Date:
September 11th 2006
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 19144
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
253/18:30:22
972 -2
0 6
7 6
7
001/03:15:28
001 -4
9 0
0 181
4
000/00:00:29
497 4
1 0
0 175
0
254/06:36:07
966 -4
8 11
3 11
3
001/15:21:12
994 -6
5 0
0 182
5
000/00:00:17
027 7
9 -0
0 180
5
254/07:10:26
160 0
1 0
1 0
1
001/15:55:31
188 -0
0 -0
0 182
4
000/00:00:00
376 -0
1 -0
0 180
5
254/08:08:15
005 -3
8 9
0 9
0
001/16:53:20
033 -5
7 0
4 187
5
000/00:00:14
067 5
8 0
1 181
3
254/09:25:08
421 -1
2 2
5 2
9
001/18:10:13
449 -0
5 -0
7 188
9
000/00:00:12
899 2
7 1
5 181
3
Coasting Arc #1 (begining on orbit 13)
---------------------------------------
Vector Time (GMT): 2006/253/09:43:32
000
Vector Time (MET): 000/18:28:37
028
Weight (LBS) : 248841
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2773115
38 A = 6701015
75 meter
Y = -3743935
31 meter E =
0013401
Z = 4823158
10 I = 51
92048
XDOT = 3982
227614 Wp = 237
54764
YDOT = -6117
986003 meter/sec RA = 107
67763 deg
ZDOT = -2471
392396 TA = 236
42894
MA = 236
55696
Ha = 181
302 n
mi
Hp = 171
280
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9098147
57 X = -2754421
54
Y = -12283252
33 feet Y = -3774879
80 meter
Z = 15824009
52 Z = 4809731
70
XDOT = 13065
051226 XDOT = 4062
434225
YDOT = -20072
132555 feet/sec YDOT = -6072
949964 meter/sec
ZDOT = -8108
242768 ZDOT = -2451
851701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2337375
57 X = -712432
07
Y = 15158756
70 feet Y = 4620389
04 meter
Z = 15773478
53 Z = 4807756
26
XDOT = -22404
008004 XDOT = -6828
741640
YDOT = 4866
693183 feet/sec YDOT = 1483
368082 meter/sec
ZDOT = -8036
350668 ZDOT = -2449
479684
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 06253
44839792
00014500 00000-0 95600-4 0 9007
2 29391 51
6332 108
2741 0020459 238
1804 121
7371 15
81416434 149
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06253
44839792 = yrday
fracday
Element set: 900
Inclination: 51
6332 deg
RA of node: 108
2741 deg
Eccentricity:
0020459
Arg of perigee: 238
1804 deg
Mean anomaly: 121
7371 deg
Mean motion: 15
81416434 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 14
Checksum: 284
Coasting Arc #2 (begining on orbit 19)
---------------------------------------
Vector Time (GMT): 2006/253/18:30:37
721
Vector Time (MET): 001/03:15:42
749
Weight (LBS) : 248649
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3941187
77 A = 6709819
51 meter
Y = 4278160
52 meter E =
0006964
Z = 3352981
93 I = 51
94074
XDOT = -2198
451726 Wp = 193
49589
YDOT = -5702
927020 meter/sec RA = 105
82426 deg
ZDOT = 4687
708899 TA = 205
86926
MA = 205
90409
Ha = 181
362 n
mi
Hp = 175
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12930406
07 X = -4005081
22
Y = 14035959
72 feet Y = 4233675
30 meter
Z = 11000596
90 Z = 3333680
28
XDOT = -7212
768129 XDOT = -2157
209667
YDOT = -18710
390484 feet/sec YDOT = -5727
311093 meter/sec
ZDOT = 15379
622372 ZDOT = 4677
128970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13236081
02 X = -4034357
49
Y = -13804804
02 feet Y = -4207704
27 meter
Z = 10929329
51 Z = 3331259
64
XDOT = 18105
818492 XDOT = 5518
653476
YDOT = -5203
357499 feet/sec YDOT = -1585
983366 meter/sec
ZDOT = 15339
413955 ZDOT = 4675
453373
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 06253
82760459
00014500 00000-0 95600-4 0 9013
2 29391 51
6327 106
3001 0015908 244
3012 115
6512 15
80170644 209
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06253
82760459 = yrday
fracday
Element set: 901
Inclination: 51
6327 deg
RA of node: 106
3001 deg
Eccentricity:
0015908
Arg of perigee: 244
3012 deg
Mean anomaly: 115
6512 deg
Mean motion: 15
80170644 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 20
Checksum: 260
Coasting Arc #3 (begining on orbit 27)
---------------------------------------
Vector Time (GMT): 2006/254/06:36:16
479
Vector Time (MET): 001/15:21:21
508
Weight (LBS) : 248372
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3241170
92 A = 6718118
79 meter
Y = 5334465
21 meter E =
0006548
Z = 2472312
15 I = 51
95055
XDOT = -3263
384067 Wp = 28
01608
YDOT = -4469
360193 meter/sec RA = 103
22303 deg
ZDOT = 5365
172341 TA = 359
86439
MA = 359
86457
Ha = 182
532 n
mi
Hp = 180
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10633762
86 X = -3312664
84
Y = 17501526
28 feet Y = 5297775
14 meter
Z = 8111260
35 Z = 2456392
79
XDOT = -10706
640639 XDOT = -3239
164870
YDOT = -14663
255227 feet/sec YDOT = -4505
763161 meter/sec
ZDOT = 17602
271459 ZDOT = 5349
377499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17213781
30 X = 5246760
54
Y = 11136072
19 feet Y = 3394274
80 meter
Z = 8052732
99 Z = 2454473
02
XDOT = -14131
173534 XDOT = -4307
181693
YDOT = 9157
843942 feet/sec YDOT = 2791
310834 meter/sec
ZDOT = 17542
821422 ZDOT = 5347
051969
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 06254
33363273
00014500 00000-0 95600-4 0 9024
2 29391 51
6315 103
6821 0010594 282
0722 77
9256 15
78023616 285
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06254
33363273 = yrday
fracday
Element set: 902
Inclination: 51
6315 deg
RA of node: 103
6821 deg
Eccentricity:
0010594
Arg of perigee: 282
0722 deg
Mean anomaly: 77
9256 deg
Mean motion: 15
78023616 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 28
Checksum: 287
Coasting Arc #4 (begining on orbit 27)
---------------------------------------
Vector Time (GMT): 2006/254/07:10:26
348
Vector Time (MET): 001/15:55:31
376
Weight (LBS) : 248370
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 252864
51 A = 6719711
34 meter
Y = -6525400
33 meter E =
0004912
Z = 1570355
72 I = 51
95670
XDOT = 4934
290539 Wp = 152
99903
YDOT = -1203
966878 meter/sec RA = 103
06518 deg
ZDOT = -5794
724047 TA = 9
73061
MA = 9
72110
Ha = 182
418 n
mi
Hp = 180
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 829607
96 X = 318276
12
Y = -21408793
75 feet Y = -6522202
95 meter
Z = 5152085
70 Z = 1571742
99
XDOT = 16188
617253 XDOT = 4975
552711
YDOT = -3950
022567 feet/sec YDOT = -1148
488997 meter/sec
ZDOT = -19011
561833 ZDOT = -5770
652856
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21345212
70 X = -6506020
83
Y = 1833807
45 feet Y = 558944
51 meter
Z = 5156329
23 Z = 1571649
15
XDOT = -5786
935289 XDOT = -1763
857876
YDOT = -14128
305004 feet/sec YDOT = -4306
307365 meter/sec
ZDOT = -18922
093827 ZDOT = -5767
454199
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 06254
33363318
00014500 00000-0 95600-4 0 9035
2 29391 51
6322 103
6825 0010519 281
6381 78
3603 15
78009078 287
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06254
33363318 = yrday
fracday
Element set: 903
Inclination: 51
6322 deg
RA of node: 103
6825 deg
Eccentricity:
0010519
Arg of perigee: 281
6381 deg
Mean anomaly: 78
3603 deg
Mean motion: 15
78009078 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 28
Checksum: 290
Coasting Arc #5 (begining on orbit 28)
---------------------------------------
Vector Time (GMT): 2006/254/08:08:22
039
Vector Time (MET): 001/16:53:27
067
Weight (LBS) : 248150
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3382091
58 A = 6722291
17 meter
Y = 5102315
66 meter E =
0012722
Z = 2757197
84 I = 51
94907
XDOT = -3055
073953 Wp = 32
37380
YDOT = -4824
635212 meter/sec RA = 102
89530 deg
ZDOT = 5180
329627 TA = 359
06064
MA = 359
06303
Ha = 187
541 n
mi
Hp = 181
297
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11096100
99 X = -3452359
78
Y = 16739880
77 feet Y = 5064054
63 meter
Z = 9045924
67 Z = 2740596
86
XDOT = -10023
208508 XDOT = -3025
994640
YDOT = -15828
855683 feet/sec YDOT = -4858
678633 meter/sec
ZDOT = 16995
832109 ZDOT = 5165
558557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19665472
15 X = 5994035
91
Y = 4209267
52 feet Y = 1282984
74 meter
Z = 8984825
56 Z = 2738574
83
XDOT = -10692
900520 XDOT = -3259
196078
YDOT = 13794
582317 feet/sec YDOT = 4204
588690 meter/sec
ZDOT = 16940
144566 ZDOT = 5163
356064
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 06254
39703020
00014500 00000-0 95600-4 0 9040
2 29391 51
6318 103
3549 0010541 321
5415 38
4997 15
76326687 299
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06254
39703020 = yrday
fracday
Element set: 904
Inclination: 51
6318 deg
RA of node: 103
3549 deg
Eccentricity:
0010541
Arg of perigee: 321
5415 deg
Mean anomaly: 38
4997 deg
Mean motion: 15
76326687 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 29
Checksum: 297
Coasting Arc #6 (begining on orbit 28)
---------------------------------------
Vector Time (GMT): 2006/254/09:25:14
870
Vector Time (MET): 001/18:10:19
899
Weight (LBS) : 248066
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 415721
56 A = 6724561
04 meter
Y = 6304825
02 meter E =
0014817
Z = -2272942
36 I = 51
95529
XDOT = -4909
118385 Wp = 348
77150
YDOT = 2297
523021 meter/sec RA = 102
57742 deg
ZDOT = 5483
412438 TA = 345
77268
MA = 345
81436
Ha = 188
899 n
mi
Hp = 181
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1363915
88 X = 356142
80
Y = 20685121
47 feet Y = 6309146
14 meter
Z = -7457159
98 Z = -2271067
43
XDOT = -16106
031446 XDOT = -4961
113686
YDOT = 7537
805188 feet/sec YDOT = 2242
266881 meter/sec
ZDOT = 17990
198286 ZDOT = 5459
437474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14728327
57 X = 4489194
24
Y = -14592060
64 feet Y = -4447660
08 meter
Z = -7449287
54 Z = -2270542
84
XDOT = 15236
641150 XDOT = 4644
128223
YDOT = 6254
180547 feet/sec YDOT = 1906
274231 meter/sec
ZDOT = 17901
242522 ZDOT = 5456
298721
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 06254
39702845
00014500 00000-0 95600-4 0 9055
2 29391 51
6341 103
3544 0012422 325
6739 34
3621 15
75886878 295
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06254
39702845 = yrday
fracday
Element set: 905
Inclination: 51
6341 deg
RA of node: 103
3544 deg
Eccentricity:
0012422
Arg of perigee: 325
6739 deg
Mean anomaly: 34
3621 deg
Mean motion: 15
75886878 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 29
Checksum: 308
Coasting Arc #7 (begining on orbit 44)
---------------------------------------
Vector Time (GMT): 2006/255/09:30:16
169
Vector Time (MET): 002/18:15:21
197
Weight (LBS) : 248066
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4088775
38 A = 6714637
06 meter
Y = 685568
89 meter E =
0013627
Z = -5289085
59 I = 51
92700
XDOT = -1107
694967 Wp = 39
62289
YDOT = 7616
810303 meter/sec RA = 97
44962 deg
ZDOT = 141
436201 TA = 231
65314
MA = 231
77568
Ha = 189
090 n
mi
Hp = 181
107
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13414617
38 X = 4106488
77
Y = 2249241
76 feet Y = 731448
26 meter
Z = -17352643
01 Z = -5269179
12
XDOT = -3634
169839 XDOT = -1193
578083
YDOT = 24989
535114 feet/sec YDOT = 7603
927181 meter/sec
ZDOT = 464
029532 ZDOT = 135
846626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7587113
21 X = -2312552
11
Y = -11402517
22 feet Y = -3475487
25 meter
Z = -17278413
74 Z = -5266460
51
XDOT = 19901
667418 XDOT = 6066
028229
YDOT = -13863
340531 feet/sec YDOT = -4225
546194 meter/sec
ZDOT = 444
277256 ZDOT = 135
415708
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 06255
41164368
00014500 00000-0 95600-4 0 9062
2 29391 51
6341 98
1282 0012518 329
4220 30
6213 15
75919908 453
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06255
41164368 = yrday
fracday
Element set: 906
Inclination: 51
6341 deg
RA of node: 98
1282 deg
Eccentricity:
0012518
Arg of perigee: 329
4220 deg
Mean anomaly: 30
6213 deg
Mean motion: 15
75919908 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 45
Checksum: 293
Coasting Arc #8 (begining on orbit 60)
---------------------------------------
Vector Time (GMT): 2006/256/09:35:00
161
Vector Time (MET): 003/18:20:05
189
Weight (LBS) : 248066
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2131529
04 A = 6724227
25 meter
Y = -5906538
60 meter E =
0007507
Z = -2415776
18 I = 51
96176
XDOT = 4073
006114 Wp = 346
29174
YDOT = 3679
762440 meter/sec RA = 92
32644 deg
ZDOT = -5392
678283 TA = 220
83062
MA = 220
88689
Ha = 189
181 n
mi
Hp = 180
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6993205
52 X = 2209235
93
Y = -19378407
48 feet Y = -5882237
76 meter
Z = -7925774
87 Z = -2405232
71
XDOT = 13362
880951 XDOT = 4057
700574
YDOT = 12072
711417 feet/sec YDOT = 3725
280497 meter/sec
ZDOT = -17692
514053 ZDOT = -5372
928508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18637799
02 X = -5680801
14
Y = 8812949
24 feet Y = 2686186
93 meter
Z = -7887324
05 Z = -2404056
37
XDOT = -421
686002 XDOT = -128
529893
YDOT = -16690
824529 feet/sec YDOT = -5087
363317 meter/sec
ZDOT = -17618
450095 ZDOT = -5370
103589
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 06256
42624102
00014500 00000-0 95600-4 0 9072
2 29391 51
6343 92
9023 0012531 332
4331 27
6168 15
75910147 611
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06256
42624102 = yrday
fracday
Element set: 907
Inclination: 51
6343 deg
RA of node: 92
9023 deg
Eccentricity:
0012531
Arg of perigee: 332
4331 deg
Mean anomaly: 27
6168 deg
Mean motion: 15
75910147 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 61
Checksum: 271
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
http://www aus-city com/cgi-bin/dada/mail cgi/u/[list]/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
http://www aus-city com/cgi-bin/dada/mail cgi/list/[list]
If you're still having trouble, please contact the list owner at:
<mailto:list
admin@aus-city
com>
The following physical address is associated with this mailing list:
http://www aus-city com
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
Shuttle TLE list
Privacy Policy:
Private list