ISS TRAJECTORY DATA
Lift off time (UTC) : N/A
Area (sq ft) : 8611.13
Drag Coefficient (Cd) : 2.00
Monthly MSFC 50% solar flux (F10.7-jansky) : 72.1
Monthly MSFC 50% earth geomagnetic index (Kp) : 2.19
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 1009)
---------------------------------------
Vector Time (GMT): 2009/194/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1083731.96 A = 6719244.83 meter
Y = 4041775.52 meter E = .0011213
Z = -5265632.56 I = 51.66783
XDOT = -7531.196620 Wp = 114.84032
YDOT = 1530.204177 meter/sec RA = 170.75967 deg
ZDOT = -380.715399 TA = 151.57389
MA = 151.51268
Ha = 189.619 n.mi
Hp = 184.728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3555551.06 X = 1064034.91
Y = 13260418.39 feet Y = 4053784.82 meter
Z = -17275697.37 Z = -5260415.28
XDOT = -24708.650328 XDOT = -7545.898454
YDOT = 5020.354911 feet/sec YDOT = 1445.903761 meter/sec
ZDOT = -1249.066269 ZDOT = -417.337270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11106685.02 X = 3385317.60
Y = -8114068.74 feet Y = -2473168.15 meter
Z = -17254964.35 Z = -5259313.13
XDOT = 12849.231736 XDOT = 3916.445833
YDOT = 20513.394124 feet/sec YDOT = 6252.482529 meter/sec
ZDOT = -1392.778884 ZDOT = -424.519004
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 09194.51659774 .00010596 00000-0 82463-4 0 9007
2 25544 51.6362 171.6940 0007249 220.8002 139.2619 15.74320561 10106
Satellite: ISS
Catalog Number: 25544
Epoch time: 09194.51659774 = yrday.fracday
Element set: 900
Inclination: 51.6362 deg
RA of node: 171.6940 deg
Eccentricity: .0007249
Arg of perigee: 220.8002 deg
Mean anomaly: 139.2619 deg
Mean motion: 15.74320561 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 1010
Checksum: 293
Coasting Arc #2 (Orbit 1025)
---------------------------------------
Vector Time (GMT): 2009/195/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6467813.37 A = 6731138.41 meter
Y = -1819749.74 meter E = .0014239
Z = 198465.16 I = 51.73791
XDOT = 1467.586747 Wp = 163.16229
YDOT = 4546.476326 meter/sec RA = 165.62069 deg
ZDOT = -6046.199472 TA = 14.68271
MA = 14.64140
Ha = 189.349 n.mi
Hp = 184.861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21219860.14 X = 6486717.31
Y = -5970307.56 feet Y = -1747317.19 meter
Z = 651132.42 Z = 229931.45
XDOT = 4814.917148 XDOT = 1446.009460
YDOT = 14916.260913 feet/sec YDOT = 4562.767700 meter/sec
ZDOT = -19836.612440 ZDOT = -6039.121911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13398327.51 X = -4083810.22
Y = -17499595.33 feet Y = -5333876.66 meter
Z = 774592.38 Z = 236095.76
XDOT = 10756.002381 XDOT = 3278.429526
YDOT = -9123.464176 feet/sec YDOT = -2780.831881 meter/sec
ZDOT = -19808.543285 ZDOT = -6037.643993
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 09195.53220718 .00010596 00000-0 82463-4 0 9013
2 25544 51.6366 166.4755 0007192 225.8436 134.2136 15.74357923 10267
Satellite: ISS
Catalog Number: 25544
Epoch time: 09195.53220718 = yrday.fracday
Element set: 901
Inclination: 51.6366 deg
RA of node: 166.4755 deg
Eccentricity: .0007192
Arg of perigee: 225.8436 deg
Mean anomaly: 134.2136 deg
Mean motion: 15.74357923 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 1026
Checksum: 310
Coasting Arc #3 (Orbit 1041)
---------------------------------------
Vector Time (GMT): 2009/196/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1470467.56 A = 6719062.62 meter
Y = -3895555.93 meter E = .0005823
Z = 5276120.04 I = 51.72578
XDOT = 7237.761165 Wp = 213.12735
YDOT = -2625.791445 meter/sec RA = 160.49255 deg
ZDOT = 73.717654 TA = 236.14617
MA = 236.20160
Ha = 189.216 n.mi
Hp = 185.069
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4824368.64 X = -1452427.95
Y = -12780695.30 feet Y = -3911899.28 meter
Z = 17310105.12 Z = 5269019.89
XDOT = 23745.935580 XDOT = 7266.227177
YDOT = -8614.801328 feet/sec YDOT = -2544.695408 meter/sec
ZDOT = 241.855820 ZDOT = 108.947566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9888597.40 X = -3014044.49
Y = 9476760.95 feet Y = 2888516.74 meter
Z = 17281987.38 Z = 5267549.75
XDOT = -16421.859259 XDOT = -5005.382702
YDOT = -17857.028987 feet/sec YDOT = -5442.822435 meter/sec
ZDOT = 380.060091 ZDOT = 115.842316
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 09196.54780467 .00010596 00000-0 82463-4 0 9028
2 25544 51.6365 161.2573 0007232 230.0953 129.9575 15.74364502 10421
Satellite: ISS
Catalog Number: 25544
Epoch time: 09196.54780467 = yrday.fracday
Element set: 902
Inclination: 51.6365 deg
RA of node: 161.2573 deg
Eccentricity: .0007232
Arg of perigee: 230.0953 deg
Mean anomaly: 129.9575 deg
Mean motion: 15.74364502 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 1042
Checksum: 309
Coasting Arc #4 (Orbit 1057)
---------------------------------------
Vector Time (GMT): 2009/197/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6141689.45 A = 6731015.31 meter
Y = 2746039.26 meter E = .0005232
Z = 81692.99 I = 51.79396
XDOT = -1874.515815 Wp = 35.93376
YDOT = -4378.085269 meter/sec RA = 155.36226 deg
ZDOT = 6048.787009 TA = 324.95161
MA = 324.98603
Ha = 188.970 n.mi
Hp = 185.194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20149899.77 X = -6172336.51
Y = 9009315.14 feet Y = 2677187.92 meter
Z = 268021.61 Z = 51782.52
XDOT = -6149.986269 XDOT = -1854.803969
YDOT = -14363.796814 feet/sec YDOT = -4398.937782 meter/sec
ZDOT = 19845.101735 ZDOT = 6039.727897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16347413.12 X = 4982691.52
Y = 14832310.30 feet Y = 4520888.18 meter
Z = 150702.04 Z = 45933.98
XDOT = -9553.552585 XDOT = -2911.922828
YDOT = 10316.877302 feet/sec YDOT = 3144.584202 meter/sec
ZDOT = 19809.262856 ZDOT = 6037.863318
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 09197.56338798 .00010596 00000-0 82463-4 0 9038
2 25544 51.6362 156.0383 0007265 233.2978 126.7518 15.74407449 10584
Satellite: ISS
Catalog Number: 25544
Epoch time: 09197.56338798 = yrday.fracday
Element set: 903
Inclination: 51.6362 deg
RA of node: 156.0383 deg
Eccentricity: .0007265
Arg of perigee: 233.2978 deg
Mean anomaly: 126.7518 deg
Mean motion: 15.74407449 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 1058
Checksum: 342
Coasting Arc #5 (Orbit 1072)
---------------------------------------
Vector Time (GMT): 2009/198/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1796655.89 A = 6718968.34 meter
Y = 3760450.73 meter E = .0009836
Z = -5277968.51 I = 51.78059
XDOT = -6780.092202 Wp = 116.26590
YDOT = 3629.478964 meter/sec RA = 150.23107 deg
ZDOT = 274.073194 TA = 156.35499
MA = 156.30975
Ha = 188.748 n.mi
Hp = 185.472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5894540.34 X = 1780111.81
Y = 12337436.78 feet Y = 3780450.30 meter
Z = -17316169.64 Z = -5269279.94
XDOT = -22244.396989 XDOT = -6821.505141
YDOT = 11907.739384 feet/sec YDOT = 3553.428411 meter/sec
ZDOT = 899.190270 ZDOT = 241.035426
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8707148.63 X = 2653938.90
Y = -10598671.02 feet Y = -3230474.93 meter
Z = -17281823.34 Z = -5267499.76
XDOT = 19336.996938 XDOT = 5893.916667
YDOT = 14610.294864 feet/sec YDOT = 4453.217875 meter/sec
ZDOT = 769.620315 ZDOT = 234.580272
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 09198.51548710 .00010596 00000-0 82463-4 0 9042
2 25544 51.6369 151.1454 0007258 238.3409 121.7047 15.74403278 10738
Satellite: ISS
Catalog Number: 25544
Epoch time: 09198.51548710 = yrday.fracday
Element set: 904
Inclination: 51.6369 deg
RA of node: 151.1454 deg
Eccentricity: .0007258
Arg of perigee: 238.3409 deg
Mean anomaly: 121.7047 deg
Mean motion: 15.74403278 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 1073
Checksum: 310
Coasting Arc #6 (Orbit 1088)
---------------------------------------
Vector Time (GMT): 2009/199/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5678248.33 A = 6730911.57 meter
Y = -3577256.22 meter E = .0011951
Z = -399203.82 I = 51.84704
XDOT = 2238.794932 Wp = 174.20381
YDOT = 4224.824955 meter/sec RA = 145.11095 deg
ZDOT = -6041.322154 TA = 10.12676
MA = 10.10270
Ha = 188.545 n.mi
Hp = 185.545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18629423.65 X = 5719767.05
Y = -11736404.92 feet Y = -3513526.51 meter
Z = -1309723.83 Z = -371518.72
XDOT = 7345.127729 XDOT = 2220.733421
YDOT = 13860.974263 feet/sec YDOT = 4249.760552 meter/sec
ZDOT = -19820.610741 ZDOT = -6030.489229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18650124.05 X = -5684557.81
Y = -11715122.42 feet Y = -3570769.31 meter
Z = -1201158.57 Z = -366113.13
XDOT = 8407.913508 XDOT = 2562.732037
YDOT = -11367.303789 feet/sec YDOT = -3464.754195 meter/sec
ZDOT = -19777.813754 ZDOT = -6028.277632
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 09199.53104656 .00010596 00000-0 82463-4 0 9053
2 25544 51.6376 145.9267 0007264 242.4182 117.6244 15.74425002 10899
Satellite: ISS
Catalog Number: 25544
Epoch time: 09199.53104656 = yrday.fracday
Element set: 905
Inclination: 51.6376 deg
RA of node: 145.9267 deg
Eccentricity: .0007264
Arg of perigee: 242.4182 deg
Mean anomaly: 117.6244 deg
Mean motion: 15.74425002 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 1089
Checksum: 312
Coasting Arc #7 (Orbit 1104)
---------------------------------------
Vector Time (GMT): 2009/200/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2111894.28 A = 6718906.63 meter
Y = -3620218.32 meter E = .0004408
Z = 5254784.76 I = 51.83122
XDOT = 6187.107850 Wp = 248.03759
YDOT = -4537.333884 meter/sec RA = 139.97786 deg
ZDOT = -641.386411 TA = 208.03298
MA = 208.05672
Ha = 188.301 n.mi
Hp = 185.674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6928787.01 X = -2096782.03
Y = -11877356.69 feet Y = -3643751.26 meter
Z = 17240107.48 Z = 5244561.27
XDOT = 20298.910269 XDOT = 6240.500967
YDOT = -14886.266025 feet/sec YDOT = -4467.847365 meter/sec
ZDOT = -2104.286124 ZDOT = -611.200826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7462520.43 X = -2274576.23
Y = 11609515.65 feet Y = 3538580.37 meter
Z = 17199736.40 Z = 5242479.66
XDOT = -21568.434220 XDOT = -6574.058750
YDOT = -10931.797116 feet/sec YDOT = -3332.011761 meter/sec
ZDOT = -1985.929547 ZDOT = -605.311326
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 09200.54659252 .00010596 00000-0 82463-4 0 9065
2 25544 51.6381 140.7084 0007289 246.8660 113.1736 15.74459885 11053
Satellite: ISS
Catalog Number: 25544
Epoch time: 09200.54659252 = yrday.fracday
Element set: 906
Inclination: 51.6381 deg
RA of node: 140.7084 deg
Eccentricity: .0007289
Arg of perigee: 246.8660 deg
Mean anomaly: 113.1736 deg
Mean motion: 15.74459885 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 1105
Checksum: 318
Coasting Arc #8 (Orbit 1120)
---------------------------------------
Vector Time (GMT): 2009/201/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5105995.14 A = 6730625.51 meter
Y = 4317387.34 meter E = .0006863
Z = 730814.69 I = 51.89300
XDOT = -2584.049940 Wp = 33.23660
YDOT = -4075.338190 meter/sec RA = 134.86631 deg
ZDOT = 6000.815486 TA = 334.70003
MA = 334.73363
Ha = 188.002 n.mi
Hp = 185.846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16751952.57 X = -5157443.53
Y = 14164656.62 feet Y = 4260001.31 meter
Z = 2397686.01 Z = 705885.97
XDOT = -8477.854134 XDOT = -2567.437221
YDOT = -13370.532121 feet/sec YDOT = -4104.142796 meter/sec
ZDOT = 19687.714849 ZDOT = 5988.301928
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20325395.97 X = 6195180.69
Y = 8282680.27 feet Y = 2524560.95 meter
Z = 2299955.76 Z = 701026.52
XDOT = -7255.398904 XDOT = -2211.445586
YDOT = 12331.536302 feet/sec YDOT = 3758.652265 meter/sec
ZDOT = 19638.314948 ZDOT = 5985.758396
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 09201.56212604 .00010596 00000-0 82463-4 0 9075
2 25544 51.6383 135.4888 0007296 250.8504 109.1869 15.74470314 11218
Satellite: ISS
Catalog Number: 25544
Epoch time: 09201.56212604 = yrday.fracday
Element set: 907
Inclination: 51.6383 deg
RA of node: 135.4888 deg
Eccentricity: .0007296
Arg of perigee: 250.8504 deg
Mean anomaly: 109.1869 deg
Mean motion: 15.74470314 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 1121
Checksum: 303
Coasting Arc #9 (Orbit 1135)
---------------------------------------
Vector Time (GMT): 2009/202/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2404562.08 A = 6719041.55 meter
Y = 3504729.93 meter E = .0008318
Z = -5210742.88 I = 51.87538
XDOT = -5474.315739 Wp = 118.11483
YDOT = 5308.241537 meter/sec RA = 129.72881 deg
ZDOT = 1041.534667 TA = 161.80604
MA = 161.77626
Ha = 187.750 n.mi
Hp = 185.975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7888983.20 X = 2390505.20
Y = 11498457.78 feet Y = 3531541.44 meter
Z = -17095613.11 Z = -5199095.30
XDOT = -17960.353475 XDOT = -5538.326022
YDOT = 17415.490607 feet/sec YDOT = 5246.666457 meter/sec
ZDOT = 3417.108488 ZDOT = 1014.786408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6266621.95 X = 1910066.37
Y = -12519973.97 feet Y = -3816088.07 meter
Z = -17049641.52 Z = -5196730.74
XDOT = 22987.183053 XDOT = 7006.493395
YDOT = 6983.579838 feet/sec YDOT = 2128.595135 meter/sec
ZDOT = 3312.266487 ZDOT = 1009.578825
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 09202.51417667 .00010596 00000-0 82463-4 0 9088
2 25544 51.6393 130.5961 0007295 254.8012 105.2345 15.74489356 11362
Satellite: ISS
Catalog Number: 25544
Epoch time: 09202.51417667 = yrday.fracday
Element set: 908
Inclination: 51.6393 deg
RA of node: 130.5961 deg
Eccentricity: .0007295
Arg of perigee: 254.8012 deg
Mean anomaly: 105.2345 deg
Mean motion: 15.74489356 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 1136
Checksum: 310
Coasting Arc #10 (Orbit 1151)
---------------------------------------
Vector Time (GMT): 2009/203/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4443104.52 A = 6730258.07 meter
Y = -4927174.08 meter E = .0009179
Z = -1093267.90 I = 51.93222
XDOT = 2920.315189 Wp = 187.96654
YDOT = 3949.335637 meter/sec RA = 124.62767 deg
ZDOT = -5933.652723 TA = 3.95197
MA = 3.94472
Ha = 187.543 n.mi
Hp = 185.935
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14577114.57 X = 4503181.57
Y = -16165269.28 feet Y = -4877152.62 meter
Z = -3586836.95 Z = -1071538.58
XDOT = 9581.086578 XDOT = 2904.759909
YDOT = 12957.137916 feet/sec YDOT = 3981.906163 meter/sec
ZDOT = -19467.364578 ZDOT = -5919.503408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21266663.90 X = -6482079.16
Y = -4705397.19 feet Y = -1434205.06 meter
Z = -3501691.48 Z = -1067315.56
XDOT = 6132.627116 XDOT = 1869.224745
YDOT = -13278.915701 feet/sec YDOT = -4047.413506 meter/sec
ZDOT = -19411.528208 ZDOT = -5916.633798
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 09203.52968505 .00010596 00000-0 82463-4 0 9093
2 25544 51.6401 125.3775 0007321 258.3795 101.6547 15.74500187 11522
Satellite: ISS
Catalog Number: 25544
Epoch time: 09203.52968505 = yrday.fracday
Element set: 909
Inclination: 51.6401 deg
RA of node: 125.3775 deg
Eccentricity: .0007321
Arg of perigee: 258.3795 deg
Mean anomaly: 101.6547 deg
Mean motion: 15.74500187 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 1152
Checksum: 305
Coasting Arc #11 (Orbit 1167)
---------------------------------------
Vector Time (GMT): 2009/204/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2703618.76 A = 6719196.76 meter
Y = -3393680.61 meter E = .0004024
Z = 5133861.84 I = 51.91117
XDOT = 4675.606173 Wp = 295.94430
YDOT = -5939.234799 meter/sec RA = 119.48617 deg
ZDOT = -1462.931567 TA = 168.03105
MA = 168.02148
Ha = 187.098 n.mi
Hp = 185.801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8870140.30 X = -2690407.87
Y = -11134122.74 feet Y = -3423840.73 meter
Z = 16843378.74 Z = 5120759.71
XDOT = 15339.915266 XDOT = 4748.778694
YDOT = -19485.678474 feet/sec YDOT = -5886.540149 meter/sec
ZDOT = -4799.644249 ZDOT = -1440.040918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5020056.25 X = -1530113.15
Y = 13386032.79 feet Y = 4080062.80 meter
Z = 16791683.85 Z = 5118105.24
XDOT = -23618.383366 XDOT = -7198.883250
YDOT = -2945.649881 feet/sec YDOT = -897.834084 meter/sec
ZDOT = -4709.982548 ZDOT = -1435.602681
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 09204.54517920 .00010596 00000-0 82463-4 0 9109
2 25544 51.6398 120.1588 0007388 263.1506 96.8817 15.74555244 11685
Satellite: ISS
Catalog Number: 25544
Epoch time: 09204.54517920 = yrday.fracday
Element set: 910
Inclination: 51.6398 deg
RA of node: 120.1588 deg
Eccentricity: .0007388
Arg of perigee: 263.1506 deg
Mean anomaly: 96.8817 deg
Mean motion: 15.74555244 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 1168
Checksum: 324
Coasting Arc #12 (Orbit 1183)
---------------------------------------
Vector Time (GMT): 2009/205/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3714805.03 A = 6729727.88 meter
Y = 5409654.28 meter E = .0008112
Z = 1468673.97 I = 51.96026
XDOT = -3269.470592 Wp = 38.11637
YDOT = -3830.159711 meter/sec RA = 114.39259 deg
ZDOT = 5827.471940 TA = 337.98307
MA = 338.01789
Ha = 186.696 n.mi
Hp = 185.654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12187680.55 X = -3782155.02
Y = 17748209.58 feet Y = 5367736.46 meter
Z = 4818484.17 Z = 1450464.67
XDOT = -10726.609555 XDOT = -3254.706301
YDOT = -12566.140784 feet/sec YDOT = -3866.638753 meter/sec
ZDOT = 19119.002428 ZDOT = 5811.624749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21517025.99 X = 6558389.52
Y = 1112675.00 feet Y = 339143.34 meter
Z = 4747192.53 Z = 1446944.28
XDOT = -4948.789335 XDOT = -1508.390989
YDOT = 14244.062163 feet/sec YDOT = 4341.590147 meter/sec
ZDOT = 19056.488044 ZDOT = 5808.417556
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 09205.56066227 .00010596 00000-0 82463-4 0 9112
2 25544 51.6400 114.9390 0007321 267.2590 92.7735 15.74541213 11849
Satellite: ISS
Catalog Number: 25544
Epoch time: 09205.56066227 = yrday.fracday
Element set: 911
Inclination: 51.6400 deg
RA of node: 114.9390 deg
Eccentricity: .0007321
Arg of perigee: 267.2590 deg
Mean anomaly: 92.7735 deg
Mean motion: 15.74541213 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 1184
Checksum: 291
Coasting Arc #13 (Orbit 1198)
---------------------------------------
Vector Time (GMT): 2009/206/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3017429.86 A = 6719627.66 meter
Y = 3294423.02 meter E = .0006250
Z = -5024996.82 I = 51.93822
XDOT = -3817.539532 Wp = 119.94889
YDOT = 6406.157778 meter/sec RA = 109.24533 deg
ZDOT = 1906.254585 TA = 168.39175
MA = 168.37733
Ha = 186.562 n.mi
Hp = 185.671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9899704.26 X = 3004776.92
Y = 10808474.48 feet Y = 3328095.27 meter
Z = -16486210.03 Z = -5010368.90
XDOT = -12524.735996 XDOT = -3898.150642
YDOT = 21017.578011 feet/sec YDOT = 6363.016971 meter/sec
ZDOT = 6254.116093 ZDOT = 1887.513891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3729170.95 X = 1136651.30
Y = -14241470.02 feet Y = -4340800.06 meter
Z = -16428517.94 Z = -5007412.27
XDOT = 23435.810379 XDOT = 7143.235003
YDOT = -998.147564 feet/sec YDOT = -304.235378 meter/sec
ZDOT = 6180.784557 ZDOT = 1883.903133
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 09206.51266391 .00010596 00000-0 82463-4 0 9123
2 25544 51.6404 110.0458 0007384 270.8654 89.1664 15.74577012 11998
Satellite: ISS
Catalog Number: 25544
Epoch time: 09206.51266391 = yrday.fracday
Element set: 912
Inclination: 51.6404 deg
RA of node: 110.0458 deg
Eccentricity: .0007384
Arg of perigee: 270.8654 deg
Mean anomaly: 89.1664 deg
Mean motion: 15.74577012 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 1199
Checksum: 311
Coasting Arc #14 (Orbit 1214)
---------------------------------------
Vector Time (GMT): 2009/207/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2954936.65 A = 6729073.18 meter
Y = -5745490.17 meter E = .0005957
Z = -1866795.59 I = 51.97870
XDOT = 3640.190786 Wp = 210.14817
YDOT = 3717.726079 meter/sec RA = 104.16013 deg
ZDOT = -5677.390591 TA = 350.48377
MA = 350.49505
Ha = 186.670 n.mi
Hp = 185.727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9694674.05 X = 3028032.54
Y = -18850033.37 feet Y = -5712037.52 meter
Z = -6124657.43 Z = -1852263.48
XDOT = 11942.883156 XDOT = 3625.927408
YDOT = 12197.264040 feet/sec YDOT = 3758.353429 meter/sec
ZDOT = -18626.609549 ZDOT = -5659.741161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21087311.19 X = -6427412.45
Y = 2308385.27 feet Y = 703595.83 meter
Z = -6067829.59 Z = -1849474.46
XDOT = 3673.345722 XDOT = 1119.635776
YDOT = -15246.457602 feet/sec YDOT = -4647.120277 meter/sec
ZDOT = -18557.015948 ZDOT = -5656.178461
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 09207.52812058 .00010596 00000-0 82463-4 0 9133
2 25544 51.6405 104.8262 0007497 273.9771 86.0535 15.74567188 12157
Satellite: ISS
Catalog Number: 25544
Epoch time: 09207.52812058 = yrday.fracday
Element set: 913
Inclination: 51.6405 deg
RA of node: 104.8262 deg
Eccentricity: .0007497
Arg of perigee: 273.9771 deg
Mean anomaly: 86.0535 deg
Mean motion: 15.74567188 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 1215
Checksum: 320
Coasting Arc #15 (Orbit 1230)
---------------------------------------
Vector Time (GMT): 2009/208/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3354633.04 A = 6720075.80 meter
Y = -3192728.71 meter E = .0005065
Z = 4872681.86 I = 51.95508
XDOT = 2940.078098 Wp = 340.86412
YDOT = -6709.801566 meter/sec RA = 99.00712 deg
ZDOT = -2368.357586 TA = 132.15006
MA = 132.10702
Ha = 187.077 n.mi
Hp = 185.782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11006013.93 X = -3342352.51
Y = -10474831.72 feet Y = -3230173.86 meter
Z = 15986489.04 Z = 4856414.78
XDOT = 9645.925519 XDOT = 3026.394696
YDOT = -22013.784666 feet/sec YDOT = -6676.441103 meter/sec
ZDOT = -7770.202055 ZDOT = -2353.865604
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2336731.11 X = -712235.64
Y = 15081126.57 feet Y = 4596727.38 meter
Z = 15922361.10 Z = 4853135.66
XDOT = -22528.806463 XDOT = -6866.780210
YDOT = 4667.011202 feet/sec YDOT = 1422.505014 meter/sec
ZDOT = -7713.573338 ZDOT = -2351.097154
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 09208.54356252 .00010596 00000-0 82463-4 0 9146
2 25544 51.6403 99.6064 0007571 279.4223 80.6085 15.74650800 12314
Satellite: ISS
Catalog Number: 25544
Epoch time: 09208.54356252 = yrday.fracday
Element set: 914
Inclination: 51.6403 deg
RA of node: 99.6064 deg
Eccentricity: .0007571
Arg of perigee: 279.4223 deg
Mean anomaly: 80.6085 deg
Mean motion: 15.74650800 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 1231
Checksum: 300
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