SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2006/252/15:14:54 972 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 12 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 16339
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
260/14:04:57
861 0
4 0
4 1
6
007/22:50:02
889 -1
1 -0
0 189
6
000/00:00:05
778 -1
0 -1
5 180
4
260/14:32:56
832 -0
3 1
0 1
0
007/23:18:01
861 0
7 0
0 190
2
000/00:00:03
721 0
7 -0
0 180
6
260/16:14:54
972 -0
0 0
0 0
0
008/01:00:00
001 0
0 0
0 190
2
000/00:00:00
043 0
0 0
0 180
5
261/17:19:54
969 -0
9 -1
5 1
5
009/02:04:59
997 0
3 0
0 190
2
000/00:00:05
639 1
2 -0
0 179
6
Coasting Arc #1 (Orbit 91)
---------------------------------------
Vector Time (GMT): 2006/258/08:18:45
000
Vector Time (MET): 005/17:03:50
028
Weight (LBS) : 209988
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4197950
51 A = 6715352
86 meter
Y = -592083
34 meter E =
0013134
Z = 5210123
28 I = 51
92811
XDOT = -216
230430 Wp = 358
68449
YDOT = -7630
334359 meter/sec RA = 82
31821 deg
ZDOT = -1028
542373 TA = 101
15541
MA = 101
00772
Ha = 189
623 n
mi
Hp = 180
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13772803
50 X = -4216319
90
Y = -1942530
66 feet Y = -639180
25 meter
Z = 17093580
30 Z = 5189685
04
XDOT = -709
417421 XDOT = -125
803518
YDOT = -25033
905378 feet/sec YDOT = -7632
248750 meter/sec
ZDOT = -3374
482851 ZDOT = -1029
373563
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4822415
03 X = 1469872
10
Y = 13145626
63 feet Y = 4006787
00 meter
Z = 17017368
85 Z = 5186894
03
XDOT = -20794
643863 XDOT = -6338
207449
YDOT = 12056
743422 feet/sec YDOT = 3674
895395 meter/sec
ZDOT = -3378
621153 ZDOT = -1029
803728
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
SHUTTLE
1 29391U 06036A 06258
39221257
00014500 00000-0 95600-4 0 9007
2 29391 51
6343 82
7833 0011622 343
3367 16
7414 15
75791565 925
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06258
39221257 = yrday
fracday
Element set: 900
Inclination: 51
6343 deg
RA of node: 82
7833 deg
Eccentricity:
0011622
Arg of perigee: 343
3367 deg
Mean anomaly: 16
7414 deg
Mean motion: 15
75791565 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 92
Checksum: 300
Coasting Arc #2 (Orbit 107)
---------------------------------------
Vector Time (GMT): 2006/259/08:23:19
445
Vector Time (MET): 006/17:08:24
474
Weight (LBS) : 209988
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1046150
78 A = 6723304
46 meter
Y = 5922981
99 meter E =
0016867
Z = 2979063
20 I = 51
94924
XDOT = -4791
740682 Wp = 38
97828
YDOT = -3370
622899 meter/sec RA = 77
20649 deg
ZDOT = 5016
394713 TA = 355
32914
MA = 355
34486
Ha = 189
849 n
mi
Hp = 180
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3432253
21 X = -1126846
71
Y = 19432355
60 feet Y = 5910819
09 meter
Z = 9773829
39 Z = 2973785
27
XDOT = -15720
933995 XDOT = -4778
021567
YDOT = -11058
474078 feet/sec YDOT = -3424
187307 meter/sec
ZDOT = 16457
987904 ZDOT = 4993
149767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18542140
63 X = 5651644
46
Y = -6778939
82 feet Y = -2066220
86 meter
Z = 9754975
29 Z = 2973316
47
XDOT = -2080
880007 XDOT = -634
252226
YDOT = 17877
504663 feet/sec YDOT = 5449
063421 meter/sec
ZDOT = 16370
937363 ZDOT = 4989
861708
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
SHUTTLE
1 29391U 06036A 06259
40690584
00014500 00000-0 95600-4 0 9014
2 29391 51
6340 77
5574 0011781 347
6079 12
4794 15
75763564 1089
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06259
40690584 = yrday
fracday
Element set: 901
Inclination: 51
6340 deg
RA of node: 77
5574 deg
Eccentricity:
0011781
Arg of perigee: 347
6079 deg
Mean anomaly: 12
4794 deg
Mean motion: 15
75763564 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 108
Checksum: 321
Coasting Arc #3 (Orbit 122)
---------------------------------------
Vector Time (GMT): 2006/260/08:23:21
283
Vector Time (MET): 007/17:08:26
312
Weight (LBS) : 209988
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4334872
89 A = 6720140
67 meter
Y = 3222397
23 meter E =
0010554
Z = -3995112
53 I = 51
93101
XDOT = -1170
642572 Wp = 26
17016
YDOT = 6491
719669 meter/sec RA = 72
02790 deg
ZDOT = 3979
140784 TA = 284
77438
MA = 284
89130
Ha = 189
924 n
mi
Hp = 180
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14222023
92 X = 4317885
82
Y = 10572169
39 feet Y = 3270828
85 meter
Z = -13107324
56 Z = -3974095
08
XDOT = -3840
690852 XDOT = -1262
553830
YDOT = 21298
292878 feet/sec YDOT = 6478
100397 meter/sec
ZDOT = 13054
923832 ZDOT = 3973
230769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1624240
31 X = 495068
45
Y = -17704700
65 feet Y = -5396392
76 meter
Z = -13028588
01 Z = -3971113
63
XDOT = 18947
282568 XDOT = 5775
131727
YDOT = -7821
007343 feet/sec YDOT = -2383
843038 meter/sec
ZDOT = 13033
791119 ZDOT = 3972
699533
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
SHUTTLE
1 29391U 06036A 06260
35816321
00014500 00000-0 95600-4 0 9020
2 29391 51
6336 72
6583 0011798 350
2054 9
8879 15
75811954 1239
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06260
35816321 = yrday
fracday
Element set: 902
Inclination: 51
6336 deg
RA of node: 72
6583 deg
Eccentricity:
0011798
Arg of perigee: 350
2054 deg
Mean anomaly: 9
8879 deg
Mean motion: 15
75811954 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 123
Checksum: 307
Coasting Arc #4 (Orbit 126)
---------------------------------------
Vector Time (GMT): 2006/260/14:05:00
749
Vector Time (MET): 007/22:50:05
778
Weight (LBS) : 209950
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 668457
21 A = 6722617
06 meter
Y = -5850835
83 meter E =
0010494
Z = -3256359
08 I = 51
93438
XDOT = 5084
620929 Wp = 18
36554
YDOT = 3242
178734 meter/sec RA = 70
85681 deg
ZDOT = -4776
008706 TA = 199
56032
MA = 199
60060
Ha = 189
636 n
mi
Hp = 180
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2193101
07 X = 749720
65
Y = -19195655
61 feet Y = -5842897
89 meter
Z = -10683592
78 Z = -3252914
48
XDOT = 16681
827194 XDOT = 5071
150011
YDOT = 10637
069337 feet/sec YDOT = 3299
023061 meter/sec
ZDOT = -15669
319902 ZDOT = -4751
340495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6674622
49 X = 2034424
94
Y = 18138062
72 feet Y = 5528481
52 meter
Z = -10671557
36 Z = -3252690
68
XDOT = -18443
458912 XDOT = -5621
566276
YDOT = -2388
538169 feet/sec YDOT = -728
026434 meter/sec
ZDOT = -15576
979227 ZDOT = -4747
863268
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
SHUTTLE
1 29391U 06036A 06260
61183391
00014500 00000-0 95600-4 0 9034
2 29391 51
6313 71
3468 0010548 353
0848 7
0169 15
75743495 1276
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06260
61183391 = yrday
fracday
Element set: 903
Inclination: 51
6313 deg
RA of node: 71
3468 deg
Eccentricity:
0010548
Arg of perigee: 353
0848 deg
Mean anomaly: 7
0169 deg
Mean motion: 15
75743495 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 127
Checksum: 298
Coasting Arc #5 (Orbit 126)
---------------------------------------
Vector Time (GMT): 2006/260/14:32:58
693
Vector Time (MET): 007/23:18:03
721
Weight (LBS) : 209926
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3951147
79 A = 6724418
34 meter
Y = 4656621
45 meter E =
0013713
Z = -2798132
12 I = 51
93922
XDOT = -2462
747446 Wp = 9
79909
YDOT = 5175
527861 meter/sec RA = 70
70912 deg
ZDOT = 5152
370050 TA = 318
26045
MA = 318
36499
Ha = 190
183 n
mi
Hp = 180
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12963083
30 X = 3912319
84
Y = 15277629
43 feet Y = 4700635
18 meter
Z = -9180223
50 Z = -2779031
84
XDOT = -8079
880072 XDOT = -2545
528258
YDOT = 16980
078285 feet/sec YDOT = 5147
495263 meter/sec
ZDOT = 16904
101213 ZDOT = 5140
205167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19322913
04 X = -5889623
89
Y = -5420837
18 feet Y = -1652271
17 meter
Z = -9108432
86 Z = -2776250
34
XDOT = -3083
674948 XDOT = -939
904124
YDOT = -17242
665506 feet/sec YDOT = -5255
564446 meter/sec
ZDOT = 16859
487181 ZDOT = 5138
771693
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
SHUTTLE
1 29391U 06036A 06260
61183382
00014500 00000-0 95600-4 0 9045
2 29391 51
6323 71
3471 0011256 351
2115 8
8851 15
75544311 1278
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06260
61183382 = yrday
fracday
Element set: 904
Inclination: 51
6323 deg
RA of node: 71
3471 deg
Eccentricity:
0011256
Arg of perigee: 351
2115 deg
Mean anomaly: 8
8851 deg
Mean motion: 15
75544311 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 127
Checksum: 271
Coasting Arc #6 (Orbit 128)
---------------------------------------
Vector Time (GMT): 2006/260/16:14:54
994
Vector Time (MET): 008/01:00:00
022
Weight (LBS) : 209925
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1549378
42 A = 6727429
09 meter
Y = 6468657
16 meter E =
0021317
Z = 910603
13 I = 51
95021
XDOT = -4858
192767 Wp = 26
25408
YDOT = 316
678024 meter/sec RA = 70
37922 deg
ZDOT = 5982
532287 TA = 343
66396
MA = 343
73257
Ha = 190
164 n
mi
Hp = 180
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5083262
54 X = 1472429
08
Y = 21222628
49 feet Y = 6485570
91 meter
Z = 2987543
07 Z = 917943
16
XDOT = -15938
952649 XDOT = -4890
437751
YDOT = 1038
969894 feet/sec YDOT = 262
112541 meter/sec
ZDOT = 19627
730599 ZDOT = 5958
853087
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20852996
14 X = -6355993
22
Y = -6420484
46 feet Y = -1956963
66 meter
Z = 3015769
02 Z = 919206
40
XDOT = 6791
437599 XDOT = 2070
030180
YDOT = -12827
927218 feet/sec YDOT = -3909
952216 meter/sec
ZDOT = 19539
558906 ZDOT = 5955
657554
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
SHUTTLE
1 29391U 06036A 06260
73868772
00014500 00000-0 95600-4 0 9052
2 29391 51
6338 70
6950 0011347 351
6549 8
4424 15
75544366 1298
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06260
73868772 = yrday
fracday
Element set: 905
Inclination: 51
6338 deg
RA of node: 70
6950 deg
Eccentricity:
0011347
Arg of perigee: 351
6549 deg
Mean anomaly: 8
4424 deg
Mean motion: 15
75544366 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 129
Checksum: 318
Coasting Arc #7 (Orbit 143)
---------------------------------------
Vector Time (GMT): 2006/261/16:15:01
115
Vector Time (MET): 009/01:00:06
143
Weight (LBS) : 209925
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4398418
22 A = 6716487
77 meter
Y = 18044
59 meter E =
0014845
Z = -5084300
96 I = 51
90298
XDOT = 1900
690567 Wp = 55
66587
YDOT = 7265
927321 meter/sec RA = 65
22951 deg
ZDOT = 1681
720599 TA = 230
38901
MA = 230
52015
Ha = 190
265 n
mi
Hp = 180
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14430505
96 X = 4422587
13
Y = 59201
42 feet Y = 67417
82 meter
Z = -16680777
43 Z = -5062874
94
XDOT = 6235
861440 XDOT = 1811
044468
YDOT = 23838
344229 feet/sec YDOT = 7286
702773 meter/sec
ZDOT = 5517
456035 ZDOT = 1690
736311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7209305
30 X = -2197396
26
Y = 12606571
89 feet Y = 3842483
11 meter
Z = -16600951
93 Z = -5059970
15
XDOT = -22880
880895 XDOT = -6974
092497
YDOT = -5824
243208 feet/sec YDOT = -1775
229330 meter/sec
ZDOT = 5552
035331 ZDOT = 1692
260369
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
SHUTTLE
1 29391U 06036A 06261
69008739
00014500 00000-0 95600-4 0 9068
2 29391 51
6337 65
7979 0011371 355
2006 4
9047 15
75597850 1443
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06261
69008739 = yrday
fracday
Element set: 906
Inclination: 51
6337 deg
RA of node: 65
7979 deg
Eccentricity:
0011371
Arg of perigee: 355
2006 deg
Mean anomaly: 4
9047 deg
Mean motion: 15
75597850 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 144
Checksum: 319
Coasting Arc #8 (Orbit 144)
---------------------------------------
Vector Time (GMT): 2006/261/17:19:57
789
Vector Time (MET): 009/02:05:02
817
Weight (LBS) : 209888
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2691677
85 A = 6726885
09 meter
Y = -6164448
27 meter E =
0008192
Z = -209381
52 I = 51
93919
XDOT = 4422
608272 Wp = 61
03060
YDOT = -1731
377871 meter/sec RA = 65
01512 deg
ZDOT = -6053
714819 TA = 121
23406
MA = 121
15376
Ha = 190
232 n
mi
Hp = 179
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8830964
08 X = -2621455
16
Y = -20224567
82 feet Y = -6194187
12 meter
Z = -686947
25 Z = -222286
99
XDOT = 14509
869658 XDOT = 4471
067701
YDOT = -5680
373593 feet/sec YDOT = -1681
597898 meter/sec
ZDOT = -19861
269090 ZDOT = -6032
112274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21709256
57 X = 6616981
40
Y = -3956974
15 feet Y = -1206085
72 meter
Z = -735867
76 Z = -224292
49
XDOT = 1889
947457 XDOT = 576
055985
YDOT = 13948
780817 feet/sec YDOT = 4251
588393 meter/sec
ZDOT = -19781
024491 ZDOT = -6029
256265
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
SHUTTLE
1 29391U 06036A 06261
75350823
00014500 00000-0 95600-4 0 9070
2 29391 51
6329 65
4723 0012570 355
8969 4
2090 15
75850000 1455
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06261
75350823 = yrday
fracday
Element set: 907
Inclination: 51
6329 deg
RA of node: 65
4723 deg
Eccentricity:
0012570
Arg of perigee: 355
8969 deg
Mean anomaly: 4
2090 deg
Mean motion: 15
75850000 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 145
Checksum: 293
Coasting Arc #9 (Orbit 160)
---------------------------------------
Vector Time (GMT): 2006/262/17:20:02
355
Vector Time (MET): 010/02:05:07
383
Weight (LBS) : 209888
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4094276
33 A = 6715021
98 meter
Y = 1087389
47 meter E =
0014948
Z = 5209910
17 I = 51
88718
XDOT = -3137
897831 Wp = 10
67649
YDOT = -6965
800817 meter/sec RA = 59
87260 deg
ZDOT = -997
246691 TA = 88
87766
MA = 88
70641
Ha = 190
396 n
mi
Hp = 179
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13432665
11 X = -4131452
40
Y = 3567550
74 feet Y = 1041348
25 meter
Z = 17092881
12 Z = 5189929
99
XDOT = -10294
940392 XDOT = -3054
844257
YDOT = -22853
677220 feet/sec YDOT = -7000
463066 meter/sec
ZDOT = -3271
806730 ZDOT = -1012
288602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -617452
82 X = -188199
62
Y = -13975577
15 feet Y = -4259755
92 meter
Z = 17018592
50 Z = 5187266
99
XDOT = 23494
146826 XDOT = 7161
015953
YDOT = -5151
143649 feet/sec YDOT = -1570
068584 meter/sec
ZDOT = -3328
797505 ZDOT = -1014
617480
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
SHUTTLE
1 29391U 06036A 06262
76813931
00014500 00000-0 95600-4 0 9087
2 29391 51
6337 60
2455 0012699 359
1094 1
0046 15
75903841 1613
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06262
76813931 = yrday
fracday
Element set: 908
Inclination: 51
6337 deg
RA of node: 60
2455 deg
Eccentricity:
0012699
Arg of perigee: 359
1094 deg
Mean anomaly: 1
0046 deg
Mean motion: 15
75903841 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 161
Checksum: 298
Coasting Arc #10 (Orbit 176)
---------------------------------------
Vector Time (GMT): 2006/263/17:25:19
666
Vector Time (MET): 011/02:10:24
694
Weight (LBS) : 209888
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1040028
34 A = 6722304
78 meter
Y = 5809422
21 meter E =
0019127
Z = 3191757
41 I = 51
89600
XDOT = -5788
933829 Wp = 45
21456
YDOT = -1622
368032 meter/sec RA = 54
75570 deg
ZDOT = 4834
919409 TA = 351
98068
MA = 352
01121
Ha = 190
475 n
mi
Hp = 178
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3412166
47 X = 959415
01
Y = 19059784
16 feet Y = 5820613
68 meter
Z = 10471645
04 Z = 3196613
82
XDOT = -18992
565057 XDOT = -5793
829018
YDOT = -5322
729763 feet/sec YDOT = -1687
199291 meter/sec
ZDOT = 15862
596487 ZDOT = 4806
785045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19352573
04 X = -5898664
26
Y = 16393
95 feet Y = 4996
87 meter
Z = 10490531
44 Z = 3197513
98
XDOT = 8535
487992 XDOT = 2601
616740
YDOT = -16464
361022 feet/sec YDOT = -5018
337240 meter/sec
ZDOT = 15757
559782 ZDOT = 4802
904222
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
SHUTTLE
1 29391U 06036A 06263
78276254
00014500 00000-0 95600-4 0 9092
2 29391 51
6333 55
0198 0012737 3
4929 356
6322 15
75901506 1773
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06263
78276254 = yrday
fracday
Element set: 909
Inclination: 51
6333 deg
RA of node: 55
0198 deg
Eccentricity:
0012737
Arg of perigee: 3
4929 deg
Mean anomaly: 356
6322 deg
Mean motion: 15
75901506 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 177
Checksum: 313
Coasting Arc #11 (Orbit 191)
---------------------------------------
Vector Time (GMT): 2006/264/17:30:16
382
Vector Time (MET): 012/02:15:21
410
Weight (LBS) : 209888
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5304497
21 A = 6724404
42 meter
Y = 3383931
34 meter E =
0017858
Z = -2348100
34 I = 51
88498
XDOT = -1029
633924 Wp = 18
06542
YDOT = 5367
458446 meter/sec RA = 49
55957 deg
ZDOT = 5436
770995 TA = 315
55002
MA = 315
69319
Ha = 190
709 n
mi
Hp = 178
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17403206
06 X = 5277629
01
Y = 11102136
95 feet Y = 3443161
87 meter
Z = -7703741
28 Z = -2322396
49
XDOT = -3378
064055 XDOT = -1116
051741
YDOT = 17609
771806 feet/sec YDOT = 5355
448791 meter/sec
ZDOT = 17837
175180 ZDOT = 5431
558874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13341664
45 X = -4066539
32
Y = 15798805
69 feet Y = 4815475
98 meter
Z = -7607521
54 Z = -2318772
57
XDOT = -15832
150001 XDOT = -4825
639320
YDOT = -4833
828262 feet/sec YDOT = -1473
350854 meter/sec
ZDOT = 17818
490285 ZDOT = 5431
075839
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
SHUTTLE
1 29391U 06036A 06264
73395290
00014500 00000-0 95600-4 0 9102
2 29391 51
6328 50
1207 0012942 6
8371 353
2967 15
75906899 1925
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06264
73395290 = yrday
fracday
Element set: 910
Inclination: 51
6328 deg
RA of node: 50
1207 deg
Eccentricity:
0012942
Arg of perigee: 6
8371 deg
Mean anomaly: 353
2967 deg
Mean motion: 15
75906899 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 192
Checksum: 315
Coasting Arc #12 (Orbit 207)
---------------------------------------
Vector Time (GMT): 2006/265/17:35:15
511
Vector Time (MET): 013/02:20:20
539
Weight (LBS) : 209888
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2950107
57 A = 6714602
31 meter
Y = -2928402
44 meter E =
0021558
Z = -5288039
10 I = 51
83283
XDOT = 5460
107201 Wp = 53
93400
YDOT = 5416
820294 meter/sec RA = 44
42672 deg
ZDOT = 58
965059 TA = 216
55101
MA = 216
69832
Ha = 190
752 n
mi
Hp = 178
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9678830
60 X = 3008357
09
Y = -9607619
54 feet Y = -2895051
77 meter
Z = -17349209
65 Z = -5273565
76
XDOT = 17913
737536 XDOT = 5398
778057
YDOT = 17771
720125 feet/sec YDOT = 5477
600022 meter/sec
ZDOT = 193
454919 ZDOT = 85
341178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8631513
46 X = 2630885
30
Y = 10645997
45 feet Y = 3244900
02 meter
Z = -17295690
33 Z = -5271726
41
XDOT = -18622
582526 XDOT = -5676
163154
YDOT = 15506
582357 feet/sec YDOT = 4726
406302 meter/sec
ZDOT = 292
451417 ZDOT = 89
139192
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
SHUTTLE
1 29391U 06036A 06265
74853442
00014500 00000-0 95600-4 0 9113
2 29391 51
6329 44
8941 0013003 10
8190 349
3252 15
75933610 2086
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06265
74853442 = yrday
fracday
Element set: 911
Inclination: 51
6329 deg
RA of node: 44
8941 deg
Eccentricity:
0013003
Arg of perigee: 10
8190 deg
Mean anomaly: 349
3252 deg
Mean motion: 15
75933610 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 208
Checksum: 287
SPACE SHUTTLE ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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