Date:
September 4th 2008
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) : 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 86)
---------------------------------------
Vector Time (GMT): 2008/247/12:53:42
871
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5131530
25 A = 6730463
09 meter
Y = 1188135
42 meter E =
0015862
Z = 4177059
49 I = 51
49247
XDOT = -4218
736600 Wp = 94
44100
YDOT = 5307
632090 meter/sec RA = 333
91486 deg
ZDOT = 3659
897916 TA = 318
12335
MA = 318
24457
Ha = 195
481 n
mi
Hp = 184
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16835729
16 X = 5097571
47
Y = 3898082
07 feet Y = 1245329
46 meter
Z = 13704263
43 Z = 4201906
01
XDOT = -13840
999345 XDOT = -4295
553032
YDOT = 17413
491110 feet/sec YDOT = 5260
026412 meter/sec
ZDOT = 12007
539094 ZDOT = 3639
216394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16418016
22 X = -5004211
34
Y = -5142120
21 feet Y = -1567318
24 meter
Z = 13800398
53 Z = 4206361
47
XDOT = 14799
590659 XDOT = 4510
915233
YDOT = -15125
701935 feet/sec YDOT = -4610
313950 meter/sec
ZDOT = 11928
070179 ZDOT = 3635
675791
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 08247
59154239
00020000 00000-0 20000-3 0 9008
2 25544 51
6427 334
1302 0006278 76
2956 283
8905 15
71903324 876
Satellite: ISS
Catalog Number: 25544
Epoch time: 08247
59154239 = yrday
fracday
Element set: 900
Inclination: 51
6427 deg
RA of node: 334
1302 deg
Eccentricity:
0006278
Arg of perigee: 76
2956 deg
Mean anomaly: 283
8905 deg
Mean motion: 15
71903324 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 87
Checksum: 296
Coasting Arc #2 (Orbit 101)
---------------------------------------
Vector Time (GMT): 2008/248/12:53:42
871
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2550014
21 A = 6732163
79 meter
Y = -5009243
99 meter E =
0012004
Z = -3715245
64 I = 51
47150
XDOT = 6392
680511 Wp = 89
59807
YDOT = 96
128493 meter/sec RA = 328
73412 deg
ZDOT = 4270
067714 TA = 225
58460
MA = 225
68292
Ha = 195
632 n
mi
Hp = 184
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8366188
34 X = 2623886
94
Y = -16434527
54 feet Y = -4980315
33 meter
Z = -12189126
12 Z = -3702678
02
XDOT = 20973
361258 XDOT = 6370
387143
YDOT = 315
382195 feet/sec YDOT = 167
490609 meter/sec
ZDOT = 14009
408512 ZDOT = 4301
069361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9370474
06 X = -2856120
49
Y = 15920180
49 feet Y = 4852471
01 meter
Z = -12140991
20 Z = -3700574
12
XDOT = -19678
857461 XDOT = -5998
115754
YDOT = -837
667722 feet/sec YDOT = -255
321122 meter/sec
ZDOT = 14129
234874 ZDOT = 4306
590790
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 08248
54516499
00020000 00000-0 20000-3 0 9015
2 25544 51
6418 329
2490 0006430 79
3380 280
8506 15
71921548 1024
Satellite: ISS
Catalog Number: 25544
Epoch time: 08248
54516499 = yrday
fracday
Element set: 901
Inclination: 51
6418 deg
RA of node: 329
2490 deg
Eccentricity:
0006430
Arg of perigee: 79
3380 deg
Mean anomaly: 280
8506 deg
Mean motion: 15
71921548 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 102
Checksum: 291
Coasting Arc #3 (Orbit 117)
---------------------------------------
Vector Time (GMT): 2008/249/12:53:42
871
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5806033
59 A = 6733451
30 meter
Y = 1053695
88 meter E =
0011113
Z = -3253463
22 I = 51
45124
XDOT = 1583
554566 Wp = 87
21174
YDOT = -5847
990521 meter/sec RA = 323
65245 deg
ZDOT = -4733
330369 TA = 130
91226
MA = 130
81597
Ha = 195
645 n
mi
Hp = 184
565
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19048666
62 X = -5801579
84
Y = 3457007
47 feet Y = 988794
33 meter
Z = -10674091
93 Z = -3281658
28
XDOT = 5195
388996 XDOT = 1671
823829
YDOT = -19186
320608 feet/sec YDOT = -5829
788821 meter/sec
ZDOT = -15529
299111 ZDOT = -4725
422941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19111803
25 X = 5825277
63
Y = -2684281
11 feet Y = -818168
88 meter
Z = -10782970
40 Z = -3286649
38
XDOT = -6253
521641 XDOT = -1906
073396
YDOT = 17562
682092 feet/sec YDOT = 5353
105502 meter/sec
ZDOT = -15499
247844 ZDOT = -4724
170743
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 08249
56235117
00020000 00000-0 20000-3 0 9024
2 25544 51
6414 324
0410 0006490 82
3688 277
8211 15
71909552 1183
Satellite: ISS
Catalog Number: 25544
Epoch time: 08249
56235117 = yrday
fracday
Element set: 902
Inclination: 51
6414 deg
RA of node: 324
0410 deg
Eccentricity:
0006490
Arg of perigee: 82
3688 deg
Mean anomaly: 277
8211 deg
Mean motion: 15
71909552 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 118
Checksum: 279
Coasting Arc #4 (Orbit 133)
---------------------------------------
Vector Time (GMT): 2008/250/12:53:42
871
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -197319
12 A = 6729126
14 meter
Y = 4981209
17 meter E =
0014982
Z = 4509686
62 I = 51
41459
XDOT = -6585
250289 Wp = 73
81840
YDOT = 2543
852913 meter/sec RA = 318
47007 deg
ZDOT = -3085
383227 TA = 47
06332
MA = 46
93773
Ha = 195
534 n
mi
Hp = 184
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -647372
44 X = -274912
47
Y = 16342549
76 feet Y = 4978568
77 meter
Z = 14795559
78 Z = 4508539
58
XDOT = -21605
151867 XDOT = -6598
218331
YDOT = 8345
974123 feet/sec YDOT = 2470
140350 meter/sec
ZDOT = -10122
648383 ZDOT = -3117
406000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1113504
12 X = 339396
06
Y = -16321042
92 feet Y = -4974653
88 meter
Z = 14791561
09 Z = 4508467
82
XDOT = 20545
722238 XDOT = 6262
336138
YDOT = -7921
690697 feet/sec YDOT = -2414
531325 meter/sec
ZDOT = -10246
191819 ZDOT = -3123
039267
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 08250
57952383
00020000 00000-0 20000-3 0 9039
2 25544 51
6418 318
8335 0006358 84
4613 275
7275 15
71969503 1345
Satellite: ISS
Catalog Number: 25544
Epoch time: 08250
57952383 = yrday
fracday
Element set: 903
Inclination: 51
6418 deg
RA of node: 318
8335 deg
Eccentricity:
0006358
Arg of perigee: 84
4613 deg
Mean anomaly: 275
7275 deg
Mean motion: 15
71969503 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 134
Checksum: 306
Coasting Arc #5 (Orbit 149)
---------------------------------------
Vector Time (GMT): 2008/251/12:53:42
871
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5452249
43 A = 6736135
73 meter
Y = -3340255
86 meter E =
0020538
Z = 2091919
87 I = 51
41628
XDOT = 1089
115934 Wp = 75
38244
YDOT = 5259
889279 meter/sec RA = 313
37618 deg
ZDOT = 5520
073894 TA = 308
05724
MA = 308
24238
Ha = 195
681 n
mi
Hp = 184
503
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17887957
43 X = 5479033
29
Y = -10958844
70 feet Y = -3279135
94 meter
Z = 6863254
16 Z = 2118471
97
XDOT = 3573
215006 XDOT = 1003
402483
YDOT = 17256
854591 feet/sec YDOT = 5271
589082 meter/sec
ZDOT = 18110
478656 ZDOT = 5525
156700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17915457
66 X = -5460631
49
Y = 10848803
83 feet Y = 3306715
41 meter
Z = 6965585
99 Z = 2123110
61
XDOT = -2572
127568 XDOT = -783
984483
YDOT = -15971
515432 feet/sec YDOT = -4868
117904 meter/sec
ZDOT = 18130
584015 ZDOT = 5526
202008
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 08251
59668935
00020000 00000-0 20000-3 0 9040
2 25544 51
6412 313
6258 0006686 87
6020 272
5908 15
71928105 1506
Satellite: ISS
Catalog Number: 25544
Epoch time: 08251
59668935 = yrday
fracday
Element set: 904
Inclination: 51
6412 deg
RA of node: 313
6258 deg
Eccentricity:
0006686
Arg of perigee: 87
6020 deg
Mean anomaly: 272
5908 deg
Mean motion: 15
71928105 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 150
Checksum: 298
Coasting Arc #6 (Orbit 164)
---------------------------------------
Vector Time (GMT): 2008/252/12:53:42
871
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1990178
07 A = 6726962
44 meter
Y = -3996629
80 meter E =
0019915
Z = -5049450
56 I = 51
36682
XDOT = 5625
229158 Wp = 98
77183
YDOT = -4947
857545 meter/sec RA = 308
20507 deg
ZDOT = 1701
842206 TA = 187
68694
MA = 187
71751
Ha = 195
644 n
mi
Hp = 184
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6529455
59 X = -1920809
89
Y = -13112302
48 feet Y = -4018497
17 meter
Z = -16566438
84 Z = -5058950
41
XDOT = 18455
476239 XDOT = 5671
871579
YDOT = -16233
128430 feet/sec YDOT = -4884
692229 meter/sec
ZDOT = 5583
471804 ZDOT = 1729
282766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6578990
47 X = 2005276
30
Y = 13040457
33 feet Y = 3974731
39 meter
Z = -16603509
25 Z = -5060749
62
XDOT = -17291
789162 XDOT = -5270
537336
YDOT = 15955
938137 feet/sec YDOT = 4863
369944 meter/sec
ZDOT = 5689
097371 ZDOT = 1734
036879
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
55026890
00020000 00000-0 20000-3 0 9056
2 25544 51
6418 308
7434 0006556 90
7881 269
4032 15
71946442 1652
Satellite: ISS
Catalog Number: 25544
Epoch time: 08252
55026890 = yrday
fracday
Element set: 905
Inclination: 51
6418 deg
RA of node: 308
7434 deg
Eccentricity:
0006556
Arg of perigee: 90
7881 deg
Mean anomaly: 269
4032 deg
Mean motion: 15
71946442 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 165
Checksum: 300
Coasting Arc #7 (Orbit 180)
---------------------------------------
Vector Time (GMT): 2008/253/12:53:42
871
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4213279
49 A = 6737534
41 meter
Y = 5178126
71 meter E =
0015459
Z = -880261
71 I = 51
38616
XDOT = -3271
229159 Wp = 122
53535
YDOT = -3655
582232 meter/sec RA = 303
08883 deg
ZDOT = -5930
299380 TA = 67
09598
MA = 66
93288
Ha = 195
595 n
mi
Hp = 184
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13823095
44 X = -4266592
86
Y = 16988604
70 feet Y = 5130713
31 meter
Z = -2887997
72 Z = -900859
18
XDOT = -10732
379131 XDOT = -3201
300506
YDOT = -11993
380025 feet/sec YDOT = -3691
771937 meter/sec
ZDOT = -19456
362796 ZDOT = -5946
021144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13320927
71 X = 4060218
77
Y = -17371818
68 feet Y = -5294930
33 meter
Z = -2967151
66 Z = -904387
83
XDOT = 9688
581091 XDOT = 2953
079516
YDOT = 10717
260382 feet/sec YDOT = 3266
620965 meter/sec
ZDOT = -19517
457387 ZDOT = -5948
921012
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
56741016
00020000 00000-0 20000-3 0 9063
2 25544 51
6420 303
5354 0006697 94
3173 265
8754 15
71994381 1813
Satellite: ISS
Catalog Number: 25544
Epoch time: 08253
56741016 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 303
5354 deg
Eccentricity:
0006697
Arg of perigee: 94
3173 deg
Mean anomaly: 265
8754 deg
Mean motion: 15
71994381 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 181
Checksum: 298
Coasting Arc #8 (Orbit 196)
---------------------------------------
Vector Time (GMT): 2008/254/12:53:42
871
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3569428
15 A = 6725779
86 meter
Y = 2222403
20 meter E =
0009106
Z = 5241553
45 I = 51
33074
XDOT = -3790
891114 Wp = 91
84563
YDOT = 6703
274698 meter/sec RA = 297
93802 deg
ZDOT = -260
522404 TA =
63688
MA =
63572
Ha = 195
487 n
mi
Hp = 184
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11710722
29 X = 3518849
24
Y = 7291349
09 feet Y = 2262035
80 meter
Z = 17196697
66 Z = 5258770
77
XDOT = -12437
306803 XDOT = -3864
300899
YDOT = 21992
371056 feet/sec YDOT = 6660
472314 meter/sec
ZDOT = -854
732298 ZDOT = -279
116746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11931375
99 X = -3636683
40
Y = -6756236
77 feet Y = -2059300
97 meter
Z = 17263450
71 Z = 5261899
78
XDOT = 10927
397522 XDOT = 3330
670765
YDOT = -21664
503174 feet/sec YDOT = -6603
340567 meter/sec
ZDOT = -926
001935 ZDOT = -282
245390
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
58453996
00020000 00000-0 20000-3 0 9074
2 25544 51
6409 298
3279 0006736 97
8167 262
3760 15
72015326 1972
Satellite: ISS
Catalog Number: 25544
Epoch time: 08254
58453996 = yrday
fracday
Element set: 907
Inclination: 51
6409 deg
RA of node: 298
3279 deg
Eccentricity:
0006736
Arg of perigee: 97
8167 deg
Mean anomaly: 262
3760 deg
Mean motion: 15
72015326 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 197
Checksum: 328
Coasting Arc #9 (Orbit 211)
---------------------------------------
Vector Time (GMT): 2008/255/12:53:42
871
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2289303
63 A = 6737731
25 meter
Y = -6318419
25 meter E =
0015918
Z = -422161
55 I = 51
35900
XDOT = 4651
658239 Wp = 62
90302
YDOT = 1297
060359 meter/sec RA = 292
79523 deg
ZDOT = 5992
623458 TA = 292
49305
MA = 292
66150
Ha = 195
568 n
mi
Hp = 184
393
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7510838
68 X = 2361837
83
Y = -20729721
94 feet Y = -6292413
38 meter
Z = -1385044
44 Z = -410863
89
XDOT = 15261
345930 XDOT = 4607
697731
YDOT = 4255
447372 feet/sec YDOT = 1348
832200 meter/sec
ZDOT = 19660
838118 ZDOT = 6015
114228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6205896
72 X = -1891557
32
Y = 21159830
46 feet Y = 6449516
32 meter
Z = -1341953
10 Z = -409027
30
XDOT = -13842
244620 XDOT = -4219
116160
YDOT = -2846
084135 feet/sec YDOT = -867
486444 meter/sec
ZDOT = 19747
896377 ZDOT = 6019
158816
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
53808956
00020000 00000-0 20000-3 0 9081
2 25544 51
6414 293
4459 0006710 100
7107 259
4810 15
72023039 2125
Satellite: ISS
Catalog Number: 25544
Epoch time: 08255
53808956 = yrday
fracday
Element set: 908
Inclination: 51
6414 deg
RA of node: 293
4459 deg
Eccentricity:
0006710
Arg of perigee: 100
7107 deg
Mean anomaly: 259
4810 deg
Mean motion: 15
72023039 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 212
Checksum: 278
Coasting Arc #10 (Orbit 227)
---------------------------------------
Vector Time (GMT): 2008/256/12:53:42
871
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4335999
09 A = 6726196
51 meter
Y = -3031
77 meter E =
0020609
Z = -5159926
29 I = 51
30982
XDOT = 1393
650285 Wp = 88
41146
YDOT = -7463
845408 meter/sec RA = 287
66654 deg
ZDOT = -1170
201382 TA = 170
35497
MA = 170
31534
Ha = 195
531 n
mi
Hp = 184
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14225718
79 X = -4310577
14
Y = -9946
74 feet Y = -51377
49 meter
Z = -16928892
03 Z = -5180928
65
XDOT = 4572
343456 XDOT = 1482
693207
YDOT = -24487
681786 feet/sec YDOT = -7447
762993 meter/sec
ZDOT = -3839
243378 ZDOT = -1163
214480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14084309
66 X = 4292897
58
Y = -1117124
50 feet Y = -340499
55 meter
Z = -17010079
77 Z = -5184672
31
XDOT = -2707
604550 XDOT = -825
277867
YDOT = 23749
105641 feet/sec YDOT = 7238
727399 meter/sec
ZDOT = -3812
932481 ZDOT = -1162
181820
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
55519736
00020000 00000-0 20000-3 0 9090
2 25544 51
6413 288
2375 0006667 104
8333 255
3568 15
72022911 2280
Satellite: ISS
Catalog Number: 25544
Epoch time: 08256
55519736 = yrday
fracday
Element set: 909
Inclination: 51
6413 deg
RA of node: 288
2375 deg
Eccentricity:
0006667
Arg of perigee: 104
8333 deg
Mean anomaly: 255
3568 deg
Mean motion: 15
72022911 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 228
Checksum: 302
Coasting Arc #11 (Orbit 243)
---------------------------------------
Vector Time (GMT): 2008/257/12:53:42
871
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -123990
55 A = 6736580
86 meter
Y = 6529455
98 meter E =
0020808
Z = 1614676
05 I = 51
33585
XDOT = -4983
454148 Wp = 113
55624
YDOT = 1332
334360 meter/sec RA = 282
49785 deg
ZDOT = -5720
418702 TA = 48
54157
MA = 48
36306
Ha = 195
495 n
mi
Hp = 184
367
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -406793
13 X = -204838
52
Y = 21422099
68 feet Y = 6527617
51 meter
Z = 5297493
59 Z = 1613876
89
XDOT = -16349
915183 XDOT = -4970
193555
YDOT = 4371
175721 feet/sec YDOT = 1276
680259 meter/sec
ZDOT = -18767
777895 ZDOT = -5744
596049
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1640912
95 X = -500150
27
Y = -21363646
25 feet Y = -6511639
38 meter
Z = 5295025
71 Z = 1613923
84
XDOT = 14184
261410 XDOT = 4323
362878
YDOT = -5804
899866 feet/sec YDOT = -1769
333479 meter/sec
ZDOT = -18861
112749 ZDOT = -5748
867166
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
57229371
00020000 00000-0 20000-3 0 9108
2 25544 51
6396 283
0289 0006791 107
3796 252
8110 15
72060473 2444
Satellite: ISS
Catalog Number: 25544
Epoch time: 08257
57229371 = yrday
fracday
Element set: 910
Inclination: 51
6396 deg
RA of node: 283
0289 deg
Eccentricity:
0006791
Arg of perigee: 107
3796 deg
Mean anomaly: 252
8110 deg
Mean motion: 15
72060473 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 244
Checksum: 294
Coasting Arc #12 (Orbit 259)
---------------------------------------
Vector Time (GMT): 2008/258/12:53:42
871
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4144427
36 A = 6727745
65 meter
Y = -2315725
84 meter E =
0013941
Z = 4758461
72 I = 51
30026
XDOT = 1107
021825 Wp = 115
37117
YDOT = 7193
853132 meter/sec RA = 277
38871 deg
ZDOT = 2525
091700 TA = 309
73468
MA = 309
85745
Ha = 195
355 n
mi
Hp = 184
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13597202
64 X = 4146898
46
Y = -7597525
71 feet Y = -2269366
23 meter
Z = 15611751
04 Z = 4778601
50
XDOT = 3631
961369 XDOT = 1014
230312
YDOT = 23601
880355 feet/sec YDOT = 7205
713883 meter/sec
ZDOT = 8284
421589 ZDOT = 2530
243587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12553269
96 X = -3826236
68
Y = 9088004
49 feet Y = 2770023
77 meter
Z = 15689380
95 Z = 4782123
31
XDOT = -5589
330393 XDOT = -1703
627904
YDOT = -22123
915254 feet/sec YDOT = -6743
369369 meter/sec
ZDOT = 8305
032394 ZDOT = 2531
373874
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
58937836
00020000 00000-0 20000-3 0 9113
2 25544 51
6388 277
8202 0006714 110
8421 249
3460 15
72065476 2605
Satellite: ISS
Catalog Number: 25544
Epoch time: 08258
58937836 = yrday
fracday
Element set: 911
Inclination: 51
6388 deg
RA of node: 277
8202 deg
Eccentricity:
0006714
Arg of perigee: 110
8421 deg
Mean anomaly: 249
3460 deg
Mean motion: 15
72065476 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 260
Checksum: 300
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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