Date:
February 15th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4843 76 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 2650)
---------------------------------------
Vector Time (GMT): 2009/044/14:11:08
635
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3938748
65 A = 6729815
14 meter
Y = 2029422
14 meter E =
0017282
Z = -5078410
14 I = 51
41270
XDOT = -4962
583438 Wp = 72
98132
YDOT = -5644
524519 meter/sec RA = 218
88167 deg
ZDOT = 1602
731992 TA = 212
44029
MA = 212
54663
Ha = 197
213 n
mi
Hp = 186
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12922403
69 X = -3936479
64
Y = 6658209
10 feet Y = 1985389
20 meter
Z = -16661450
58 Z = -5097538
86
XDOT = -16281
441726 XDOT = -4906
882259
YDOT = -18518
781231 feet/sec YDOT = -5699
707496 meter/sec
ZDOT = 5258
307061 ZDOT = 1578
759711
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13282158
49 X = -4048401
91
Y = 5693912
36 feet Y = 1735504
49 meter
Z = -16735824
73 Z = -5101079
38
XDOT = -14485
999131 XDOT = -4415
332535
YDOT = -18702
833968 feet/sec YDOT = -5700
623794 meter/sec
ZDOT = 5164
407407 ZDOT = 1574
111378
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 09044
60431481
00010596 00000-0 82463-4 0 9004
2 25544 51
6388 219
7885 0008552 20
9724 339
1786 15
70883813 26512
Satellite: ISS
Catalog Number: 25544
Epoch time: 09044
60431481 = yrday
fracday
Element set: 900
Inclination: 51
6388 deg
RA of node: 219
7885 deg
Eccentricity:
0008552
Arg of perigee: 20
9724 deg
Mean anomaly: 339
1786 deg
Mean motion: 15
70883813 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2651
Checksum: 326
Coasting Arc #2 (Orbit 2666)
---------------------------------------
Vector Time (GMT): 2009/045/14:11:08
635
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5394728
78 A = 6740927
15 meter
Y = 4019302
24 meter E =
0011157
Z = -429825
36 I = 51
47379
XDOT = -3167
696283 Wp = 93
17560
YDOT = 3624
848467 meter/sec RA = 213
77181 deg
ZDOT = -5996
190069 TA = 91
49936
MA = 91
37156
Ha = 197
329 n
mi
Hp = 186
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17699241
39 X = 5351471
31
Y = 13186687
14 feet Y = 4079387
36 meter
Z = -1410188
20 Z = -403723
32
XDOT = -10392
704342 XDOT = -3178
866486
YDOT = 11892
547463 feet/sec YDOT = 3589
362795 meter/sec
ZDOT = -19672
539598 ZDOT = -6011
605783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16932452
86 X = 5161011
63
Y = 14167616
51 feet Y = 4318289
51 meter
Z = -1308119
63 Z = -398714
86
XDOT = -9902
391393 XDOT = -3018
248897
YDOT = 10056
868341 feet/sec YDOT = 3065
333470 meter/sec
ZDOT = -19732
311949 ZDOT = -6014
408682
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 09045
62216622
00010596 00000-0 82463-4 0 9016
2 25544 51
6386 214
5840 0008655 24
1373 336
0193 15
70903317 26671
Satellite: ISS
Catalog Number: 25544
Epoch time: 09045
62216622 = yrday
fracday
Element set: 901
Inclination: 51
6386 deg
RA of node: 214
5840 deg
Eccentricity:
0008655
Arg of perigee: 24
1373 deg
Mean anomaly: 336
0193 deg
Mean motion: 15
70903317 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2667
Checksum: 297
Coasting Arc #3 (Orbit 2682)
---------------------------------------
Vector Time (GMT): 2009/046/14:11:08
635
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1343671
14 A = 6729041
65 meter
Y = -4010592
84 meter E =
0009145
Z = 5227167
17 I = 51
46031
XDOT = 6972
990007 Wp = 46
96405
YDOT = 3201
855155 meter/sec RA = 208
64983 deg
ZDOT = 669
618365 TA = 36
68559
MA = 36
62302
Ha = 197
297 n
mi
Hp = 186
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4408369
89 X = 1363026
07
Y = -13158113
00 feet Y = -3995458
84 meter
Z = 17149498
59 Z = 5233741
71
XDOT = 22877
263801 XDOT = 6933
415239
YDOT = 10504
774131 feet/sec YDOT = 3279
609919 meter/sec
ZDOT = 2196
910646 ZDOT = 703
396558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4824501
30 X = 1470508
00
Y = -12977902
61 feet Y = -3955664
72 meter
Z = 17174783
72 Z = 5234874
08
XDOT = 21486
085430 XDOT = 6548
958839
YDOT = 11045
895395 feet/sec YDOT = 3366
788916 meter/sec
ZDOT = 2328
836272 ZDOT = 709
829296
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 09046
64001078
00010596 00000-0 82463-4 0 9027
2 25544 51
6397 209
3811 0008643 27
3109 332
8505 15
70921831 26832
Satellite: ISS
Catalog Number: 25544
Epoch time: 09046
64001078 = yrday
fracday
Element set: 902
Inclination: 51
6397 deg
RA of node: 209
3811 deg
Eccentricity:
0008643
Arg of perigee: 27
3109 deg
Mean anomaly: 332
8505 deg
Mean motion: 15
70921831 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2683
Checksum: 299
Coasting Arc #4 (Orbit 2697)
---------------------------------------
Vector Time (GMT): 2009/047/14:11:08
635
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6390856
48 A = 6739877
85 meter
Y = -1405639
52 meter E =
0016681
Z = -1585522
48 I = 51
52357
XDOT = -291
846183 Wp = 34
59612
YDOT = -5110
341198 meter/sec RA = 203
50736 deg
ZDOT = 5749
904370 TA = 307
89813
MA = 308
04886
Ha = 197
443 n
mi
Hp = 186
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20967376
91 X = -6366961
33
Y = -4611678
23 feet Y = -1476972
19 meter
Z = -5201845
41 Z = -1616510
81
XDOT = -957
500601 XDOT = -262
611434
YDOT = -16766
211281 feet/sec YDOT = -5113
441352 meter/sec
ZDOT = 18864
515648 ZDOT = 5748
557592
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20829377
71 X = -6348794
33
Y = -5075722
28 feet Y = -1547080
15 meter
Z = -5322756
22 Z = -1622376
10
XDOT = -1063
780461 XDOT = -324
240284
YDOT = -15266
682485 feet/sec YDOT = -4653
284821 meter/sec
ZDOT = 18858
833233 ZDOT = 5748
172369
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 09047
59423462
00010596 00000-0 82463-4 0 9038
2 25544 51
6402 204
5039 0008756 31
2188 328
9492 15
70896771 26985
Satellite: ISS
Catalog Number: 25544
Epoch time: 09047
59423462 = yrday
fracday
Element set: 903
Inclination: 51
6402 deg
RA of node: 204
5039 deg
Eccentricity:
0008756
Arg of perigee: 31
2188 deg
Mean anomaly: 328
9492 deg
Mean motion: 15
70896771 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2698
Checksum: 333
Coasting Arc #5 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2009/048/14:11:08
635
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1858934
43 A = 6731703
20 meter
Y = 4515676
88 meter E =
0018425
Z = -4651316
82 I = 51
52348
XDOT = -7135
056648 Wp = 54
77076
YDOT = 5
433985 meter/sec RA = 198
42396 deg
ZDOT = -2843
802372 TA = 186
99140
MA = 187
01713
Ha = 197
535 n
mi
Hp = 186
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6098866
24 X = 1830896
13
Y = 14815212
85 feet Y = 4536307
87 meter
Z = -15260225
78 Z = -4642354
29
XDOT = -23408
978504 XDOT = -7120
772657
YDOT = 17
828035 feet/sec YDOT = -74
274456 meter/sec
ZDOT = -9330
060275 ZDOT = -2878
429242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6112483
20 X = 1863084
88
Y = 14845909
82 feet Y = 4525033
31 meter
Z = -15224904
04 Z = -4640550
75
XDOT = -22271
938733 XDOT = -6788
486926
YDOT = -545
125771 feet/sec YDOT = -166
154335 meter/sec
ZDOT = -9465
049027 ZDOT = -2884
946943
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 09048
61206569
00010596 00000-0 82463-4 0 9040
2 25544 51
6402 199
3009 0008677 34
7210 325
4517 15
70906181 27145
Satellite: ISS
Catalog Number: 25544
Epoch time: 09048
61206569 = yrday
fracday
Element set: 904
Inclination: 51
6402 deg
RA of node: 199
3009 deg
Eccentricity:
0008677
Arg of perigee: 34
7210 deg
Mean anomaly: 325
4517 deg
Mean motion: 15
70906181 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2714
Checksum: 305
Coasting Arc #6 (Orbit 2729)
---------------------------------------
Vector Time (GMT): 2009/049/14:11:08
635
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5702232
24 A = 6736141
12 meter
Y = -1355823
32 meter E =
0019362
Z = 3311138
80 I = 51
56705
XDOT = 3862
264373 Wp = 70
36559
YDOT = 4730
240015 meter/sec RA = 193
25868 deg
ZDOT = -4685
852726 TA = 70
73836
MA = 70
52901
Ha = 197
589 n
mi
Hp = 186
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18708111
03 X = 5700884
87
Y = -4448239
25 feet Y = -1292065
25 meter
Z = 10863316
26 Z = 3338836
43
XDOT = 12671
471040 XDOT = 3831
845596
YDOT = 15519
160153 feet/sec YDOT = 4773
260115 meter/sec
ZDOT = -15373
532567 ZDOT = -4667
163984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18589487
87 X = 5666075
90
Y = -4675020
53 feet Y = -1424946
26 meter
Z = 10971190
21 Z = 3344018
78
XDOT = 12607
285950 XDOT = 3842
700758
YDOT = 14006
793858 feet/sec YDOT = 4269
270768 meter/sec
ZDOT = -15300
266777 ZDOT = -4663
521314
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 09049
62989010
00010596 00000-0 82463-4 0 9052
2 25544 51
6402 194
0979 0008788 39
4387 320
7412 15
70910771 27303
Satellite: ISS
Catalog Number: 25544
Epoch time: 09049
62989010 = yrday
fracday
Element set: 905
Inclination: 51
6402 deg
RA of node: 194
0979 deg
Eccentricity:
0008788
Arg of perigee: 39
4387 deg
Mean anomaly: 320
7412 deg
Mean motion: 15
70910771 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2730
Checksum: 325
Coasting Arc #7 (Orbit 2745)
---------------------------------------
Vector Time (GMT): 2009/050/14:11:08
635
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4715335
34 A = 6735926
93 meter
Y = -3392188
00 meter E =
0019691
Z = 3387918
92 I = 51
59607
XDOT = 5431
325306 Wp = 70
84325
YDOT = -2919
053975 meter/sec RA = 188
19282 deg
ZDOT = 4621
224030 TA = 329
16570
MA = 329
28121
Ha = 197
697 n
mi
Hp = 185
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15470260
30 X = -4693510
42
Y = -11129225
73 feet Y = -3444795
65 meter
Z = 11115219
54 Z = 3365065
27
XDOT = 17819
308748 XDOT = 5441
114406
YDOT = -9576
948736 feet/sec YDOT = -2858
263086 meter/sec
ZDOT = 15161
496160 ZDOT = 4647
632556
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15854498
82 X = -4832451
24
Y = -10667846
61 feet Y = -3251559
65 meter
Z = 11025817
00 Z = 3360669
02
XDOT = 16664
490245 XDOT = 5079
336627
YDOT = -8937
572306 feet/sec YDOT = -2724
172039 meter/sec
ZDOT = 15264
222904 ZDOT = 4652
535141
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 09050
64770479
00010596 00000-0 82463-4 0 9064
2 25544 51
6407 188
8943 0008836 42
7395 317
4452 15
70964892 27467
Satellite: ISS
Catalog Number: 25544
Epoch time: 09050
64770479 = yrday
fracday
Element set: 906
Inclination: 51
6407 deg
RA of node: 188
8943 deg
Eccentricity:
0008836
Arg of perigee: 42
7395 deg
Mean anomaly: 317
4452 deg
Mean motion: 15
70964892 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2746
Checksum: 351
Coasting Arc #8 (Orbit 2760)
---------------------------------------
Vector Time (GMT): 2009/051/14:11:08
635
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3475685
87 A = 6731514
07 meter
Y = 3475306
54 meter E =
0016630
Z = -4612390
77 I = 51
61110
XDOT = -6572
703256 Wp = 81
35231
YDOT = -2682
940605 meter/sec RA = 183
03195 deg
ZDOT = 2942
838081 TA = 217
83462
MA = 217
95163
Ha = 197
666 n
mi
Hp = 185
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11403168
85 X = -3491883
40
Y = 11401924
34 feet Y = 3436348
87 meter
Z = -15132515
65 Z = -4629314
55
XDOT = -21563
987060 XDOT = -6556
509093
YDOT = -8802
298573 feet/sec YDOT = -2756
349873 meter/sec
ZDOT = 9654
980581 ZDOT = 2910
947996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10772290
12 X = -3283394
03
Y = 11916422
86 feet Y = 3632125
69 meter
Z = -15198217
02 Z = -4632416
55
XDOT = -21136
914754 XDOT = -6442
531617
YDOT = -7000
221808 feet/sec YDOT = -2133
667607 meter/sec
ZDOT = 9530
386105 ZDOT = 2904
861685
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 09051
60190173
00010596 00000-0 82463-4 0 9079
2 25544 51
6408 184
0174 0008928 45
9387 314
2509 15
70977715 27613
Satellite: ISS
Catalog Number: 25544
Epoch time: 09051
60190173 = yrday
fracday
Element set: 907
Inclination: 51
6408 deg
RA of node: 184
0174 deg
Eccentricity:
0008928
Arg of perigee: 45
9387 deg
Mean anomaly: 314
2509 deg
Mean motion: 15
70977715 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2761
Checksum: 322
Coasting Arc #9 (Orbit 2776)
---------------------------------------
Vector Time (GMT): 2009/052/14:11:08
635
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6428922
42 A = 6739638
64 meter
Y = 1113589
92 meter E =
0011573
Z = -1697393
07 I = 51
66730
XDOT = -2296
816696 Wp = 92
34254
YDOT = 4602
493368 meter/sec RA = 177
95679 deg
ZDOT = -5713
665671 TA = 106
37861
MA = 106
25134
Ha = 197
786 n
mi
Hp = 185
769
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21092265
16 X = 6424237
67
Y = 3653510
24 feet Y = 1185455
66 meter
Z = -5568874
89 Z = -1666173
60
XDOT = -7535
487849 XDOT = -2320
356638
YDOT = 15100
043859 feet/sec YDOT = 4576
677374 meter/sec
ZDOT = -18745
622279 ZDOT = -5724
880508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21314011
43 X = 6496510
68
Y = 2299367
67 feet Y = 700847
27 meter
Z = -5447015
65 Z = -1660250
37
XDOT = -6281
715605 XDOT = -1914
666916
YDOT = 13988
390694 feet/sec YDOT = 4263
661483 meter/sec
ZDOT = -18788
965109 ZDOT = -5726
876565
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 09052
61970399
00010596 00000-0 82463-4 0 9088
2 25544 51
6405 178
8138 0008938 49
5009 310
6930 15
70960398 27777
Satellite: ISS
Catalog Number: 25544
Epoch time: 09052
61970399 = yrday
fracday
Element set: 908
Inclination: 51
6405 deg
RA of node: 178
8138 deg
Eccentricity:
0008938
Arg of perigee: 49
5009 deg
Mean anomaly: 310
6930 deg
Mean motion: 15
70960398 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2777
Checksum: 345
Coasting Arc #10 (Orbit 2792)
---------------------------------------
Vector Time (GMT): 2009/053/14:11:08
635
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 408317
00 A = 6728820
85 meter
Y = -4214005
65 meter E =
0012115
Z = 5222304
55 I = 51
66180
XDOT = 7652
439487 Wp = 54
76549
YDOT = -300
134223 meter/sec RA = 172
82352 deg
ZDOT = -832
291056 TA = 43
19934
MA = 43
10437
Ha = 197
711 n
mi
Hp = 185
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1339622
71 X = 430040
07
Y = -13825477
85 feet Y = -4209318
02 meter
Z = 17133545
11 Z = 5224340
97
XDOT = 25106
428763 XDOT = 7659
269900
YDOT = -984
692334 feet/sec YDOT = -214
522024 meter/sec
ZDOT = -2730
613702 ZDOT = -795
099964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 118023
44 X = 35973
54
Y = -13880375
67 feet Y = -4230738
51 meter
Z = 17141121
21 Z = 5224613
74
XDOT = 23947
578141 XDOT = 7299
221817
YDOT = -3022
620425 feet/sec YDOT = -921
294706 meter/sec
ZDOT = -2585
571321 ZDOT = -788
082139
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 09053
63749718
00010596 00000-0 82463-4 0 9091
2 25544 51
6414 173
6101 0008947 52
2558 307
9413 15
71013847 27932
Satellite: ISS
Catalog Number: 25544
Epoch time: 09053
63749718 = yrday
fracday
Element set: 909
Inclination: 51
6414 deg
RA of node: 173
6101 deg
Eccentricity:
0008947
Arg of perigee: 52
2558 deg
Mean anomaly: 307
9413 deg
Mean motion: 15
71013847 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2793
Checksum: 323
Coasting Arc #11 (Orbit 2807)
---------------------------------------
Vector Time (GMT): 2009/054/14:11:08
635
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6523129
27 A = 6740826
42 meter
Y = 1641776
21 meter E =
0020627
Z = -274836
97 I = 51
73064
XDOT = -1392
066730 Wp = 48
63329
YDOT = -4571
294216 meter/sec RA = 167
72002 deg
ZDOT = 6037
359543 TA = 308
38607
MA = 308
57117
Ha = 197
909 n
mi
Hp = 185
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21401342
76 X = -6539668
00
Y = 5386404
90 feet Y = 1568738
30 meter
Z = -901696
09 Z = -306565
69
XDOT = -4567
148063 XDOT = -1370
173884
YDOT = -14997
684436 feet/sec YDOT = -4586
738423 meter/sec
ZDOT = 19807
610049 ZDOT = 6030
650463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20764622
13 X = -6329056
82
Y = 7458087
08 feet Y = 2273224
94 meter
Z = -1025324
50 Z = -312518
91
XDOT = -5585
412928 XDOT = -1702
433860
YDOT = -12952
108365 feet/sec YDOT = -3947
802630 meter/sec
ZDOT = 19781
036372 ZDOT = 6029
259886
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 09054
59167426
00010596 00000-0 82463-4 0 9109
2 25544 51
6414 168
7329 0009164 55
2054 304
9969 15
70950833 28089
Satellite: ISS
Catalog Number: 25544
Epoch time: 09054
59167426 = yrday
fracday
Element set: 910
Inclination: 51
6414 deg
RA of node: 168
7329 deg
Eccentricity:
0009164
Arg of perigee: 55
2054 deg
Mean anomaly: 304
9969 deg
Mean motion: 15
70950833 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2808
Checksum: 328
Coasting Arc #12 (Orbit 2823)
---------------------------------------
Vector Time (GMT): 2009/055/14:11:08
635
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2709259
80 A = 6729438
71 meter
Y = 3410578
19 meter E =
0022661
Z = -5149556
08 I = 51
72029
XDOT = -6798
540831 Wp = 71
66062
YDOT = 3284
236225 meter/sec RA = 162
62838 deg
ZDOT = -1399
697069 TA = 184
90146
MA = 184
92369
Ha = 197
903 n
mi
Hp = 185
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8888647
63 X = 2695935
76
Y = 11189560
98 feet Y = 3440799
86 meter
Z = -16894869
04 Z = -5136427
43
XDOT = -22304
923985 XDOT = -6827
961123
YDOT = 10775
053230 feet/sec YDOT = 3208
046391 meter/sec
ZDOT = -4592
181985 ZDOT = -1432
795218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10214696
75 X = 3113439
57
Y = 10080301
95 feet Y = 3072476
03 meter
Z = -16843349
26 Z = -5133852
86
XDOT = -20154
111884 XDOT = -6142
973302
YDOT = 12523
657366 feet/sec YDOT = 3817
210765 meter/sec
ZDOT = -4721
015447 ZDOT = -1438
965508
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 09055
60945503
00010596 00000-0 82463-4 0 9113
2 25544 51
6407 163
5296 0009049 59
3252 300
8800 15
70973613 28242
Satellite: ISS
Catalog Number: 25544
Epoch time: 09055
60945503 = yrday
fracday
Element set: 911
Inclination: 51
6407 deg
RA of node: 163
5296 deg
Eccentricity:
0009049
Arg of perigee: 59
3252 deg
Mean anomaly: 300
8800 deg
Mean motion: 15
70973613 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2824
Checksum: 305
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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