ISS TRAJECTORY DATA
Lift off time (UTC) : N/A
Area (sq ft) : 7534.74
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 164)
---------------------------------------
Vector Time (GMT): 2008/252/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 609794.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4229537.26 A = 6726536.85 meter
Y = 1203800.29 meter E = .0010599
Z = 5081868.92 I = 51.36687
XDOT = -3692.988057 Wp = 105.78786
YDOT = 6592.315680 meter/sec RA = 308.42660 deg
ZDOT = 1506.556678 TA = 329.68577
MA = 329.74703
Ha = 195.387 n.mi
Hp = 184.530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13876434.60 X = 4191075.04
Y = 3949476.03 feet Y = 1250882.28 meter
Z = 16672798.30 Z = 5102322.60
XDOT = -12116.102549 XDOT = -3773.748495
YDOT = 21628.332285 feet/sec YDOT = 6550.566981 meter/sec
ZDOT = 4942.771254 ZDOT = 1488.420092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12559382.26 X = -3828099.71
Y = -6911565.40 feet Y = -2106645.14 meter
Z = 16751960.54 Z = 5105997.57
XDOT = 16140.509154 XDOT = 4919.627190
YDOT = -17475.116286 feet/sec YDOT = -5326.415444 meter/sec
ZDOT = 4873.251610 ZDOT = 1485.367091
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 08252.55022161 .00020000 00000-0 20000-3 0 9008
2 25544 51.6420 308.7468 0006392 92.0765 268.1130 15.71998112 1652
Satellite: ISS
Catalog Number: 25544
Epoch time: 08252.55022161 = yrday.fracday
Element set: 900
Inclination: 51.6420 deg
RA of node: 308.7468 deg
Eccentricity: .0006392
Arg of perigee: 92.0765 deg
Mean anomaly: 268.1130 deg
Mean motion: 15.71998112 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 165
Checksum: 272
Coasting Arc #2 (Orbit 179)
---------------------------------------
Vector Time (GMT): 2008/253/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 609794.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2138575.23 A = 6736292.99 meter
Y = -6085819.64 meter E = .0011937
Z = -1939344.74 I = 51.38188
XDOT = 5284.072388 Wp = 65.33370
YDOT = 85.560158 meter/sec RA = 303.25741 deg
ZDOT = 5590.262337 TA = 273.04347
MA = 273.18006
Ha = 195.558 n.mi
Hp = 184.522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7016322.93 X = 2215889.85
Y = -19966599.86 feet Y = -6061472.54 meter
Z = -6362679.58 Z = -1928767.86
XDOT = 17336.195498 XDOT = 5255.566526
YDOT = 280.709179 feet/sec YDOT = 144.490245 meter/sec
ZDOT = 18340.755700 ZDOT = 5615.863032
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11001438.64 X = -3353238.50
Y = 18093478.65 feet Y = 5514892.29 meter
Z = -6322338.73 Z = -1927048.84
XDOT = -15486.849221 XDOT = -4720.391643
YDOT = -3009.940696 feet/sec YDOT = -917.429924 meter/sec
ZDOT = 18439.717092 ZDOT = 5620.425770
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 08253.50378452 .00020000 00000-0 20000-3 0 9012
2 25544 51.6415 303.8646 0006475 94.2900 265.9002 15.71987038 1802
Satellite: ISS
Catalog Number: 25544
Epoch time: 08253.50378452 = yrday.fracday
Element set: 901
Inclination: 51.6415 deg
RA of node: 303.8646 deg
Eccentricity: .0006475
Arg of perigee: 94.2900 deg
Mean anomaly: 265.9002 deg
Mean motion: 15.71987038 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 180
Checksum: 286
Coasting Arc #3 (Orbit 195)
---------------------------------------
Vector Time (GMT): 2008/254/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 609794.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4776130.43 A = 6728481.50 meter
Y = 1070341.50 meter E = .0016914
Z = -4632521.91 I = 51.34125
XDOT = 1180.998121 Wp = 80.72955
YDOT = -7038.096462 meter/sec RA = 298.15615 deg
ZDOT = -2849.939791 TA = 160.94697
MA = 160.88362
Ha = 195.545 n.mi
Hp = 184.342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15669719.27 X = -4765240.38
Y = 3511619.08 feet Y = 1016992.95 meter
Z = -15198562.71 Z = -4655697.76
XDOT = 3874.665752 XDOT = 1273.455880
YDOT = -23090.867659 feet/sec YDOT = -7024.372900 meter/sec
ZDOT = -9350.196164 ZDOT = -2843.977966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15964984.59 X = 4866127.30
Y = -512500.21 feet Y = -156210.06 meter
Z = -15288050.55 Z = -4659797.81
XDOT = -8246.125327 XDOT = -2513.419000
YDOT = 20772.910056 feet/sec YDOT = 6331.582985 meter/sec
ZDOT = -9327.786484 ZDOT = -2843.109320
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 08254.52090736 .00020000 00000-0 20000-3 0 9022
2 25544 51.6420 298.6563 0006579 98.3722 261.8186 15.72001393 1966
Satellite: ISS
Catalog Number: 25544
Epoch time: 08254.52090736 = yrday.fracday
Element set: 902
Inclination: 51.6420 deg
RA of node: 298.6563 deg
Eccentricity: .0006579
Arg of perigee: 98.3722 deg
Mean anomaly: 261.8186 deg
Mean motion: 15.72001393 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 196
Checksum: 300
Coasting Arc #4 (Orbit 211)
---------------------------------------
Vector Time (GMT): 2008/255/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 609794.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 79257.69 A = 6733757.45 meter
Y = 6006957.28 meter E = .0019760
Z = 3021980.46 I = 51.34609
XDOT = -5353.368807 Wp = 97.42570
YDOT = 2556.017251 meter/sec RA = 292.96887 deg
ZDOT = -4915.412873 TA = 47.44366
MA = 47.27703
Ha = 195.452 n.mi
Hp = 184.407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 260031.80 X = -2599.08
Y = 19707865.10 feet Y = 6007385.96 meter
Z = 9914634.06 Z = 3022166.55
XDOT = -17563.545954 XDOT = -5357.674731
YDOT = 8385.883369 feet/sec YDOT = 2496.128631 meter/sec
ZDOT = -16126.682655 ZDOT = -4941.429836
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3179802.99 X = 969203.95
Y = -19450738.24 feet Y = -5928585.02 meter
Z = 9915904.74 Z = 3022367.76
XDOT = 17231.902213 XDOT = 5252.283795
YDOT = -5497.073050 feet/sec YDOT = -1675.507866 meter/sec
ZDOT = -16227.017780 ZDOT = -4945.995019
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 08255.53801787 .00020000 00000-0 20000-3 0 9031
2 25544 51.6413 293.4486 0006567 100.5501 259.6401 15.72054904 2123
Satellite: ISS
Catalog Number: 25544
Epoch time: 08255.53801787 = yrday.fracday
Element set: 903
Inclination: 51.6413 deg
RA of node: 293.4486 deg
Eccentricity: .0006567
Arg of perigee: 100.5501 deg
Mean anomaly: 259.6401 deg
Mean motion: 15.72054904 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 212
Checksum: 276
Coasting Arc #5 (Orbit 227)
---------------------------------------
Vector Time (GMT): 2008/256/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 609794.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4348210.45 A = 6731114.99 meter
Y = -3346016.06 meter E = .0017916
Z = 3886978.51 I = 51.32620
XDOT = 1321.053348 Wp = 101.33698
YDOT = 6427.350979 meter/sec RA = 287.87684 deg
ZDOT = 4035.838775 TA = 306.43269
MA = 306.59773
Ha = 195.472 n.mi
Hp = 184.359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14265782.32 X = 4366420.89
Y = -10977742.97 feet Y = -3297289.88 meter
Z = 12752554.16 Z = 3908146.31
XDOT = 4334.164529 XDOT = 1229.478276
YDOT = 21087.109511 feet/sec YDOT = 6441.611906 meter/sec
ZDOT = 13240.940862 ZDOT = 4042.033695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15718471.88 X = -4790990.23
Y = 8652592.22 feet Y = 2637310.11 meter
Z = 12834068.45 Z = 3911824.06
XDOT = -317.449559 XDOT = -96.758626
YDOT = -20345.673568 feet/sec YDOT = -6201.361304 meter/sec
ZDOT = 13265.488695 ZDOT = 4043.320954
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 08256.55511954 .00020000 00000-0 20000-3 0 9049
2 25544 51.6406 288.2405 0006769 103.9801 256.2114 15.72041195 2281
Satellite: ISS
Catalog Number: 25544
Epoch time: 08256.55511954 = yrday.fracday
Element set: 904
Inclination: 51.6406 deg
RA of node: 288.2405 deg
Eccentricity: .0006769
Arg of perigee: 103.9801 deg
Mean anomaly: 256.2114 deg
Mean motion: 15.72041195 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 228
Checksum: 282
Coasting Arc #6 (Orbit 242)
---------------------------------------
Vector Time (GMT): 2008/257/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 609794.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2125499.56 A = 6730832.80 meter
Y = -5017157.40 meter E = .0013668
Z = -3965837.66 I = 51.31866
XDOT = 4352.572848 Wp = 107.29558
YDOT = -4956.417790 meter/sec RA = 282.68206 deg
ZDOT = 3944.770833 TA = 203.78080
MA = 203.84402
Ha = 195.456 n.mi
Hp = 184.337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6973423.75 X = -2049973.72
Y = -16460490.16 feet Y = -5040503.94 meter
Z = -13011278.43 Z = -3975979.49
XDOT = 14280.094645 XDOT = 4388.509953
YDOT = -16261.213223 feet/sec YDOT = -4907.543613 meter/sec
ZDOT = 12942.161525 ZDOT = 3966.003115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4569640.21 X = 1392826.33
Y = 17252842.02 feet Y = 5258666.25 meter
Z = -13050960.58 Z = -3977932.78
XDOT = -15048.882916 XDOT = -4586.899513
YDOT = 13819.924489 feet/sec YDOT = 4212.312984 meter/sec
ZDOT = 13023.767126 ZDOT = 3969.644220
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 08257.50864089 .00020000 00000-0 20000-3 0 9056
2 25544 51.6415 283.3580 0006677 106.9715 253.2179 15.72067095 2438
Satellite: ISS
Catalog Number: 25544
Epoch time: 08257.50864089 = yrday.fracday
Element set: 905
Inclination: 51.6415 deg
RA of node: 283.3580 deg
Eccentricity: .0006677
Arg of perigee: 106.9715 deg
Mean anomaly: 253.2179 deg
Mean motion: 15.72067095 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 243
Checksum: 306
Coasting Arc #7 (Orbit 258)
---------------------------------------
Vector Time (GMT): 2008/258/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 609794.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3102342.83 A = 6733724.89 meter
Y = 5178749.28 meter E = .0011173
Z = -2987307.26 I = 51.32262
XDOT = -3347.960820 Wp = 110.31540
YDOT = -4847.410481 meter/sec RA = 277.58779 deg
ZDOT = -4945.291860 TA = 104.30325
MA = 104.17916
Ha = 195.378 n.mi
Hp = 184.382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10178290.13 X = -3145510.10
Y = 16990647.24 feet Y = 5143815.47 meter
Z = -9800876.85 Z = -3002483.71
XDOT = -10984.123425 XDOT = -3269.484189
YDOT = -15903.577694 feet/sec YDOT = -4884.410950 meter/sec
ZDOT = -16224.710827 ZDOT = -4961.365176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12094971.01 X = 3686547.16
Y = -15647613.39 feet Y = -4769392.56 meter
Z = -9859043.66 Z = -3005036.51
XDOT = 7754.938533 XDOT = 2363.705265
YDOT = 16217.756212 feet/sec YDOT = 4943.172093 meter/sec
ZDOT = -16287.313201 ZDOT = -4964.373064
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 08258.52571970 .00020000 00000-0 20000-3 0 9064
2 25544 51.6407 278.1491 0006650 111.1017 249.0857 15.72081046 2591
Satellite: ISS
Catalog Number: 25544
Epoch time: 08258.52571970 = yrday.fracday
Element set: 906
Inclination: 51.6407 deg
RA of node: 278.1491 deg
Eccentricity: .0006650
Arg of perigee: 111.1017 deg
Mean anomaly: 249.0857 deg
Mean motion: 15.72081046 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 259
Checksum: 287
Coasting Arc #8 (Orbit 274)
---------------------------------------
Vector Time (GMT): 2008/259/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 609794.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3578399.19 A = 6728107.14 meter
Y = 3298234.42 meter E = .0013262
Z = 4634892.17 I = 51.30019
XDOT = -2535.088769 Wp = 85.99874
YDOT = 6711.819050 meter/sec RA = 272.39723 deg
ZDOT = -2811.140011 TA = 31.91030
MA = 31.83004
Ha = 195.225 n.mi
Hp = 184.405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11740154.83 X = 3518736.31
Y = 10820979.07 feet Y = 3337917.00 meter
Z = 15206339.14 Z = 4652130.85
XDOT = -8317.220370 XDOT = -2596.296941
YDOT = 22020.403708 feet/sec YDOT = 6683.127723 meter/sec
ZDOT = -9222.900299 ZDOT = -2823.604827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10471938.47 X = -3191846.85
Y = -11967555.26 feet Y = -3647710.84 meter
Z = 15273300.21 Z = 4655301.90
XDOT = 9623.459289 XDOT = 2933.230391
YDOT = -20284.563492 feet/sec YDOT = -6182.734952 meter/sec
ZDOT = -9270.428528 ZDOT = -2825.626615
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 08259.54278687 .00020000 00000-0 20000-3 0 9077
2 25544 51.6394 272.9403 0006639 114.0719 246.1138 15.72118909 2756
Satellite: ISS
Catalog Number: 25544
Epoch time: 08259.54278687 = yrday.fracday
Element set: 907
Inclination: 51.6394 deg
RA of node: 272.9403 deg
Eccentricity: .0006639
Arg of perigee: 114.0719 deg
Mean anomaly: 246.1138 deg
Mean motion: 15.72118909 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 275
Checksum: 315
Coasting Arc #9 (Orbit 290)
---------------------------------------
Vector Time (GMT): 2008/260/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 609794.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1216067.68 A = 6735959.38 meter
Y = -6342880.55 meter E = .0018982
Z = 1892076.19 I = 51.32672
XDOT = 4612.129899 Wp = 82.66965
YDOT = 2569.616051 meter/sec RA = 267.29195 deg
ZDOT = 5604.263782 TA = 298.43739
MA = 298.62853
Ha = 195.263 n.mi
Hp = 184.451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3989723.36 X = 1277712.96
Y = -20809975.55 feet Y = -6328936.92 meter
Z = 6207599.06 Z = 1898134.23
XDOT = 15131.659773 XDOT = 4555.828499
YDOT = 8430.498856 feet/sec YDOT = 2620.877274 meter/sec
ZDOT = 18386.692197 ZDOT = 5626.532715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5734049.75 X = -1747738.36
Y = 20391423.36 feet Y = 6215305.84 meter
Z = 6230392.25 Z = 1899023.56
XDOT = -12756.106031 XDOT = -3888.061118
YDOT = -9276.865216 feet/sec YDOT = -2827.588518 meter/sec
ZDOT = 18473.028586 ZDOT = 5630.579113
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 08260.55984314 .00020000 00000-0 20000-3 0 9082
2 25544 51.6394 267.7320 0006596 118.0186 242.1644 15.72126803 2918
Satellite: ISS
Catalog Number: 25544
Epoch time: 08260.55984314 = yrday.fracday
Element set: 908
Inclination: 51.6394 deg
RA of node: 267.7320 deg
Eccentricity: .0006596
Arg of perigee: 118.0186 deg
Mean anomaly: 242.1644 deg
Mean motion: 15.72126803 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 291
Checksum: 292
Coasting Arc #10 (Orbit 305)
---------------------------------------
Vector Time (GMT): 2008/261/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 609794.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4272152.89 A = 6726282.47 meter
Y = -1144857.34 meter E = .0020052
Z = -5085492.31 I = 51.29660
XDOT = 194.965244 Wp = 107.94974
YDOT = -7526.364120 meter/sec RA = 262.11629 deg
ZDOT = 1529.438895 TA = 176.83599
MA = 176.82329
Ha = 195.235 n.mi
Hp = 184.423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14016249.63 X = -4234328.63
Y = -3756093.65 feet Y = -1192419.94 meter
Z = -16684686.06 Z = -5106154.76
XDOT = 639.649751 XDOT = 271.681924
YDOT = -24692.795669 feet/sec YDOT = -7523.754841 meter/sec
ZDOT = 5017.844143 ZDOT = 1530.572987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13627688.11 X = 4153719.33
Y = 4708938.21 feet Y = 1435284.37 meter
Z = -16764672.98 Z = -5109872.32
XDOT = -1972.112640 XDOT = -601.099933
YDOT = 23597.822041 feet/sec YDOT = 7192.616158 meter/sec
ZDOT = 5021.484276 ZDOT = 1530.548407
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 08261.51332293 .00020000 00000-0 20000-3 0 9093
2 25544 51.6394 262.8483 0006507 121.3286 238.8514 15.72108877 3060
Satellite: ISS
Catalog Number: 25544
Epoch time: 08261.51332293 = yrday.fracday
Element set: 909
Inclination: 51.6394 deg
RA of node: 262.8483 deg
Eccentricity: .0006507
Arg of perigee: 121.3286 deg
Mean anomaly: 238.8514 deg
Mean motion: 15.72108877 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 306
Checksum: 295
Coasting Arc #11 (Orbit 321)
---------------------------------------
Vector Time (GMT): 2008/262/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 609794.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 892110.69 A = 6737200.43 meter
Y = 6625656.26 meter E = .0016883
Z = -777701.22 I = 51.33835
XDOT = -4890.023735 Wp = 134.35227
YDOT = -28.946960 meter/sec RA = 256.99140 deg
ZDOT = -5947.123663 TA = 54.15749
MA = 54.00078
Ha = 195.166 n.mi
Hp = 184.534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2926872.33 X = 821733.23
Y = 21737717.38 feet Y = 6635238.81 meter
Z = -2551513.18 Z = -773538.58
XDOT = -16043.384958 XDOT = -4860.446050
YDOT = -94.970340 feet/sec YDOT = -83.464972 meter/sec
ZDOT = -19511.560573 ZDOT = -5970.807962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1808833.89 X = -551332.57
Y = -21861112.41 feet Y = -6663267.06 meter
Z = -2534766.66 Z = -772596.88
XDOT = 14310.819705 XDOT = 4361.937846
YDOT = 1053.963573 feet/sec YDOT = 321.248097 meter/sec
ZDOT = -19603.121074 ZDOT = -5975.031303
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 08262.53035667 .00020000 00000-0 20000-3 0 9103
2 25544 51.6387 257.6388 0006590 124.3669 235.8117 15.72146195 3227
Satellite: ISS
Catalog Number: 25544
Epoch time: 08262.53035667 = yrday.fracday
Element set: 910
Inclination: 51.6387 deg
RA of node: 257.6388 deg
Eccentricity: .0006590
Arg of perigee: 124.3669 deg
Mean anomaly: 235.8117 deg
Mean motion: 15.72146195 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 322
Checksum: 302
Coasting Arc #12 (Orbit 337)
---------------------------------------
Vector Time (GMT): 2008/263/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 609794.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4060411.70 A = 6725338.38 meter
Y = -1093079.48 meter E = .0008272
Z = 5242140.91 I = 51.30607
XDOT = 2243.980236 Wp = 115.88727
YDOT = 7367.539309 meter/sec RA = 251.83781 deg
ZDOT = -205.173981 TA = 336.04883
MA = 336.08729
Ha = 194.931 n.mi
Hp = 184.639
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13321560.70 X = 4046867.09
Y = -3586218.78 feet Y = -1047749.21 meter
Z = 17198625.04 Z = 5261833.87
XDOT = 7362.139883 XDOT = 2162.425162
YDOT = 24171.716892 feet/sec YDOT = 7392.176787 meter/sec
ZDOT = -673.142981 ZDOT = -194.470830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13339427.10 X = -4065857.38
Y = 3124711.21 feet Y = 952411.98 meter
Z = 17274649.42 Z = 5265313.14
XDOT = -6293.971898 XDOT = -1918.402634
YDOT = -23440.254890 feet/sec YDOT = -7144.589690 meter/sec
ZDOT = -631.037850 ZDOT = -192.340337
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 08263.54737767 .00020000 00000-0 20000-3 0 9116
2 25544 51.6383 252.4298 0006433 128.4129 231.7612 15.72165576 3384
Satellite: ISS
Catalog Number: 25544
Epoch time: 08263.54737767 = yrday.fracday
Element set: 911
Inclination: 51.6383 deg
RA of node: 252.4298 deg
Eccentricity: .0006433
Arg of perigee: 128.4129 deg
Mean anomaly: 231.7612 deg
Mean motion: 15.72165576 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 338
Checksum: 302
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