ISS TRAJECTORY DATA
Lift off time (UTC) : N/A
Area (sq ft) : 10763.91
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 3779)
---------------------------------------
Vector Time (GMT): 2012/039/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 886586.8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1970552.12 A = 6764806.62 meter
Y = 3968533.42 meter E = .0019840
Z = 5097982.73 I = 51.89810
XDOT = -5604.142355 Wp = 34.41123
YDOT = -4974.311681 meter/sec RA = 51.95470 deg
ZDOT = 1718.801399 TA = 39.15472
MA = 39.01133
Ha = 220.408 n.mi
Hp = 202.122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6465066.01 X = -2039546.78
Y = 13020122.77 feet Y = 3946111.97 meter
Z = 16725665.14 Z = 5088242.37
XDOT = -18386.293817 XDOT = -5556.451416
YDOT = -16319.920212 feet/sec YDOT = -5036.713917 meter/sec
ZDOT = 5639.112202 ZDOT = 1691.693551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13663984.12 X = -4164782.36
Y = 5095251.41 feet Y = 1553032.63 meter
Z = 16685397.83 Z = 5085709.26
XDOT = -2060.723150 XDOT = -628.108416
YDOT = -23492.717300 feet/sec YDOT = -7160.580233 meter/sec
ZDOT = 5528.352054 ZDOT = 1685.041706
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 12039.55102448 .00016717 00000-0 10270-3 0 9001
2 25544 51.6396 52.3132 0020532 20.4509 339.7464 15.58761355 37800
Satellite: ISS
Catalog Number: 25544
Epoch time: 12039.55102448 = yrday.fracday
Element set: 900
Inclination: 51.6396 deg
RA of node: 52.3132 deg
Eccentricity: .0020532
Arg of perigee: 20.4509 deg
Mean anomaly: 339.7464 deg
Mean motion: 15.58761355 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3780
Checksum: 295
Coasting Arc #2 (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 = 4362662.91 A = 6765123.99 meter
Y = -1142760.42 meter E = .0025981
Z = -5055894.12 I = 51.88003
XDOT = 3860.756741 Wp = 52.81440
YDOT = 6336.506257 meter/sec RA = 46.92413 deg
ZDOT = 1921.245220 TA = 235.64172
MA = 235.88777
Ha = 220.455 n.mi
Hp = 202.023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14313198.52 X = 4399677.05
Y = -3749213.98 feet Y = -1093767.81 meter
Z = -16587579.13 Z = -5034611.03
XDOT = 12666.524740 XDOT = 3780.280964
YDOT = 20789.062523 feet/sec YDOT = 6379.229780 meter/sec
ZDOT = 6303.297966 ZDOT = 1939.804266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13244270.39 X = 4036853.62
Y = 6812080.80 feet Y = 2076322.23 meter
Z = -16500208.96 Z = -5029263.69
XDOT = -3947.238964 XDOT = -1203.118436
YDOT = 22949.027293 feet/sec YDOT = 6994.863519 meter/sec
ZDOT = 6378.885428 ZDOT = 1944.284278
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 12040.51267859 .00016717 00000-0 10270-3 0 9018
2 25544 51.6401 47.4861 0020542 23.6269 336.5825 15.58764183 37954
Satellite: ISS
Catalog Number: 25544
Epoch time: 12040.51267859 = yrday.fracday
Element set: 901
Inclination: 51.6401 deg
RA of node: 47.4861 deg
Eccentricity: .0020542
Arg of perigee: 23.6269 deg
Mean anomaly: 336.5825 deg
Mean motion: 15.58764183 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3795
Checksum: 316
Coasting Arc #3 (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 = -5723618.08 A = 6771667.93 meter
Y = -1868261.32 meter E = .0028199
Z = 3100531.90 I = 51.88030
XDOT = -768.160018 Wp = 52.47508
YDOT = -5854.054791 meter/sec RA = 41.91040 deg
ZDOT = -4898.232051 TA = 91.93756
MA = 91.61458
Ha = 220.465 n.mi
Hp = 201.651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18778274.54 X = -5717362.81
Y = -6129466.27 feet Y = -1932231.14 meter
Z = 10172348.74 Z = 3072742.69
XDOT = -2520.210034 XDOT = -678.847663
YDOT = -19206.216507 feet/sec YDOT = -5862.145818 meter/sec
ZDOT = -16070.315127 ZDOT = -4901.746301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10251763.66 X = -3124737.56
Y = -16952803.00 feet Y = -5167214.36 meter
Z = 10058550.72 Z = 3065846.26
XDOT = 9484.940295 XDOT = 2891.009802
YDOT = -15371.956046 feet/sec YDOT = -4685.372203 meter/sec
ZDOT = -16084.242999 ZDOT = -4902.477266
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 12041.53842645 .00016717 00000-0 10270-3 0 9024
2 25544 51.6394 42.3347 0020657 27.3663 332.8575 15.58841052 38115
Satellite: ISS
Catalog Number: 25544
Epoch time: 12041.53842645 = yrday.fracday
Element set: 902
Inclination: 51.6394 deg
RA of node: 42.3347 deg
Eccentricity: .0020657
Arg of perigee: 27.3663 deg
Mean anomaly: 332.8575 deg
Mean motion: 15.58841052 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3811
Checksum: 303
Coasting Arc #4 (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 = 5429188.47 A = 6775567.59 meter
Y = 4023840.63 meter E = .0032343
Z = -57971.89 I = 51.87073
XDOT = -2797.544073 Wp = 36.25487
YDOT = 3836.743197 meter/sec RA = 36.92978 deg
ZDOT = 6048.792371 TA = 323.12030
MA = 323.34229
Ha = 220.406 n.mi
Hp = 201.340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17812298.13 X = 5384071.18
Y = 13201576.88 feet Y = 4084300.90 meter
Z = -190196.50 Z = -31707.40
XDOT = -9178.294204 XDOT = -2869.622623
YDOT = 12587.740149 feet/sec YDOT = 3805.056744 meter/sec
ZDOT = 19845.119328 ZDOT = 6035.026888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5223296.27 X = 1592060.70
Y = 21547762.89 feet Y = 6567758.13 meter
Z = -82836.86 Z = -25248.68
XDOT = -13632.908438 XDOT = -4155.310492
YDOT = 3330.506275 feet/sec YDOT = 1015.138312 meter/sec
ZDOT = 19788.355536 ZDOT = 6031.490767
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 12042.50005134 .00016717 00000-0 10270-3 0 9037
2 25544 51.6396 37.5077 0020459 31.4816 328.7559 15.58879152 38263
Satellite: ISS
Catalog Number: 25544
Epoch time: 12042.50005134 = yrday.fracday
Element set: 903
Inclination: 51.6396 deg
RA of node: 37.5077 deg
Eccentricity: .0020459
Arg of perigee: 31.4816 deg
Mean anomaly: 328.7559 deg
Mean motion: 15.58879152 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3826
Checksum: 314
Coasting Arc #5 (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 = -3422817.71 A = 6771529.74 meter
Y = -4986261.43 meter E = .0022568
Z = -3078804.71 I = 51.83191
XDOT = 5791.122116 Wp = 45.43282
YDOT = -943.499980 meter/sec RA = 31.94592 deg
ZDOT = -4916.910781 TA = 169.80908
MA = 169.76325
Ha = 220.574 n.mi
Hp = 201.122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11229716.89 X = -3351849.97
Y = -16359125.42 feet Y = -5024140.85 meter
Z = -10101065.32 Z = -3095259.76
XDOT = 18999.744474 XDOT = 5825.127083
YDOT = -3095.472374 feet/sec YDOT = -878.550223 meter/sec
ZDOT = -16131.597052 ZDOT = -4888.695447
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1562988.62 X = 476398.93
Y = -19746533.32 feet Y = -6018743.35 meter
Z = -10168113.65 Z = -3099241.04
XDOT = 15375.870049 XDOT = 4686.565191
YDOT = 9452.762119 feet/sec YDOT = 2881.201894 meter/sec
ZDOT = -16015.827770 ZDOT = -4881.624304
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 12043.52576775 .00016717 00000-0 10270-3 0 9045
2 25544 51.6393 32.3563 0020666 35.0305 325.2205 15.58858170 38421
Satellite: ISS
Catalog Number: 25544
Epoch time: 12043.52576775 = yrday.fracday
Element set: 904
Inclination: 51.6393 deg
RA of node: 32.3563 deg
Eccentricity: .0020666
Arg of perigee: 35.0305 deg
Mean anomaly: 325.2205 deg
Mean motion: 15.58858170 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3842
Checksum: 300
Coasting Arc #6 (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 = 178048.69 A = 6764734.98 meter
Y = 4517770.35 meter E = .0021755
Z = 5013028.93 I = 51.78294
XDOT = -7185.660019 Wp = 52.95802
YDOT = -1903.473446 meter/sec RA = 26.92857 deg
ZDOT = 1977.577270 TA = 17.97981
MA = 17.90298
Ha = 220.607 n.mi
Hp = 200.957
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 584149.24 X = 103164.93
Y = 14822081.21 feet Y = 4519342.88 meter
Z = 16446945.30 Z = 5013711.82
XDOT = -23575.000063 XDOT = -7173.447469
YDOT = -6244.991620 feet/sec YDOT = -1983.759572 meter/sec
ZDOT = 6488.114404 ZDOT = 1942.699746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8715020.58 X = -2656338.27
Y = 12000182.13 feet Y = 3657655.51 meter
Z = 16449357.93 Z = 5013764.30
XDOT = -13935.859398 XDOT = -4247.649944
YDOT = -18787.418121 feet/sec YDOT = -5726.405043 meter/sec
ZDOT = 6345.275578 ZDOT = 1934.039996
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 12044.55146617 .00016717 00000-0 10270-3 0 9058
2 25544 51.6392 27.2063 0020605 38.3361 321.9255 15.58888850 38582
Satellite: ISS
Catalog Number: 25544
Epoch time: 12044.55146617 = yrday.fracday
Element set: 905
Inclination: 51.6392 deg
RA of node: 27.2063 deg
Eccentricity: .0020605
Arg of perigee: 38.3361 deg
Mean anomaly: 321.9255 deg
Mean motion: 15.58888850 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3858
Checksum: 314
Coasting Arc #7 (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 = 3275046.01 A = 6764533.16 meter
Y = -3023382.07 meter E = .0029512
Z = -5108259.15 I = 51.75464
XDOT = 6313.021114 Wp = 64.88348
YDOT = 3986.869624 meter/sec RA = 21.88803 deg
ZDOT = 1707.698486 TA = 221.49661
MA = 221.72106
Ha = 220.683 n.mi
Hp = 200.846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10744901.60 X = 3333425.15
Y = -9919232.52 feet Y = -2986432.14 meter
Z = -16759380.40 Z = -5092207.46
XDOT = 20712.011530 XDOT = 6259.674421
YDOT = 13080.280919 feet/sec YDOT = 4057.167462 meter/sec
ZDOT = 5602.685322 ZDOT = 1738.236878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14629348.46 X = 4459025.41
Y = -1427114.60 feet Y = -434984.53 meter
Z = -16693304.74 Z = -5088119.29
XDOT = 8587.842176 XDOT = 2617.574295
YDOT = 21804.965758 feet/sec YDOT = 6646.153563 meter/sec
ZDOT = 5727.548190 ZDOT = 1745.756688
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 12045.51304313 .00016717 00000-0 10270-3 0 9065
2 25544 51.6395 22.3782 0020656 42.0133 318.2602 15.58887834 38737
Satellite: ISS
Catalog Number: 25544
Epoch time: 12045.51304313 = yrday.fracday
Element set: 906
Inclination: 51.6395 deg
RA of node: 22.3782 deg
Eccentricity: .0020656
Arg of perigee: 42.0133 deg
Mean anomaly: 318.2602 deg
Mean motion: 15.58887834 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3873
Checksum: 296
Coasting Arc #8 (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 = -5893750.32 A = 6771059.34 meter
Y = 859860.34 meter E = .0030759
Z = 3212411.81 I = 51.74829
XDOT = -3362.876349 Wp = 63.26277
YDOT = -4966.661762 meter/sec RA = 16.86348 deg
ZDOT = -4791.497193 TA = 79.54536
MA = 79.19889
Ha = 220.694 n.mi
Hp = 200.589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19336451.17 X = -5918532.35
Y = 2821064.09 feet Y = 793814.22 meter
Z = 10539408.82 Z = 3183720.46
XDOT = -11033.058887 XDOT = -3283.812535
YDOT = -16294.822055 feet/sec YDOT = -5003.825440 meter/sec
ZDOT = -15720.135149 ZDOT = -4807.641621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17371160.57 X = -5294729.74
Y = -9086632.84 feet Y = -2769605.69 meter
Z = 10421697.02 Z = 3176533.25
XDOT = 29.151305 XDOT = 8.885318
YDOT = -18347.028776 feet/sec YDOT = -5592.174371 meter/sec
ZDOT = -15785.892257 ZDOT = -4811.539960
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 12046.53870727 .00016717 00000-0 10270-3 0 9076
2 25544 51.6394 17.2270 0020667 45.5215 314.7625 15.58948351 38897
Satellite: ISS
Catalog Number: 25544
Epoch time: 12046.53870727 = yrday.fracday
Element set: 907
Inclination: 51.6394 deg
RA of node: 17.2270 deg
Eccentricity: .0020667
Arg of perigee: 45.5215 deg
Mean anomaly: 314.7625 deg
Mean motion: 15.58948351 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3889
Checksum: 327
Coasting Arc #9 (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 = 6640362.98 A = 6775272.74 meter
Y = 1259069.50 meter E = .0032498
Z = -169801.23 I = 51.73344
XDOT = -756.707189 Wp = 47.23704
YDOT = 4703.309174 meter/sec RA = 11.87185 deg
ZDOT = 6032.388615 TA = 310.92983
MA = 311.21074
Ha = 220.658 n.mi
Hp = 200.311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21785967.79 X = 6626615.13
Y = 4130805.46 feet Y = 1333249.27 meter
Z = -557090.66 Z = -137576.66
XDOT = -2482.635135 XDOT = -838.547711
YDOT = 15430.804376 feet/sec YDOT = 4694.389578 meter/sec
ZDOT = 19791.301229 ZDOT = 6028.513878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15505934.28 X = 4726208.77
Y = 15855207.57 feet Y = 4832667.27 meter
Z = -425077.98 Z = -129563.77
XDOT = -9808.386907 XDOT = -2989.596329
YDOT = 10036.047253 feet/sec YDOT = 3058.987203 meter/sec
ZDOT = 19774.999302 ZDOT = 6027.419787
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 12047.50025165 .00016717 00000-0 10270-3 0 9083
2 25544 51.6395 12.3991 0020633 49.5618 310.7333 15.58977311 39046
Satellite: ISS
Catalog Number: 25544
Epoch time: 12047.50025165 = yrday.fracday
Element set: 908
Inclination: 51.6395 deg
RA of node: 12.3991 deg
Eccentricity: .0020633
Arg of perigee: 49.5618 deg
Mean anomaly: 310.7333 deg
Mean motion: 15.58977311 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3904
Checksum: 303
Coasting Arc #10 (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 = -5254944.66 A = 6771210.93 meter
Y = -3043180.60 meter E = .0023576
Z = -3027726.77 I = 51.69123
XDOT = 4783.714007 Wp = 61.36588
YDOT = -3358.208670 meter/sec RA = 6.87865 deg
ZDOT = -4945.520967 TA = 153.29015
MA = 153.16852
Ha = 220.660 n.mi
Hp = 200.091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17240632.07 X = -5205816.98
Y = -9984188.32 feet Y = -3101669.95 meter
Z = -9933486.79 Z = -3053135.11
XDOT = 15694.599761 XDOT = 4844.934282
YDOT = -11017.744979 feet/sec YDOT = -3304.371940 meter/sec
ZDOT = -16225.462489 ZDOT = -4922.133753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8685173.04 X = -2647240.74
Y = -17872213.87 feet Y = -5447450.79 meter
Z = -10037395.64 Z = -3059398.19
XDOT = 17950.659003 XDOT = 5471.360864
YDOT = 302.005276 feet/sec YDOT = 92.051208 meter/sec
ZDOT = -16129.275593 ZDOT = -4916.203201
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 12048.52588093 .00016717 00000-0 10270-3 0 9091
2 25544 51.6404 7.2475 0020684 52.9070 307.3972 15.59003009 39207
Satellite: ISS
Catalog Number: 25544
Epoch time: 12048.52588093 = yrday.fracday
Element set: 909
Inclination: 51.6404 deg
RA of node: 7.2475 deg
Eccentricity: .0020684
Arg of perigee: 52.9070 deg
Mean anomaly: 307.3972 deg
Mean motion: 15.59003009 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3920
Checksum: 302
Coasting Arc #11 (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 = 2101763.13 A = 6764272.28 meter
Y = 4022875.71 meter E = .0023257
Z = 4994189.98 I = 51.63856
XDOT = -7308.878183 Wp = 69.26352
YDOT = 1343.223293 meter/sec RA = 1.85130 deg
ZDOT = 1994.503236 TA = 1.43526
MA = 1.42860
Ha = 220.516 n.mi
Hp = 200.021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6895548.34 X = 2032362.35
Y = 13198411.12 feet Y = 4045990.97 meter
Z = 16385137.73 Z = 5004231.32
XDOT = -23979.259131 XDOT = -7333.043745
YDOT = 4406.900567 feet/sec YDOT = 1261.355832 meter/sec
ZDOT = 6543.645787 ZDOT = 1958.939297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1471781.97 X = -448599.15
Y = 14772989.87 feet Y = 4502807.31 meter
Z = 16425955.36 Z = 5006631.19
XDOT = -21477.861841 XDOT = -6546.452289
YDOT = -9251.124357 feet/sec YDOT = -2819.742704 meter/sec
ZDOT = 6397.711220 ZDOT = 1950.022380
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 12049.55149068 .00016717 00000-0 10270-3 0 9102
2 25544 51.6408 2.0975 0020450 56.6411 303.6698 15.59056756 39368
Satellite: ISS
Catalog Number: 25544
Epoch time: 12049.55149068 = yrday.fracday
Element set: 910
Inclination: 51.6408 deg
RA of node: 2.0975 deg
Eccentricity: .0020450
Arg of perigee: 56.6411 deg
Mean anomaly: 303.6698 deg
Mean motion: 15.59056756 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3936
Checksum: 314
Coasting Arc #12 (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 = 1726414.48 A = 6764151.88 meter
Y = -4136425.15 meter E = .0031558
Z = -5090429.64 I = 51.60744
XDOT = 7392.760939 Wp = 76.37388
YDOT = 966.159851 meter/sec RA = 356.79838 deg
ZDOT = 1738.480155 TA = 210.37640
MA = 210.55964
Ha = 220.660 n.mi
Hp = 199.931
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5664089.50 X = 1797267.94
Y = -13570948.65 feet Y = -4116723.36 meter
Z = -16700884.66 Z = -5081870.79
XDOT = 24254.465022 XDOT = 7372.962805
YDOT = 3169.815784 feet/sec YDOT = 1048.719634 meter/sec
ZDOT = 5703.675048 ZDOT = 1774.344670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12073404.01 X = 3679973.54
Y = -8465717.29 feet Y = -2580350.63 meter
Z = -16665432.85 Z = -5079623.93
XDOT = 18256.466198 XDOT = 5564.570897
YDOT = 14624.707845 feet/sec YDOT = 4457.610951 meter/sec
ZDOT = 5850.638065 ZDOT = 1783.274482
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 12050.51298555 .00016717 00000-0 10270-3 0 9117
2 25544 51.6411 357.2682 0020561 60.0938 300.2257 15.59036949 39511
Satellite: ISS
Catalog Number: 25544
Epoch time: 12050.51298555 = yrday.fracday
Element set: 911
Inclination: 51.6411 deg
RA of node: 357.2682 deg
Eccentricity: .0020561
Arg of perigee: 60.0938 deg
Mean anomaly: 300.2257 deg
Mean motion: 15.59036949 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3951
Checksum: 302
Coasting Arc #13 (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 = -5032926.28 A = 6770836.73 meter
Y = 3244950.64 meter E = .0032403
Z = 3142245.56 I = 51.60055
XDOT = -5075.194312 Wp = 75.30803
YDOT = -3139.258615 meter/sec RA = 351.76349 deg
ZDOT = -4837.333339 TA = 68.32980
MA = 67.98504
Ha = 220.685 n.mi
Hp = 199.762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16512225.32 X = -5084101.79
Y = 10646163.52 feet Y = 3188383.41 meter
Z = 10309204.61 Z = 3117672.05
XDOT = -16650.899974 XDOT = -5016.215304
YDOT = -10299.404905 feet/sec YDOT = -3195.683096 meter/sec
ZDOT = -15870.516204 ZDOT = -4861.844235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19690191.49 X = -6001570.36
Y = 602994.15 feet Y = 183792.62 meter
Z = 10208175.15 Z = 3111451.79
XDOT = -8852.608425 XDOT = -2698.275048
YDOT = -15913.227499 feet/sec YDOT = -4850.351742 meter/sec
ZDOT = -15970.739621 ZDOT = -4867.881437
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 12051.53856064 .00016717 00000-0 10270-3 0 9126
2 25544 51.6417 352.1170 0020579 63.8843 296.4427 15.59084218 39672
Satellite: ISS
Catalog Number: 25544
Epoch time: 12051.53856064 = yrday.fracday
Element set: 912
Inclination: 51.6417 deg
RA of node: 352.1170 deg
Eccentricity: .0020579
Arg of perigee: 63.8843 deg
Mean anomaly: 296.4427 deg
Mean motion: 15.59084218 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3967
Checksum: 322
Coasting Arc #14 (Orbit 3981)
---------------------------------------
Vector Time (GMT): 2012/052/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 886586.8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6574845.76 A = 6774937.35 meter
Y = -1586855.45 meter E = .0032110
Z = -49205.89 I = 51.58446
XDOT = 1142.021639 Wp = 58.86263
YDOT = 4635.453469 meter/sec RA = 346.76158 deg
ZDOT = 6019.677937 TA = 300.60539
MA = 300.92169
Ha = 220.635 n.mi
Hp = 199.616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21571016.29 X = 6592340.67
Y = -5206218.67 feet Y = -1513233.65 meter
Z = -161436.65 Z = -17223.84
XDOT = 3746.790154 XDOT = 1060.860747
YDOT = 15208.180674 feet/sec YDOT = 4647.770957 meter/sec
ZDOT = 19749.599530 ZDOT = 6025.028162
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21287377.74 X = 6488392.74
Y = 6267866.95 feet Y = 1910445.85 meter
Z = -30182.46 Z = -9199.61
XDOT = -4000.176351 XDOT = -1219.253752
YDOT = 13434.658897 feet/sec YDOT = 4094.884032 meter/sec
ZDOT = 19771.140105 ZDOT = 6026.243504
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 12052.50002059 .00016717 00000-0 10270-3 0 9132
2 25544 51.6417 347.2887 0020530 67.4280 292.9045 15.59094551 39829
Satellite: ISS
Catalog Number: 25544
Epoch time: 12052.50002059 = yrday.fracday
Element set: 913
Inclination: 51.6417 deg
RA of node: 347.2887 deg
Eccentricity: .0020530
Arg of perigee: 67.4280 deg
Mean anomaly: 292.9045 deg
Mean motion: 15.59094551 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3982
Checksum: 305
Coasting Arc #15 (Orbit 3997)
---------------------------------------
Vector Time (GMT): 2012/053/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 886586.8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5961568.60 A = 6770434.77 meter
Y = -680806.30 meter E = .0024647
Z = -3163804.45 I = 51.54161
XDOT = 3123.938734 Wp = 75.90925
YDOT = -5062.859855 meter/sec RA = 341.75688 deg
ZDOT = -4822.703726 TA = 140.64787
MA = 140.46852
Ha = 220.575 n.mi
Hp = 199.393
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19558952.11 X = -5938143.93
Y = -2233616.46 feet Y = -747341.57 meter
Z = -10379935.86 Z = -3192707.82
XDOT = 10249.142827 XDOT = 3203.747518
YDOT = -16610.432595 feet/sec YDOT = -5027.480282 meter/sec
ZDOT = -15822.518785 ZDOT = -4807.333794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15970123.64 X = -4867693.69
Y = -11402811.32 feet Y = -3475576.89 meter
Z = -10498369.56 Z = -3199903.04
XDOT = 16268.040717 XDOT = 4958.498811
YDOT = -8351.757414 feet/sec YDOT = -2545.615660 meter/sec
ZDOT = -15759.083239 ZDOT = -4803.368571
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 12053.52555968 .00016717 00000-0 10270-3 0 9148
2 25544 51.6426 342.1371 0020559 71.2598 289.0786 15.59141219 39987
Satellite: ISS
Catalog Number: 25544
Epoch time: 12053.52555968 = yrday.fracday
Element set: 914
Inclination: 51.6426 deg
RA of node: 342.1371 deg
Eccentricity: .0020559
Arg of perigee: 71.2598 deg
Mean anomaly: 289.0786 deg
Mean motion: 15.59141219 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3998
Checksum: 339
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