ISS TRAJECTORY DATA
Lift off time (UTC) : N/A
Area (sq ft) : 9256.96
Drag Coefficient (Cd) : 2.00
Monthly MSFC 50% solar flux (F10.7-jansky) : 71.3
Monthly MSFC 50% earth geomagnetic index (Kp) : 2.07
ET - UTC (sec) : 65.18
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 2242)
---------------------------------------
Vector Time (GMT): 2008/130/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 615213.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 213473.80 A = 6715477.05 meter
Y = -4599788.86 meter E = .0010581
Z = 4887941.70 I = 51.43921
XDOT = 6887.627628 Wp = 157.41052
YDOT = 2664.431997 meter/sec RA = 214.85672 deg
ZDOT = 2195.354167 TA = 271.15777
MA = 271.27900
Ha = 187.506 n.mi
Hp = 180.502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 700373.36 X = 241148.65
Y = -15091170.79 feet Y = -4597247.58 meter
Z = 16036554.15 Z = 4889045.38
XDOT = 22597.203505 XDOT = 6846.656947
YDOT = 8741.574793 feet/sec YDOT = 2741.224018 meter/sec
ZDOT = 7202.605534 ZDOT = 2228.715248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10607075.96 X = -3233036.75
Y = -10751900.35 feet Y = -3277179.23 meter
Z = 16040311.91 Z = 4889087.07
XDOT = 21006.359462 XDOT = 6402.738364
YDOT = -9731.818552 feet/sec YDOT = -2966.258295 meter/sec
ZDOT = 7330.989741 ZDOT = 2234.485673
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 08130.55138401 .00020000 00000-0 20000-3 0 9008
2 25544 51.6409 215.5337 0006386 192.6751 167.4254 15.76207648 22433
Satellite: ISS
Catalog Number: 25544
Epoch time: 08130.55138401 = yrday.fracday
Element set: 900
Inclination: 51.6409 deg
RA of node: 215.5337 deg
Eccentricity: .0006386
Arg of perigee: 192.6751 deg
Mean anomaly: 167.4254 deg
Mean motion: 15.76207648 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 2243
Checksum: 283
Coasting Arc #2 (Orbit 2257)
---------------------------------------
Vector Time (GMT): 2008/131/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 615213.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6162633.98 A = 6725319.13 meter
Y = -2408145.20 meter E = .0004049
Z = -1203364.35 I = 51.49652
XDOT = 782.369713 Wp = 69.57242
YDOT = -4924.759337 meter/sec RA = 209.66306 deg
ZDOT = 5865.947790 TA = 277.20961
MA = 277.25564
Ha = 187.335 n.mi
Hp = 180.733
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20218615.42 X = -6129401.97
Y = -7900738.86 feet Y = -2476873.36 meter
Z = -3948045.78 Z = -1233222.01
XDOT = 2566.829767 XDOT = 808.885264
YDOT = -16157.346907 feet/sec YDOT = -4915.862835 meter/sec
ZDOT = 19245.235531 ZDOT = 5869.812398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19400529.75 X = -5913281.47
Y = 9690866.66 feet Y = 2953776.16 meter
Z = -4062966.71 Z = -1238392.25
XDOT = -9636.110057 XDOT = -2937.086346
YDOT = -11239.297033 feet/sec YDOT = -3425.737736 meter/sec
ZDOT = 19259.559056 ZDOT = 5870.313600
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 08131.50239849 .00020000 00000-0 20000-3 0 9013
2 25544 51.6403 210.6345 0006099 196.9589 163.1372 15.76174627 22589
Satellite: ISS
Catalog Number: 25544
Epoch time: 08131.50239849 = yrday.fracday
Element set: 901
Inclination: 51.6403 deg
RA of node: 210.6345 deg
Eccentricity: .0006099
Arg of perigee: 196.9589 deg
Mean anomaly: 163.1372 deg
Mean motion: 15.76174627 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 2258
Checksum: 304
Coasting Arc #3 (Orbit 2273)
---------------------------------------
Vector Time (GMT): 2008/132/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 615213.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1216464.82 A = 6713884.76 meter
Y = 4029818.22 meter E = .0013511
Z = -5240915.63 I = 51.48350
XDOT = -7145.192114 Wp = 110.46711
YDOT = -2812.644158 meter/sec RA = 204.51633 deg
ZDOT = -509.923934 TA = 154.70807
MA = 154.64186
Ha = 187.136 n.mi
Hp = 180.802
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3991026.32 X = -1235977.07
Y = 13221188.39 feet Y = 4016106.39 meter
Z = -17194605.10 Z = -5246872.25
XDOT = -23442.231344 XDOT = -7110.732522
YDOT = -9227.835164 feet/sec YDOT = -2892.353064 meter/sec
ZDOT = -1672.978787 ZDOT = -544.551813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7402543.75 X = 2256295.34
Y = 11625742.48 feet Y = 3543526.31 meter
Z = -17217055.96 Z = -5247758.66
XDOT = -21511.003366 XDOT = -6556.553826
YDOT = 11049.544541 feet/sec YDOT = 3367.901176 meter/sec
ZDOT = -1806.279139 ZDOT = -550.553882
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 08132.51679482 .00020000 00000-0 20000-3 0 9027
2 25544 51.6395 205.4079 0006152 200.8933 159.1980 15.76218254 22746
Satellite: ISS
Catalog Number: 25544
Epoch time: 08132.51679482 = yrday.fracday
Element set: 902
Inclination: 51.6395 deg
RA of node: 205.4079 deg
Eccentricity: .0006152
Arg of perigee: 200.8933 deg
Mean anomaly: 159.1980 deg
Mean motion: 15.76218254 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 2274
Checksum: 295
Coasting Arc #4 (Orbit 2289)
---------------------------------------
Vector Time (GMT): 2008/133/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 615213.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6239207.20 A = 6725696.31 meter
Y = 2465221.07 meter E = .0015115
Z = -325264.52 I = 51.55110
XDOT = -2030.777869 Wp = 158.83513
YDOT = 4357.843401 meter/sec RA = 199.35365 deg
ZDOT = -6026.068256 TA = 24.71009
MA = 24.63776
Ha = 186.970 n.mi
Hp = 180.860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20469839.89 X = 6212757.07
Y = 8087995.64 feet Y = 2534843.59 meter
Z = -1067140.82 Z = -295018.51
XDOT = -6662.657049 XDOT = -2050.083458
YDOT = 14297.386487 feet/sec YDOT = 4335.026551 meter/sec
ZDOT = -19770.565144 ZDOT = -6035.980376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19379159.86 X = 5906767.92
Y = -10445723.99 feet Y = -3183856.67 meter
Z = -950695.36 Z = -289771.95
XDOT = 5950.567328 XDOT = 1813.732922
YDOT = 12808.770434 feet/sec YDOT = 3904.113228 meter/sec
ZDOT = -19808.173628 ZDOT = -6037.531322
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 08133.53117264 .00020000 00000-0 20000-3 0 9036
2 25544 51.6396 200.1812 0005982 203.4523 156.6370 15.76269579 22907
Satellite: ISS
Catalog Number: 25544
Epoch time: 08133.53117264 = yrday.fracday
Element set: 903
Inclination: 51.6396 deg
RA of node: 200.1812 deg
Eccentricity: .0005982
Arg of perigee: 203.4523 deg
Mean anomaly: 156.6370 deg
Mean motion: 15.76269579 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 2290
Checksum: 285
Coasting Arc #5 (Orbit 2305)
---------------------------------------
Vector Time (GMT): 2008/134/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 615213.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2342842.94 A = 6713950.27 meter
Y = -3622114.48 meter E = .0002976
Z = 5143893.03 I = 51.54057
XDOT = 7067.728678 Wp = 172.61509
YDOT = 2806.434975 meter/sec RA = 194.18073 deg
ZDOT = -1245.725566 TA = 289.28310
MA = 289.31529
Ha = 186.653 n.mi
Hp = 181.012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7686492.59 X = 2358183.68
Y = -11883577.69 feet Y = -3595829.97 meter
Z = 16876289.46 Z = 5155311.67
XDOT = 23188.086215 XDOT = 7041.872923
YDOT = 9207.463829 feet/sec YDOT = 2885.325861 meter/sec
ZDOT = -4087.026136 ZDOT = -1211.453067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4427053.80 X = -1349366.00
Y = -13387810.97 feet Y = -4080604.78 meter
Z = 16919764.92 Z = 5157144.35
XDOT = 20815.105478 XDOT = 6344.444150
YDOT = -11869.901092 feet/sec YDOT = -3617.945853 meter/sec
ZDOT = -3955.066487 ZDOT = -1205.504265
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 08134.54552997 .00020000 00000-0 20000-3 0 9045
2 25544 51.6400 194.9542 0005994 209.1928 150.8902 15.76327109 23067
Satellite: ISS
Catalog Number: 25544
Epoch time: 08134.54552997 = yrday.fracday
Element set: 904
Inclination: 51.6400 deg
RA of node: 194.9542 deg
Eccentricity: .0005994
Arg of perigee: 209.1928 deg
Mean anomaly: 150.8902 deg
Mean motion: 15.76327109 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 2306
Checksum: 304
Coasting Arc #6 (Orbit 2321)
---------------------------------------
Vector Time (GMT): 2008/135/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 615213.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5991732.27 A = 6724224.00 meter
Y = -2428862.29 meter E = .0009999
Z = 1837399.76 I = 51.60299
XDOT = 3364.710745 Wp = 84.96355
YDOT = -4002.707185 meter/sec RA = 189.05000 deg
ZDOT = 5655.654648 TA = 295.45077
MA = 295.55420
Ha = 186.605 n.mi
Hp = 181.160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19657914.28 X = -5973052.86
Y = -7968708.30 feet Y = -2495760.91 meter
Z = 6028214.43 Z = 1808336.95
XDOT = 11039.077246 XDOT = 3381.745207
YDOT = -13132.241419 feet/sec YDOT = -3964.986089 meter/sec
ZDOT = 18555.297402 ZDOT = 5672.041728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18430477.45 X = -5617609.53
Y = 10563529.63 feet Y = 3219763.83 meter
Z = 5916301.03 Z = 1803288.55
XDOT = -2803.355763 XDOT = -854.462837
YDOT = -15365.957174 feet/sec YDOT = -4683.543747 meter/sec
ZDOT = 18617.821637 ZDOT = 5674.712035
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 08135.55987296 .00020000 00000-0 20000-3 0 9052
2 25544 51.6395 189.7270 0005679 211.4440 148.6385 15.76302181 23226
Satellite: ISS
Catalog Number: 25544
Epoch time: 08135.55987296 = yrday.fracday
Element set: 905
Inclination: 51.6395 deg
RA of node: 189.7270 deg
Eccentricity: .0005679
Arg of perigee: 211.4440 deg
Mean anomaly: 148.6385 deg
Mean motion: 15.76302181 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 2322
Checksum: 310
Coasting Arc #7 (Orbit 2336)
---------------------------------------
Vector Time (GMT): 2008/136/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 615213.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3516258.05 A = 6716202.96 meter
Y = 3416476.50 meter E = .0010622
Z = -4600007.59 I = 51.60589
XDOT = -6548.635874 Wp = 140.87911
YDOT = -2775.983071 meter/sec RA = 183.85502 deg
ZDOT = 2939.621288 TA = 158.30924
MA = 158.26422
Ha = 186.351 n.mi
Hp = 181.106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11536279.68 X = -3531854.00
Y = 11208912.39 feet Y = 3377068.72 meter
Z = -15091888.42 Z = -4617127.49
XDOT = -21485.025834 XDOT = -6531.388010
YDOT = -9107.556007 feet/sec YDOT = -2849.117380 meter/sec
ZDOT = 9644.426798 ZDOT = 2907.849369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2015584.40 X = 614350.13
Y = 15896048.47 feet Y = 4845115.57 meter
Z = -15157296.08 Z = -4619943.85
XDOT = -19110.594464 XDOT = -5824.909192
YDOT = 11516.483492 feet/sec YDOT = 3510.224168 meter/sec
ZDOT = 9522.061610 ZDOT = 2902.324379
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 08136.51080025 .00020000 00000-0 20000-3 0 9064
2 25544 51.6396 184.8264 0005636 215.5282 144.5508 15.76350772 23375
Satellite: ISS
Catalog Number: 25544
Epoch time: 08136.51080025 = yrday.fracday
Element set: 906
Inclination: 51.6396 deg
RA of node: 184.8264 deg
Eccentricity: .0005636
Arg of perigee: 215.5282 deg
Mean anomaly: 144.5508 deg
Mean motion: 15.76350772 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 2337
Checksum: 291
Coasting Arc #8 (Orbit 2352)
---------------------------------------
Vector Time (GMT): 2008/137/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 615213.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5350320.38 A = 6720882.57 meter
Y = 2449195.66 meter E = .0005111
Z = -3242828.78 I = 51.65154
XDOT = -4655.343320 Wp = 168.22624
YDOT = 3871.050036 meter/sec RA = 178.74828 deg
ZDOT = -4763.373448 TA = 49.75764
MA = 49.71295
Ha = 186.251 n.mi
Hp = 181.303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17553544.56 X = 5338288.78
Y = 8035418.82 feet Y = 2508958.94 meter
Z = -10639202.03 Z = -3216865.56
XDOT = -15273.436088 XDOT = -4675.144025
YDOT = 12700.295394 feet/sec YDOT = 3818.880923 meter/sec
ZDOT = -15627.865644 ZDOT = -4786.037322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16883363.15 X = 5146049.09
Y = -9474447.30 feet Y = -2887811.54 meter
Z = -10539183.99 Z = -3212343.28
XDOT = 597.482437 XDOT = 182.112647
YDOT = 18522.303816 feet/sec YDOT = 5645.598203 meter/sec
ZDOT = -15714.532555 ZDOT = -4789.789523
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 08137.52510631 .00020000 00000-0 20000-3 0 9078
2 25544 51.6400 179.5991 0005562 218.8350 141.2415 15.76389579 23535
Satellite: ISS
Catalog Number: 25544
Epoch time: 08137.52510631 = yrday.fracday
Element set: 907
Inclination: 51.6400 deg
RA of node: 179.5991 deg
Eccentricity: .0005562
Arg of perigee: 218.8350 deg
Mean anomaly: 141.2415 deg
Mean motion: 15.76389579 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 2353
Checksum: 295
Coasting Arc #9 (Orbit 2368)
---------------------------------------
Vector Time (GMT): 2008/138/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 615213.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4542347.80 A = 6719506.80 meter
Y = -3382714.65 meter E = .0008665
Z = 3606366.16 I = 51.67565
XDOT = 5637.445300 Wp = 110.62773
YDOT = 2867.011623 meter/sec RA = 173.54523 deg
ZDOT = -4405.874775 TA = 26.16397
MA = 26.12022
Ha = 185.856 n.mi
Hp = 181.330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14902715.88 X = 4562316.84
Y = -11098145.17 feet Y = -3331808.17 meter
Z = 11831909.99 Z = 3628481.53
XDOT = 18495.555446 XDOT = 5626.370288
YDOT = 9406.206111 feet/sec YDOT = 2929.991212 meter/sec
ZDOT = -14454.969733 ZDOT = -4378.514196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -519858.34 X = -158452.82
Y = -18519716.32 feet Y = -5644809.53 meter
Z = 11916531.18 Z = 3632158.70
XDOT = 17043.046804 XDOT = 5194.720666
YDOT = -9723.112974 feet/sec YDOT = -2963.604834 meter/sec
ZDOT = -14349.533032 ZDOT = -4373.737668
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 08138.53939355 .00020000 00000-0 20000-3 0 9089
2 25544 51.6389 174.3719 0005492 223.8315 136.2414 15.76432258 23694
Satellite: ISS
Catalog Number: 25544
Epoch time: 08138.53939355 = yrday.fracday
Element set: 908
Inclination: 51.6389 deg
RA of node: 174.3719 deg
Eccentricity: .0005492
Arg of perigee: 223.8315 deg
Mean anomaly: 136.2414 deg
Mean motion: 15.76432258 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 2369
Checksum: 315
Coasting Arc #10 (Orbit 2384)
---------------------------------------
Vector Time (GMT): 2008/139/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 615213.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4402505.92 A = 6717109.57 meter
Y = -2607875.93 meter E = .0008636
Z = 4351189.41 I = 51.69559
XDOT = 5695.060121 Wp = 143.01536
YDOT = -3911.627592 meter/sec RA = 168.44463 deg
ZDOT = 3407.541362 TA = 272.62511
MA = 272.72396
Ha = 185.882 n.mi
Hp = 181.409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14443917.07 X = -4394154.76
Y = -8556023.41 feet Y = -2657061.04 meter
Z = 14275555.80 Z = 4329821.60
XDOT = 18684.580450 XDOT = 5721.823725
YDOT = -12833.423858 feet/sec YDOT = -3847.792892 meter/sec
ZDOT = 11179.597645 ZDOT = 3435.273126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15241510.44 X = -4645612.38
Y = 7202365.00 feet Y = 2195280.85 meter
Z = 14193169.78 Z = 4326078.15
XDOT = 379.883597 XDOT = 115.788520
YDOT = -21502.820751 feet/sec YDOT = -6554.059765 meter/sec
ZDOT = 11285.757883 ZDOT = 3439.899003
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 08139.55366473 .00020000 00000-0 20000-3 0 9098
2 25544 51.6383 169.1438 0005356 226.3990 133.6731 15.76431267 23854
Satellite: ISS
Catalog Number: 25544
Epoch time: 08139.55366473 = yrday.fracday
Element set: 909
Inclination: 51.6383 deg
RA of node: 169.1438 deg
Eccentricity: .0005356
Arg of perigee: 226.3990 deg
Mean anomaly: 133.6731 deg
Mean motion: 15.76431267 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 2385
Checksum: 314
Coasting Arc #11 (Orbit 2399)
---------------------------------------
Vector Time (GMT): 2008/140/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 615213.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5309715.75 A = 6722797.10 meter
Y = 3452787.75 meter E = .0000755
Z = -2252759.75 I = 51.74503
XDOT = -4389.238832 Wp = 358.37021
YDOT = -3182.164942 meter/sec RA = 163.25188 deg
ZDOT = 5468.775077 TA = 336.36793
MA = 336.37139
Ha = 185.588 n.mi
Hp = 181.371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17420327.26 X = -5336987.01
Y = 11328043.81 feet Y = 3393259.28 meter
Z = -7390944.08 Z = -2278620.68
XDOT = -14400.389869 XDOT = -4379.895995
YDOT = -10440.173694 feet/sec YDOT = -3231.196379 meter/sec
ZDOT = 17942.175449 ZDOT = 5447.474013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -44221.90 X = -13478.84
Y = 20744076.68 feet Y = 6322794.57 meter
Z = -7489977.29 Z = -2282945.08
XDOT = -15166.469553 XDOT = -4622.739920
YDOT = 6415.484854 feet/sec YDOT = 1955.439783 meter/sec
ZDOT = 17859.981515 ZDOT = 5443.722366
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 08140.50452668 .00020000 00000-0 20000-3 0 9109
2 25544 51.6391 164.2431 0005395 229.8014 130.2679 15.76499141 24007
Satellite: ISS
Catalog Number: 25544
Epoch time: 08140.50452668 = yrday.fracday
Element set: 910
Inclination: 51.6391 deg
RA of node: 164.2431 deg
Eccentricity: .0005395
Arg of perigee: 229.8014 deg
Mean anomaly: 130.2679 deg
Mean motion: 15.76499141 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 2400
Checksum: 278
Coasting Arc #12 (Orbit 2415)
---------------------------------------
Vector Time (GMT): 2008/141/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 615213.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3214303.74 A = 6714002.10 meter
Y = 3018585.74 meter E = .0008760
Z = -5070482.78 I = 51.74207
XDOT = -6374.060232 Wp = 90.85950
YDOT = 3979.701126 meter/sec RA = 158.13899 deg
ZDOT = -1674.060955 TA = 163.07846
MA = 163.04923
Ha = 185.445 n.mi
Hp = 181.678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10545615.95 X = 3204942.48
Y = 9903496.54 feet Y = 3054478.32 meter
Z = -16635442.21 Z = -5054889.71
XDOT = -20912.271101 XDOT = -6409.955705
YDOT = 13056.762223 feet/sec YDOT = 3908.222280 meter/sec
ZDOT = -5492.325967 ZDOT = -1705.113320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14052373.83 X = 4283163.54
Y = -3717627.58 feet Y = -1133132.89 meter
Z = -16575199.30 Z = -5052120.75
XDOT = -364.540034 XDOT = -111.111802
YDOT = 23601.949669 feet/sec YDOT = 7193.874259 meter/sec
ZDOT = -5611.275091 ZDOT = -1710.316648
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 08141.51876241 .00020000 00000-0 20000-3 0 9119
2 25544 51.6386 159.0150 0005417 235.2106 124.8549 15.76481403 24163
Satellite: ISS
Catalog Number: 25544
Epoch time: 08141.51876241 = yrday.fracday
Element set: 911
Inclination: 51.6386 deg
RA of node: 159.0150 deg
Eccentricity: .0005417
Arg of perigee: 235.2106 deg
Mean anomaly: 124.8549 deg
Mean motion: 15.76481403 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 2416
Checksum: 274
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