SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2006/344/01:47:34 973 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 12 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 06121
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
352/22:41:38
141 1
1 -0
0 1
5
008/20:54:03
168 -0
0 -0
0 193
5
000/00:00:06
336 1
0 -1
5 175
9
352/23:09:34
964 5
8 -10
0 10
0
008/21:21:59
991 2
7 -0
0 193
4
000/00:00:14
743 7
6 0
0 170
4
352/23:52:34
954 -8
7 -12
7 12
7
008/22:04:59
981 -1
5 0
0 186
7
000/00:00:18
139 -9
1 -0
0 169
8
354/18:29:45
995 0
9 2
0 2
0
010/16:42:11
022 0
9 -0
0 188
1
000/00:00:08
428 1
6 0
0 169
1
Coasting Arc #1 (Orbit 76)
---------------------------------------
Vector Time (GMT): 2006/348/21:00:48
000
Vector Time (MET): 004/19:13:13
027
Weight (LBS) : 238337
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5716411
25 A = 6726538
64 meter
Y = -3390962
65 meter E =
0030341
Z = -892545
59 I = 51
52112
XDOT = 3159
950681 Wp = 353
48611
YDOT = 3761
739026 meter/sec RA = 335
45091 deg
ZDOT = 5956
679860 TA = 356
72526
MA = 356
74507
Ha = 193
183 n
mi
Hp = 177
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18754630
09 X = 5758255
34
Y = -11125205
55 feet Y = -3326778
91 meter
Z = -2928299
19 Z = -864673
66
XDOT = 10367
292262 XDOT = 3088
697778
YDOT = 12341
663471 feet/sec YDOT = 3796
690259 meter/sec
ZDOT = 19542
912927 ZDOT = 5971
858411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7991805
76 X = 2435902
39
Y = -20303565
60 feet Y = -6188526
79 meter
Z = -2824455
60 Z = -860894
07
XDOT = 14193
380419 XDOT = 4326
142352
YDOT = 2864
886990 feet/sec YDOT = 873
217555 meter/sec
ZDOT = 19600
104912 ZDOT = 5974
111977
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 29647U 06055A 06348
87721122
00014500 00000-0 95600-4 0 9001
2 29647 51
6346 335
9517 0024212 336
4624 23
5430 15
75874037 775
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06348
87721122 = yrday
fracday
Element set: 900
Inclination: 51
6346 deg
RA of node: 335
9517 deg
Eccentricity:
0024212
Arg of perigee: 336
4624 deg
Mean anomaly: 23
5430 deg
Mean motion: 15
75874037 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 77
Checksum: 303
Coasting Arc #2 (Orbit 92)
---------------------------------------
Vector Time (GMT): 2006/349/21:05:55
363
Vector Time (MET): 005/19:18:20
390
Weight (LBS) : 238337
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -244366
25 A = 6715659
97 meter
Y = -4460037
86 meter E =
0020040
Z = -5013611
99 I = 51
45841
XDOT = 7096
723320 Wp = 13
59479
YDOT = -2396
409415 meter/sec RA = 330
26416 deg
ZDOT = 1806
547213 TA = 273
73380
MA = 273
96293
Ha = 193
208 n
mi
Hp = 176
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -801726
56 X = -170099
85
Y = -14632670
13 feet Y = -4462355
56 meter
Z = -16448858
24 Z = -5014619
29
XDOT = 23283
212993 XDOT = 7114
227197
YDOT = -7862
235613 feet/sec YDOT = -2316
920558 meter/sec
ZDOT = 5926
992169 ZDOT = 1841
065812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9974268
53 X = -3040157
05
Y = -10729916
76 feet Y = -3270478
63 meter
Z = -16453133
19 Z = -5014915
00
XDOT = 11926
936132 XDOT = 3635
330133
YDOT = -20269
117076 feet/sec YDOT = -6178
026885 meter/sec
ZDOT = 6055
807006 ZDOT = 1845
809976
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 29647U 06055A 06349
89181310
00014500 00000-0 95600-4 0 9014
2 29647 51
6333 330
7248 0024024 340
3365 19
6870 15
75945640 933
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06349
89181310 = yrday
fracday
Element set: 901
Inclination: 51
6333 deg
RA of node: 330
7248 deg
Eccentricity:
0024024
Arg of perigee: 340
3365 deg
Mean anomaly: 19
6870 deg
Mean motion: 15
75945640 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 93
Checksum: 304
Coasting Arc #3 (Orbit 108)
---------------------------------------
Vector Time (GMT): 2006/350/21:06:04
642
Vector Time (MET): 006/19:18:29
669
Weight (LBS) : 238337
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6020813
57 A = 6724260
25 meter
Y = 2002485
31 meter E =
0019036
Z = -2258208
56 I = 51
46338
XDOT = 237
473626 Wp = 352
12797
YDOT = -5436
129697 meter/sec RA = 325
13601 deg
ZDOT = -5429
713712 TA = 213
25413
MA = 213
37389
Ha = 193
382 n
mi
Hp = 176
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19753325
37 X = -6031796
66
Y = 6569833
70 feet Y = 1935069
25 meter
Z = -7408820
73 Z = -2287484
51
XDOT = 779
112945 XDOT = 324
644750
YDOT = -17835
071183 feet/sec YDOT = -5432
984701 meter/sec
ZDOT = -17814
021364 ZDOT = -5428
349088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10518522
28 X = -3206045
59
Y = 17918883
79 feet Y = 5461675
78 meter
Z = -7518077
90 Z = -2291510
14
XDOT = -9769
315737 XDOT = -2977
687437
YDOT = -13239
377503 feet/sec YDOT = -4035
362263 meter/sec
ZDOT = -17809
534709 ZDOT = -5428
346179
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 29647U 06055A 06350
90638534
00014500 00000-0 95600-4 0 9024
2 29647 51
6328 325
4989 0024008 344
1966 15
8447 15
75979742 1097
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06350
90638534 = yrday
fracday
Element set: 902
Inclination: 51
6328 deg
RA of node: 325
4989 deg
Eccentricity:
0024008
Arg of perigee: 344
1966 deg
Mean anomaly: 15
8447 deg
Mean motion: 15
75979742 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 109
Checksum: 338
Coasting Arc #4 (Orbit 124)
---------------------------------------
Vector Time (GMT): 2006/351/21:10:31
211
Vector Time (MET): 007/19:22:56
238
Weight (LBS) : 238337
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2271613
44 A = 6721523
63 meter
Y = 5387347
17 meter E =
0024399
Z = 3333905
11 I = 51
43220
XDOT = -6121
748457 Wp = 17
68574
YDOT = 312
627991 meter/sec RA = 319
90724 deg
ZDOT = -4644
531465 TA = 123
00232
MA = 122
76761
Ha = 193
448 n
mi
Hp = 176
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7452800
00 X = -2347906
34
Y = 17675023
53 feet Y = 5361507
29 meter
Z = 10938008
90 Z = 3322685
04
XDOT = -20084
476564 XDOT = -6102
227802
YDOT = 1025
682386 feet/sec YDOT = 244
253845 meter/sec
ZDOT = -15237
964124 ZDOT = -4674
223878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6639142
85 X = 2023610
74
Y = 18021525
88 feet Y = 5492961
09 meter
Z = 10896655
93 Z = 3321300
73
XDOT = -12549
450944 XDOT = -3825
072648
YDOT = 13967
277705 feet/sec YDOT = 4257
226245 meter/sec
ZDOT = -15348
974967 ZDOT = -4678
367570
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 29647U 06055A 06351
92092599
00014500 00000-0 95600-4 0 9033
2 29647 51
6330 320
2707 0024020 347
7212 12
3364 15
76062564 1252
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06351
92092599 = yrday
fracday
Element set: 903
Inclination: 51
6330 deg
RA of node: 320
2707 deg
Eccentricity:
0024020
Arg of perigee: 347
7212 deg
Mean anomaly: 12
3364 deg
Mean motion: 15
76062564 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 125
Checksum: 282
Coasting Arc #5 (Orbit 140)
---------------------------------------
Vector Time (GMT): 2006/352/21:15:15
662
Vector Time (MET): 008/19:27:40
689
Weight (LBS) : 238337
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3957296
25 A = 6714896
07 meter
Y = 1806351
39 meter E =
0021079
Z = 5111018
95 I = 51
38756
XDOT = -4514
984178 Wp =
38884
YDOT = 6097
542016 meter/sec RA = 314
75846 deg
ZDOT = 1361
546286 TA = 76
66397
MA = 76
42902
Ha = 193
550 n
mi
Hp = 176
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12983255
42 X = 3911966
32
Y = 5926349
71 feet Y = 1850367
23 meter
Z = 16768434
89 Z = 5130133
95
XDOT = -14812
940218 XDOT = -4589
473387
YDOT = 20005
059108 feet/sec YDOT = 6046
615897 meter/sec
ZDOT = 4467
015375 ZDOT = 1339
432446
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13268132
17 X = 4044126
69
Y = -5023307
61 feet Y = -1531104
16 meter
Z = 16840130
65 Z = 5132871
82
XDOT = 3471
348799 XDOT = 1058
067114
YDOT = 23641
902579 feet/sec YDOT = 7206
051906 meter/sec
ZDOT = 4384
994529 ZDOT = 1336
546333
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 29647U 06055A 06352
93544118
00014500 00000-0 95600-4 0 9045
2 29647 51
6320 315
0427 0023796 352
3140 7
7656 15
76027364 1412
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06352
93544118 = yrday
fracday
Element set: 904
Inclination: 51
6320 deg
RA of node: 315
0427 deg
Eccentricity:
0023796
Arg of perigee: 352
3140 deg
Mean anomaly: 7
7656 deg
Mean motion: 15
76027364 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 141
Checksum: 294
Coasting Arc #6 (Orbit 141)
---------------------------------------
Vector Time (GMT): 2006/352/22:41:41
309
Vector Time (MET): 008/20:54:06
336
Weight (LBS) : 238295
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5032866
44 A = 6717515
24 meter
Y = -74908
49 meter E =
0020893
Z = 4433470
17 I = 51
39540
XDOT = -2728
648451 Wp = 13
00224
YDOT = 6455
683394 meter/sec RA = 314
45862 deg
ZDOT = 3223
776630 TA = 44
75566
MA = 44
58727
Ha = 193
471 n
mi
Hp = 175
911
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16512028
99 X = 5011792
87
Y = -245762
76 feet Y = -18724
43 meter
Z = 14545505
82 Z = 4457868
91
XDOT = -8952
258696 XDOT = -2816
323373
YDOT = 21180
063627 feet/sec YDOT = 6424
666938 meter/sec
ZDOT = 10576
694979 ZDOT = 3210
308956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6169092
06 X = 1880339
26
Y = -15231120
91 feet Y = -4642445
65 meter
Z = 14636751
66 Z = 4461281
91
XDOT = 14891
823439 XDOT = 4539
027784
YDOT = 16094
200958 feet/sec YDOT = 4905
512452 meter/sec
ZDOT = 10527
051814 ZDOT = 3208
645393
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 29647U 06055A 06352
99884647
00014500 00000-0 95600-4 0 9056
2 29647 51
6315 314
7142 0024020 351
7896 8
2872 15
76091124 1420
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06352
99884647 = yrday
fracday
Element set: 905
Inclination: 51
6315 deg
RA of node: 314
7142 deg
Eccentricity:
0024020
Arg of perigee: 351
7896 deg
Mean anomaly: 8
2872 deg
Mean motion: 15
76091124 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 142
Checksum: 313
Coasting Arc #7 (Orbit 141)
---------------------------------------
Vector Time (GMT): 2006/352/23:09:42
336
Vector Time (MET): 008/21:22:07
363
Weight (LBS) : 238062
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3989242
90 A = 6720376
23 meter
Y = 5318122
95 meter E =
0024808
Z = 1080649
24 I = 51
42271
XDOT = -4461
994158 Wp = 14
54954
YDOT = -2141
840651 meter/sec RA = 314
32419 deg
ZDOT = -5878
137386 TA = 153
60725
MA = 153
48067
Ha = 193
445 n
mi
Hp = 170
399
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13088067
27 X = -4053687
60
Y = 17447909
93 feet Y = 5273134
54 meter
Z = 3545437
15 Z = 1061113
75
XDOT = -14639
088444 XDOT = -4409
147154
YDOT = -7027
036257 feet/sec YDOT = -2191
460351 meter/sec
ZDOT = -19285
227643 ZDOT = -5899
686031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13194516
90 X = 4021688
75
Y = 17382185
85 feet Y = 5298090
25 meter
Z = 3472971
29 Z = 1058561
65
XDOT = -9468
225436 XDOT = -2885
915113
YDOT = 11091
939840 feet/sec YDOT = 3380
823263 meter/sec
ZDOT = -19366
063698 ZDOT = -5902
776215
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 29647U 06055A 06352
99880267
00014500 00000-0 95600-4 0 9061
2 29647 51
6316 314
7139 0032042 350
8737 9
1842 15
77976846 1425
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06352
99880267 = yrday
fracday
Element set: 906
Inclination: 51
6316 deg
RA of node: 314
7139 deg
Eccentricity:
0032042
Arg of perigee: 350
8737 deg
Mean anomaly: 9
1842 deg
Mean motion: 15
77976846 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 142
Checksum: 333
Coasting Arc #8 (Orbit 141)
---------------------------------------
Vector Time (GMT): 2006/352/23:52:44
023
Vector Time (MET): 008/22:05:09
050
Weight (LBS) : 237764
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3181522
69 A = 6712550
69 meter
Y = -5548070
51 meter E =
0027585
Z = -1984279
38 I = 51
41987
XDOT = 5232
891804 Wp = 6
49316
YDOT = 1013
503873 meter/sec RA = 314
16162 deg
ZDOT = 5590
986332 TA = 331
23143
MA = 331
38329
Ha = 186
671 n
mi
Hp = 169
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10438066
57 X = 3252989
51
Y = -18202331
06 feet Y = -5512078
63 meter
Z = -6510102
97 Z = -1968650
83
XDOT = 17168
280198 XDOT = 5194
004668
YDOT = 3325
143939 feet/sec YDOT = 1071
825754 meter/sec
ZDOT = 18343
131011 ZDOT = 5616
313734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17199838
47 X = -5242510
77
Y = -12049615
34 feet Y = -3672722
76 meter
Z = -6452275
33 Z = -1966653
52
XDOT = 3949
376259 XDOT = 1203
769884
YDOT = -15449
299973 feet/sec YDOT = -4708
946632 meter/sec
ZDOT = 18437
973124 ZDOT = 5619
894208
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 29647U 06055A 06352
99880607
00014500 00000-0 95600-4 0 9070
2 29647 51
6334 314
7141 0022119 357
1657 2
9380 15
80320812 1421
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06352
99880607 = yrday
fracday
Element set: 907
Inclination: 51
6334 deg
RA of node: 314
7141 deg
Eccentricity:
0022119
Arg of perigee: 357
1657 deg
Mean anomaly: 2
9380 deg
Mean motion: 15
80320812 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 142
Checksum: 298
Coasting Arc #9 (Orbit 157)
---------------------------------------
Vector Time (GMT): 2006/353/23:55:08
171
Vector Time (MET): 009/22:07:33
198
Weight (LBS) : 237764
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2455376
73 A = 6702406
31 meter
Y = -3519546
54 meter E =
0024819
Z = -5157873
00 I = 51
36726
XDOT = 5437
789740 Wp = 36
27742
YDOT = -5347
903244 meter/sec RA = 308
96132 deg
ZDOT = 1082
957827 TA = 243
96236
MA = 244
21811
Ha = 186
706 n
mi
Hp = 169
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8055697
94 X = -2390766
19
Y = -11547068
70 feet Y = -3546652
44 meter
Z = -16922155
53 Z = -5169645
07
XDOT = 17840
517520 XDOT = 5491
949345
YDOT = -17545
614318 feet/sec YDOT = -5286
767870 meter/sec
ZDOT = 3553
011244 ZDOT = 1109
505249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12012626
77 X = -3661448
64
Y = 7240180
05 feet Y = 2206806
88 meter
Z = -16966584
91 Z = -5171415
08
XDOT = -15894
096588 XDOT = -4844
520640
YDOT = -17985
031615 feet/sec YDOT = -5481
837636 meter/sec
ZDOT = 3651
707075 ZDOT = 1113
040317
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 29647U 06055A 06354
01056251
00014500 00000-0 95600-4 0 9086
2 29647 51
6337 309
4696 0022084 1
2377 358
8840 15
80367696 1589
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06354
01056251 = yrday
fracday
Element set: 908
Inclination: 51
6337 deg
RA of node: 309
4696 deg
Eccentricity:
0022084
Arg of perigee: 1
2377 deg
Mean anomaly: 358
8840 deg
Mean motion: 15
80367696 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 158
Checksum: 322
Coasting Arc #10 (Orbit 170)
---------------------------------------
Vector Time (GMT): 2006/354/18:29:50
209
Vector Time (MET): 010/16:42:15
236
Weight (LBS) : 237709
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4249202
67 A = 6714938
01 meter
Y = -5124581
00 meter E =
0034660
Z = 684868
27 I = 51
39397
XDOT = 3335
732870 Wp = 20
36229
YDOT = 3574
000800 meter/sec RA = 304
95305 deg
ZDOT = 5988
516045 TA = 347
16265
MA = 347
25068
Ha = 188
111 n
mi
Hp = 169
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13940953
65 X = 4302886
33
Y = -16812929
79 feet Y = -5076744
96 meter
Z = 2246943
14 Z = 705640
28
XDOT = 10944
005479 XDOT = 3266
412690
YDOT = 11725
724410 feet/sec YDOT = 3610
928732 meter/sec
ZDOT = 19647
362354 ZDOT = 6004
553419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12117004
50 X = 3693262
97
Y = -18161786
05 feet Y = -5535712
39 meter
Z = 2324065
40 Z = 708375
13
XDOT = 10663
890066 XDOT = 3250
353692
YDOT = 9660
058875 feet/sec YDOT = 2944
385945 meter/sec
ZDOT = 19707
757130 ZDOT = 6006
924373
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 29647U 06055A 06354
83261455
00014500 00000-0 95600-4 0 9091
2 29647 51
6348 305
2107 0024279 3
8239 356
3109 15
80007614 1712
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06354
83261455 = yrday
fracday
Element set: 909
Inclination: 51
6348 deg
RA of node: 305
2107 deg
Eccentricity:
0024279
Arg of perigee: 3
8239 deg
Mean anomaly: 356
3109 deg
Mean motion: 15
80007614 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 171
Checksum: 300
Coasting Arc #11 (Orbit 185)
---------------------------------------
Vector Time (GMT): 2006/355/18:32:51
109
Vector Time (MET): 011/16:45:16
136
Weight (LBS) : 237709
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -551110
15 A = 6708247
24 meter
Y = -5393907
54 meter E =
0023983
Z = -3941782
45 I = 51
35522
XDOT = 5633
380294 Wp = 23
76629
YDOT = -3458
992630 meter/sec RA = 299
70728 deg
ZDOT = 3975
647110 TA = 287
39288
MA = 287
65500
Ha = 188
237 n
mi
Hp = 168
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1808104
17 X = -471581
28
Y = -17696547
06 feet Y = -5399627
19 meter
Z = -12932357
11 Z = -3944267
63
XDOT = 18482
218811 XDOT = 5652
342815
YDOT = -11348
401018 feet/sec YDOT = -3395
866630 meter/sec
ZDOT = 13043
461646 ZDOT = 4003
059333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4082975
30 X = -1244490
87
Y = -17306353
80 feet Y = -5274976
64 meter
Z = -12942268
34 Z = -3944803
39
XDOT = 15468
148422 XDOT = 4714
691639
YDOT = -13406
475793 feet/sec YDOT = -4086
293822 meter/sec
ZDOT = 13145
617823 ZDOT = 4006
784312
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 29647U 06055A 06355
78133602
00014500 00000-0 95600-4 0 9100
2 29647 51
6339 300
2939 0024232 7
4120 352
7400 15
80023694 1864
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06355
78133602 = yrday
fracday
Element set: 910
Inclination: 51
6339 deg
RA of node: 300
2939 deg
Eccentricity:
0024232
Arg of perigee: 7
4120 deg
Mean anomaly: 352
7400 deg
Mean motion: 15
80023694 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 186
Checksum: 281
Coasting Arc #12 (Orbit 201)
---------------------------------------
Vector Time (GMT): 2006/356/18:35:20
396
Vector Time (MET): 012/16:47:45
423
Weight (LBS) : 237709
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4466840
61 A = 6703900
42 meter
Y = 109526
77 meter E =
0032215
Z = -5020058
77 I = 51
32655
XDOT = 1794
897118 Wp = 33
60397
YDOT = -7275
494102 meter/sec RA = 294
53590 deg
ZDOT = -1734
684505 TA = 219
48822
MA = 219
72342
Ha = 188
320 n
mi
Hp = 168
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14654988
88 X = -4443347
32
Y = 359339
80 feet Y = 59688
47 meter
Z = -16470009
08 Z = -5041701
40
XDOT = 5888
770073 XDOT = 1884
578397
YDOT = -23869
731307 feet/sec YDOT = -7254
912606 meter/sec
ZDOT = -5691
222130 ZDOT = -1725
748468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14314923
77 X = -4363188
77
Y = 2703219
17 feet Y = 823941
20 meter
Z = -16550969
35 Z = -5044735
46
XDOT = 2190
650007 XDOT = 667
710122
YDOT = -23468
125897 feet/sec YDOT = -7153
084773 meter/sec
ZDOT = -5658
626366 ZDOT = -1724
749316
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 29647U 06055A 06356
79328495
00014500 00000-0 95600-4 0 9119
2 29647 51
6326 295
0494 0024191 11
3909 348
7800 15
80058827 2024
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06356
79328495 = yrday
fracday
Element set: 911
Inclination: 51
6326 deg
RA of node: 295
0494 deg
Eccentricity:
0024191
Arg of perigee: 11
3909 deg
Mean anomaly: 348
7800 deg
Mean motion: 15
80058827 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 202
Checksum: 320
Coasting Arc #13 (Orbit 217)
---------------------------------------
Vector Time (GMT): 2006/357/18:37:58
883
Vector Time (MET): 013/16:50:23
910
Weight (LBS) : 237709
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3233898
97 A = 6713886
59 meter
Y = 5717217
09 meter E =
0020165
Z = -1450587
67 I = 51
35002
XDOT = -3656
137318 Wp = 34
44788
YDOT = -3527
184188 meter/sec RA = 289
32191 deg
ZDOT = -5773
606102 TA = 161
58106
MA = 161
50795
Ha = 188
406 n
mi
Hp = 168
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10609904
75 X = -3290568
09
Y = 18757273
93 feet Y = 5680722
66 meter
Z = -4759145
90 Z = -1466434
51
XDOT = -11995
201176 XDOT = -3588
361400
YDOT = -11572
126600 feet/sec YDOT = -3567
705444 meter/sec
ZDOT = -18942
277238 ZDOT = -5791
203341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6835609
32 X = -2083493
72
Y = 20423476
37 feet Y = 6225075
60 meter
Z = -4817772
50 Z = -1468457
06
XDOT = -12378
851514 XDOT = -3773
073941
YDOT = -8609
715233 feet/sec YDOT = -2624
241203 meter/sec
ZDOT = -19008
530872 ZDOT = -5793
800210
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 29647U 06055A 06357
80520676
00014500 00000-0 95600-4 0 9128
2 29647 51
6325 289
8049 0024200 15
2996 344
8897 15
80109521 2188
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06357
80520676 = yrday
fracday
Element set: 912
Inclination: 51
6325 deg
RA of node: 289
8049 deg
Eccentricity:
0024200
Arg of perigee: 15
2996 deg
Mean anomaly: 344
8897 deg
Mean motion: 15
80109521 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 218
Checksum: 323
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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