.059819 TA = 332.69352
MA = 332.79541
Ha = 192.405 n.mi
Hp = 183.133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11609156.78 X = 3468656.32
Y = 17555476.98 feet Y = 5390088.41 meter
Z = 6562552.19 Z = 2017285.83
XDOT = -16818.389230 XDOT = -5167.477560
YDOT = 4210.669489 feet/sec YDOT = 1225.857079 meter/sec
ZDOT = 18412.269746 ZDOT = 5587.056488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5704649.21 X = 1738777.08
Y = 20236865.79 feet Y = 6168196.69 meter
Z = 6630280.91 Z = 2020909.62
XDOT = -15930.778484 XDOT = -4855.701282
YDOT = -1533.646841 feet/sec YDOT = -467.455557 meter/sec
ZDOT = 18312.977224 ZDOT = 5581.795458
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 10064.55953376 .00016717 00000-0 10270-3 0 9001
2 25544 51.6442 42.6164 0007589 13.1385 346.9974 15.73689781 7157
Satellite: ISS
Catalog Number: 25544
Epoch time: 10064.55953376 = yrday.fracday
Element set: 900
Inclination: 51.6442 deg
RA of node: 42.6164 deg
Eccentricity: .0007589
Arg of perigee: 13.1385 deg
Mean anomaly: 346.9974 deg
Mean motion: 15.73689781 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 715
Checksum: 332
Coasting Arc #2 (Orbit 729)
Vector Time (GMT): 2010/065/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4282605.51 A = 6722697.56 meter
Y = -1617277.15 meter E = .0014779
Z = -4934025.76 I = 51.83384
XDOT = 4667.925050 Wp = 73.87764
YDOT = 5706.538127 meter/sec RA = 37.21201 deg
ZDOT = 2190.555086 TA = 217.31011
MA = 217.41285
Ha = 192.673 n.mi
Hp = 183.099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14050543.02 X = 4324340.28
Y = -5306027.39 feet Y = -1569153.32 meter
Z = -16187748.55 Z = -4913119.63
XDOT = 15314.714732 XDOT = 4593.125373
YDOT = 18722.237951 feet/sec YDOT = 5758.319482 meter/sec
ZDOT = 7186.860519 ZDOT = 2213.049776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15072975.86 X = 4594243.04
Y = -1028474.63 feet Y = -313479.07 meter
Z = -16104736.19 Z = -4908723.59
XDOT = 9188.862879 XDOT = 2800.765405
YDOT = 21215.642113 feet/sec YDOT = 6466.527716 meter/sec
ZDOT = 7276.337678 ZDOT = 2217.827724
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 10065.51208237 .00016717 00000-0 10270-3 0 9018
2 25544 51.6444 37.7273 0007834 16.5794 343.5623 15.73656771 7303
Satellite: ISS
Catalog Number: 25544
Epoch time: 10065.51208237 = yrday.fracday
Element set: 901
Inclination: 51.6444 deg
RA of node: 37.7273 deg
Eccentricity: .0007834
Arg of perigee: 16.5794 deg
Mean anomaly: 343.5623 deg
Mean motion: 15.73656771 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 730
Checksum: 305
Coasting Arc #3 (Orbit 745)
Vector Time (GMT): 2010/066/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4567097.43 A = 6731432.16 meter
Y = -4588506.69 meter E = .0007407
Z = -1854252.48 I = 51.83996
XDOT = 4645.267125 Wp = 75.11438
YDOT = -2340.609214 meter/sec RA = 32.12739 deg
ZDOT = -5666.316637 TA = 125.38406
MA = 125.31484
Ha = 192.634 n.mi
Hp = 182.739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14983915.45 X = -4506440.98
Y = -15054155.81 feet Y = -4639239.58 meter
Z = -6083505.50 Z = -1876291.71
XDOT = 15240.377707 XDOT = 4698.620581
YDOT = -7679.164088 feet/sec YDOT = -2288.364901 meter/sec
ZDOT = -18590.277681 ZDOT = -5643.620567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10325048.23 X = -3147074.70
Y = -18532800.64 feet Y = -5648797.63 meter
Z = -6171146.41 Z = -1880965.43
XDOT = 15501.934850 XDOT = 4724.989742
YDOT = -2494.379960 feet/sec YDOT = -760.287012 meter/sec
ZDOT = -18500.166592 ZDOT = -5638.850777
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 10066.52811156 .00016717 00000-0 10270-3 0 9021
2 25544 51.6450 32.5121 0007904 20.1449 340.0024 15.73719172 7460
Satellite: ISS
Catalog Number: 25544
Epoch time: 10066.52811156 = yrday.fracday
Element set: 902
Inclination: 51.6450 deg
RA of node: 32.5121 deg
Eccentricity: .0007904
Arg of perigee: 20.1449 deg
Mean anomaly: 340.0024 deg
Mean motion: 15.73719172 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 746
Checksum: 265
Coasting Arc #4 (Orbit 761)
Vector Time (GMT): 2010/067/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3800393.49 A = 6722260.26 meter
Y = 2455152.33 meter E = .0013403
Z = 4968011.10 I = 51.78297
XDOT = -5734.879842 Wp = 37.43359
YDOT = -4721.422964 meter/sec RA = 26.97307 deg
ZDOT = -2040.435039 TA = 72.34143
MA = 72.19512
Ha = 192.759 n.mi
Hp = 182.611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12468482.57 X = -3851698.29
Y = 8054961.73 feet Y = 2412367.34 meter
Z = 16299249.02 Z = 4949424.42
XDOT = -18815.222578 XDOT = -5671.745918
YDOT = -15490.232821 feet/sec YDOT = -4785.200845 meter/sec
ZDOT = -6694.340680 ZDOT = -2068.141163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14195998.04 X = -4326940.20
Y = 4606409.83 feet Y = 1404033.71 meter
Z = 16225461.87 Z = 4945520.78
XDOT = -13898.394399 XDOT = -4236.230613
YDOT = -18709.626008 feet/sec YDOT = -5702.694007 meter/sec
ZDOT = -6804.494008 ZDOT = -2074.009774
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 10067.54411960 .00016717 00000-0 10270-3 0 9034
2 25544 51.6451 27.2974 0007852 23.6292 336.5231 15.73742358 7624
Satellite: ISS
Catalog Number: 25544
Epoch time: 10067.54411960 = yrday.fracday
Element set: 903
Inclination: 51.6451 deg
RA of node: 27.2974 deg
Eccentricity: .0007852
Arg of perigee: 23.6292 deg
Mean anomaly: 336.5231 deg
Mean motion: 15.73742358 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 762
Checksum: 302
Coasting Arc #5 (Orbit 777)
Vector Time (GMT): 2010/068/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5398513.51 A = 6731460.57 meter
Y = 3617972.86 meter E = .0020833
Z = 1708704.40 I = 51.78739
XDOT = -4003.522977 Wp = 51.37550
YDOT = 3252.256878 meter/sec RA = 21.88270 deg
ZDOT = 5728.684481 TA = 327.50732
MA = 327.63539
Ha = 192.611 n.mi
Hp = 182.381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17711658.49 X = 5349355.05
Y = 11869989.70 feet Y = 3678067.44 meter
Z = 5605985.56 Z = 1734810.34
XDOT = -13134.917904 XDOT = -4067.421112
YDOT = 10670.134113 feet/sec YDOT = 3207.130021 meter/sec
ZDOT = 18794.896592 ZDOT = 5709.080437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14363471.90 X = 4377986.23
Y = 15719919.93 feet Y = 4791431.59 meter
Z = 5709760.82 Z = 1740335.10
XDOT = -14249.558237 XDOT = -4343.265351
YDOT = 6181.977361 feet/sec YDOT = 1884.266700 meter/sec
ZDOT = 18717.081924 ZDOT = 5704.966570
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 10068.56010487 .00016717 00000-0 10270-3 0 9047
2 25544 51.6453 22.0823 0007780 27.5836 332.5739 15.73791987 7787
Satellite: ISS
Catalog Number: 25544
Epoch time: 10068.56010487 = yrday.fracday
Element set: 904
Inclination: 51.6453 deg
RA of node: 22.0823 deg
Eccentricity: .0007780
Arg of perigee: 27.5836 deg
Mean anomaly: 332.5739 deg
Mean motion: 15.73791987 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 778
Checksum: 328
Coasting Arc #6 (Orbit 792)
Vector Time (GMT): 2010/069/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3169613.89 A = 6721901.63 meter
Y = -3179766.31 meter E = .0017002
Z = -5015852.86 I = 51.72718
XDOT = 6554.259502 Wp = 77.69374
YDOT = 3540.168276 meter/sec RA = 16.72556 deg
ZDOT = 1906.458698 TA = 210.66644
MA = 210.76592
Ha = 192.718 n.mi
Hp = 182.334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10398995.69 X = 3229300.60
Y = -10432304.18 feet Y = -3143988.32 meter
Z = -16456210.16 Z = -5000310.08
XDOT = 21503.476058 XDOT = 6504.924553
YDOT = 11614.725316 feet/sec YDOT = 3613.186143 meter/sec
ZDOT = 6254.785756 ZDOT = 1938.178595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12534699.16 X = 3820576.30
Y = -7866365.62 feet Y = -2397668.24 meter
Z = -16394527.86 Z = -4997052.09
XDOT = 17809.331851 XDOT = 5428.284348
YDOT = 15141.334494 feet/sec YDOT = 4615.078754 meter/sec
ZDOT = 6380.861126 ZDOT = 1944.886471
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 10069.51257202 .00016717 00000-0 10270-3 0 9052
2 25544 51.6458 17.1928 0007852 30.4003 329.7614 15.73805028 7931
Satellite: ISS
Catalog Number: 25544
Epoch time: 10069.51257202 = yrday.fracday
Element set: 905
Inclination: 51.6458 deg
RA of node: 17.1928 deg
Eccentricity: .0007852
Arg of perigee: 30.4003 deg
Mean anomaly: 329.7614 deg
Mean motion: 15.73805028 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 793
Checksum: 297
Coasting Arc #7 (Orbit 808)
Vector Time (GMT): 2010/070/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6003460.72 A = 6731357.67 meter
Y = -2564470.78 meter E = .0009156
Z = -1650071.50 I = 51.73126
XDOT = 3258.306751 Wp = 87.23338
YDOT = -3952.024647 meter/sec RA = 11.62904 deg
ZDOT = -5739.490348 TA = 110.95381
MA = 110.85581
Ha = 192.692 n.mi
Hp = 182.044
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19696393.45 X = -5966322.59
Y = -8413618.05 feet Y = -2631397.50 meter
Z = -5413620.41 Z = -1679145.28
XDOT = 10689.982779 XDOT = 3330.137615
YDOT = -12965.960129 feet/sec YDOT = -3915.187070 meter/sec
ZDOT = -18830.348911 ZDOT = -5723.487121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17542798.03 X = -5347044.84
Y = -12236124.61 feet Y = -3729570.78 meter
Z = -5529164.61 Z = -1685289.37
XDOT = 12318.991669 XDOT = 3754.828661
YDOT = -9220.357719 feet/sec YDOT = -2810.365033 meter/sec
ZDOT = -18766.854411 ZDOT = -5720.137225
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 10070.52851498 .00016717 00000-0 10270-3 0 9063
2 25544 51.6466 11.9773 0007870 34.1819 325.9849 15.73851463 8096
Satellite: ISS
Catalog Number: 25544
Epoch time: 10070.52851498 = yrday.fracday
Element set: 906
Inclination: 51.6466 deg
RA of node: 11.9773 deg
Eccentricity: .0007870
Arg of perigee: 34.1819 deg
Mean anomaly: 325.9849 deg
Mean motion: 15.73851463 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 809
Checksum: 333
Coasting Arc #8 (Orbit 824)
Vector Time (GMT): 2010/071/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2501102.34 A = 6721620.07 meter
Y = 3705800.68 meter E = .0013357
Z = 5013705.68 I = 51.66901
XDOT = -7122.302589 Wp = 44.68828
YDOT = -2282.487141 meter/sec RA = 6.46894 deg
ZDOT = -1853.612591 TA = 63.23840
MA = 63.10179
Ha = 192.783 n.mi
Hp = 181.913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8205716.34 X = -2566710.53
Y = 12158138.71 feet Y = 3677465.44 meter
Z = 16449165.63 Z = 5001395.93
XDOT = -23367.134477 XDOT = -7087.245745
YDOT = -7488.474871 feet/sec YDOT = -2361.937100 meter/sec
ZDOT = -6081.406140 ZDOT = -1888.126648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10423657.55 X = -3177130.82
Y = 10397371.12 feet Y = 3169118.72 meter
Z = 16400341.59 Z = 4998824.12
XDOT = -20767.432200 XDOT = -6329.913334
YDOT = -10947.199798 feet/sec YDOT = -3336.706498 meter/sec
ZDOT = -6218.553301 ZDOT = -1895.415046
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 10071.54443566 .00016717 00000-0 10270-3 0 9070
2 25544 51.6468 6.7624 0007845 37.9213 322.2502 15.73883119 8253
Satellite: ISS
Catalog Number: 25544
Epoch time: 10071.54443566 = yrday.fracday
Element set: 907
Inclination: 51.6468 deg
RA of node: 6.7624 deg
Eccentricity: .0007845
Arg of perigee: 37.9213 deg
Mean anomaly: 322.2502 deg
Mean motion: 15.73883119 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 825
Checksum: 307
Coasting Arc #9 (Orbit 840)
Vector Time (GMT): 2010/072/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6376226.59 A = 6731298.87 meter
Y = 1407205.66 meter E = .0021569
Z = 1587126.57 I = 51.67202
XDOT = -2438.508374 Wp = 55.10586
YDOT = 4499.841223 meter/sec RA = 1.36696 deg
ZDOT = 5764.034911 TA = 322.41646
MA = 322.56702
Ha = 192.687 n.mi
Hp = 181.741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20919378.57 X = 6352307.24
Y = 4616816.48 feet Y = 1478374.83 meter
Z = 5207108.18 Z = 1618043.45
XDOT = -8000.355558 XDOT = -2516.645271
YDOT = 14763.258607 feet/sec YDOT = 4472.136049 meter/sec
ZDOT = 18910.875693 ZDOT = 5751.998637
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19803404.39 X = 6036077.66
Y = 8091120.97 feet Y = 2466173.67 meter
Z = 5329944.27 Z = 1624567.01
XDOT = -9906.767595 XDOT = -3019.582763
YDOT = 11730.872396 feet/sec YDOT = 3575.569906 meter/sec
ZDOT = 18863.158165 ZDOT = 5749.490609
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 10072.56033394 .00016717 00000-0 10270-3 0 9088
2 25544 51.6470 1.5465 0007844 41.4685 318.7072 15.73908512 8419
Satellite: ISS
Catalog Number: 25544
Epoch time: 10072.56033394 = yrday.fracday
Element set: 908
Inclination: 51.6470 deg
RA of node: 1.5465 deg
Eccentricity: .0007844
Arg of perigee: 41.4685 deg
Mean anomaly: 318.7072 deg
Mean motion: 15.73908512 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 841
Checksum: 301
Coasting Arc #10 (Orbit 855)
Vector Time (GMT): 2010/073/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1760400.92 A = 6721397.26 meter
Y = -4112364.12 meter E = .0018521
Z = -5031699.63 I = 51.60940
XDOT = 7408.185617 Wp = 82.24478
YDOT = 953.802811 meter/sec RA = 356.20219 deg
ZDOT = 1820.462596 TA = 205.29425
MA = 205.38505
Ha = 192.712 n.mi
Hp = 181.650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5775593.57 X = 1830697.98
Y = -13492008.28 feet Y = -4092285.78 meter
Z = -16508200.87 Z = -5022976.53
XDOT = 24305.070921 XDOT = 7388.126090
YDOT = 3129.274314 feet/sec YDOT = 1036.533588 meter/sec
ZDOT = 5972.646311 ZDOT = 1856.402166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7862021.14 X = 2396344.04
Y = -12438660.86 feet Y = -3791303.83 meter
Z = -16473639.68 Z = -5021165.37
XDOT = 22601.083459 XDOT = 6888.810238
YDOT = 6221.622172 feet/sec YDOT = 1896.350438 meter/sec
ZDOT = 6115.417015 ZDOT = 1863.979106
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 10073.51271731 .00016717 00000-0 10270-3 0 9094
2 25544 51.6477 356.6567 0007826 44.8470 315.3324 15.73946891 8563
Satellite: ISS
Catalog Number: 25544
Epoch time: 10073.51271731 = yrday.fracday
Element set: 909
Inclination: 51.6477 deg
RA of node: 356.6567 deg
Eccentricity: .0007826
Arg of perigee: 44.8470 deg
Mean anomaly: 315.3324 deg
Mean motion: 15.73946891 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 856
Checksum: 331
Coasting Arc #11 (Orbit 871)
Vector Time (GMT): 2010/074/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6528655.20 A = 6731036.16 meter
Y = -276955.74 meter E = .0010670
Z = -1620948.22 I = 51.61294
XDOT = 1623.169391 Wp = 95.48682
YDOT = -4857.853679 meter/sec RA = 351.09571 deg
ZDOT = -5740.896374 TA = 102.40133
MA = 102.28189
Ha = 192.675 n.mi
Hp = 181.467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21419472.45 X = -6517198.82
Y = -908647.44 feet Y = -349899.18 meter
Z = -5318071.59 Z = -1652636.21
XDOT = 5325.358894 XDOT = 1705.258072
YDOT = -15937.840154 feet/sec YDOT = -4839.244125 meter/sec
ZDOT = -18834.961858 ZDOT = -5732.811145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21067356.45 X = -6421330.25
Y = -3798869.00 feet Y = -1157895.27 meter
Z = -5443933.52 Z = -1659310.94
XDOT = 7268.830112 XDOT = 2215.539418
YDOT = -13518.281891 feet/sec YDOT = -4120.372320 meter/sec
ZDOT = -18802.953338 ZDOT = -5731.140177
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 10074.52857132 .00016717 00000-0 10270-3 0 9103
2 25544 51.6482 351.4409 0007760 48.8461 311.3370 15.73977590 8723
Satellite: ISS
Catalog Number: 25544
Epoch time: 10074.52857132 = yrday.fracday
Element set: 910
Inclination: 51.6482 deg
RA of node: 351.4409 deg
Eccentricity: .0007760
Arg of perigee: 48.8461 deg
Mean anomaly: 311.3370 deg
Mean motion: 15.73977590 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 872
Checksum: 310
Coasting Arc #12 (Orbit 887)
Vector Time (GMT): 2010/075/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1059537.20 A = 6721169.27 meter
Y = 4357839.64 meter E = .0013451
Z = 4999156.04 I = 51.55010
XDOT = -7468.846185 Wp = 52.75244
YDOT = 341.987132 meter/sec RA = 345.92603 deg
ZDOT = -1869.637793 TA = 55.35597
MA = 55.22924
Ha = 192.651 n.mi
Hp = 181.323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3476171.92 X = -1132473.44
Y = 14297374.15 feet Y = 4345584.05 meter
Z = 16401430.57 Z = 4993831.16
XDOT = -24504.088532 XDOT = -7463.032937
YDOT = 1122.005026 feet/sec YDOT = 258.498336 meter/sec
ZDOT = -6133.982260 ZDOT = -1905.907133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5241094.62 X = -1597485.64
Y = 13773880.72 feet Y = 4198278.84 meter
Z = 16380376.69 Z = 4992738.82
XDOT = -23423.801388 XDOT = -7139.574663
YDOT = -1402.218914 feet/sec YDOT = -427.396325 meter/sec
ZDOT = -6278.017866 ZDOT = -1913.539845
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 10075.54440146 .00016717 00000-0 10270-3 0 9110
2 25544 51.6477 346.2253 0007750 51.6906 308.4956 15.74048386 8888
Satellite: ISS
Catalog Number: 25544
Epoch time: 10075.54440146 = yrday.fracday
Element set: 911
Inclination: 51.6477 deg
RA of node: 346.2253 deg
Eccentricity: .0007750
Arg of perigee: 51.6906 deg
Mean anomaly: 308.4956 deg
Mean motion: 15.74048386 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 888
Checksum: 322
Coasting Arc #13 (Orbit 903)
Vector Time (GMT): 2010/076/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6457965.49 A = 6730834.89 meter
Y = -864372.81 meter E = .0021871
Z = 1644813.85 I = 51.55410
XDOT = -789.999054 Wp = 60.67492
YDOT = 5092.747711 meter/sec RA = 340.81532 deg
ZDOT = 5731.628990 TA = 317.53633
MA = 317.70532
Ha = 192.649 n.mi
Hp = 181.196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21187550.82 X = 6459160.89
Y = -2835868.79 feet Y = -792149.13 meter
Z = 5396370.89 Z = 1676189.58
XDOT = -2591.860414 XDOT = -874.731523
YDOT = 16708.489864 feet/sec YDOT = 5083.440342 meter/sec
ZDOT = 18804.557054 ZDOT = 5727.584804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21333922.73 X = 6502579.65
Y = -676827.62 feet Y = -206297.06 meter
Z = 5520953.33 Z = 1682786.58
XDOT = -4431.460005 XDOT = -1350.709009
YDOT = 14793.256607 feet/sec YDOT = 4508.984614 meter/sec
ZDOT = 18788.605676 ZDOT = 5726.767010
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 10076.56021078 .00016717 00000-0 10270-3 0 9123
2 25544 51.6481 341.0090 0007814 55.6910 304.4992 15.74041996 9040
Satellite: ISS
Catalog Number: 25544
Epoch time: 10076.56021078 = yrday.fracday
Element set: 912
Inclination: 51.6481 deg
RA of node: 341.0090 deg
Eccentricity: .0007814
Arg of perigee: 55.6910 deg
Mean anomaly: 304.4992 deg
Mean motion: 15.74041996 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 904
Checksum: 297
Coasting Arc #14 (Orbit 918)
Vector Time (GMT): 2010/077/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 336948.01 A = 6721127.74 meter
Y = -4509452.93 meter E = .0019180
Z = -4988641.75 I = 51.49402
XDOT = 7265.349012 Wp = 87.60263
YDOT = -1595.314098 meter/sec RA = 335.63974 deg
ZDOT = 1939.998257 TA = 201.17143
MA = 201.25091
Ha = 192.598 n.mi
Hp = 181.105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1105472.46 X = 411582.43
Y = -14794793.06 feet Y = -4505268.15 meter
Z = -16366934.87 Z = -4986823.13
XDOT = 23836.446891 XDOT = 7273.223943
YDOT = -5233.970137 feet/sec YDOT = -1514.024429 meter/sec
ZDOT = 6364.823679 ZDOT = 1975.312653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2443669.49 X = 744830.46
Y = -14641368.43 feet Y = -4462689.10 meter
Z = -16359808.62 Z = -4986469.67
XDOT = 23087.214121 XDOT = 7036.982864
YDOT = -3388.811693 feet/sec YDOT = -1032.909804 meter/sec
ZDOT = 6505.025678 ZDOT = 1982.731827
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 10077.51250883 .00016717 00000-0 10270-3 0 9138
2 25544 51.6484 336.1187 0007699 58.9131 301.2787 15.74095011 9197
Satellite: ISS
Catalog Number: 25544
Epoch time: 10077.51250883 = yrday.fracday
Element set: 913
Inclination: 51.6484 deg
RA of node: 336.1187 deg
Eccentricity: .0007699
Arg of perigee: 58.9131 deg
Mean anomaly: 301.2787 deg
Mean motion: 15.74095011 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 919
Checksum: 319
Coasting Arc #15 (Orbit 934)
Vector Time (GMT): 2010/078/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6212427.15 A = 6730469.65 meter
Y = 1892948.05 meter E = .0011521
Z = -1770970.43 I = 51.49874
XDOT = 24.083950 Wp = 101.52850
YDOT = -5197.629223 meter/sec RA = 330.52576 deg
ZDOT = -5673.470392 TA = 98.11521
MA = 97.98449
Ha = 192.552 n.mi
Hp = 181.065
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20381978.83 X = -6224529.62
Y = 6210459.49 feet Y = 1823409.20 meter
Z = -5810270.44 Z = -1801180.04
XDOT = 79.015583 XDOT = 109.763768
YDOT = -17052.589315 feet/sec YDOT = -5196.881271 meter/sec
ZDOT = -18613.748006 ZDOT = -5673.144881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20718207.58 X = -6314909.67
Y = 4831440.04 feet Y = 1472622.92 meter
Z = -5930191.62 Z = -1807522.40
XDOT = 1684.286129 XDOT = 513.370412
YDOT = -15491.174275 feet/sec YDOT = -4721.709919 meter/sec
ZDOT = -18612.563857 ZDOT = -5673.109464
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 10078.52827227 .00016717 00000-0 10270-3 0 9143
2 25544 51.6484 330.9019 0007531 63.1550 297.0382 15.74098218 9354
Satellite: ISS
Catalog Number: 25544
Epoch time: 10078.52827227 = yrday.fracday
Element set: 914
Inclination: 51.6484 deg
RA of node: 330.9019 deg
Eccentricity: .0007531
Arg of perigee: 63.1550 deg
Mean anomaly: 297.0382 deg
Mean motion: 15.74098218 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 935
Checksum: 311
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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