Date:
December 16th 2006
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
352/22:41:41
292 2
3 -0
0 3
0
008/20:54:06
319 -0
1 -0
0 193
7
000/00:00:12
638 2
0 -3
0 176
0
352/23:09:42
385 5
9 -10
0 10
0
008/21:22:07
412 2
7 -0
0 193
7
000/00:00:14
823 7
6 0
0 170
5
352/23:59:39
495 -5
0 -12
7 12
7
008/22:12:04
522 -6
2 -0
0 186
3
000/00:00:17
947 -9
9 0
0 170
6
354/18:29:14
236 0
9 2
0 2
0
010/16:41:39
263 0
8 -0
0 187
9
000/00:00:08
404 1
6 0
0 169
9
Coasting Arc #1 (Orbit 92)
---------------------------------------
Vector Time (GMT): 2006/349/20:26:42
999
Vector Time (MET): 005/18:39:08
026
Weight (LBS) : 237695
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2521141
48 A = 6720511
93 meter
Y = 4932422
51 meter E =
0024342
Z = 3822494
10 I = 51
47721
XDOT = -6486
850663 Wp = 6
76189
YDOT = -95
073569 meter/sec RA = 330
39521 deg
ZDOT = -4129
280941 TA = 126
68999
MA = 126
46607
Ha = 193
323 n
mi
Hp = 176
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8271461
54 X = -2594700
27
Y = 16182488
54 feet Y = 4903806
53 meter
Z = 12540991
13 Z = 3810068
14
XDOT = -21282
318449 XDOT = -6465
245089
YDOT = -311
921157 feet/sec YDOT = -167
520727 meter/sec
ZDOT = -13547
509649 ZDOT = -4160
742043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 963425
99 X = 293652
24
Y = 18179965
68 feet Y = 5541253
54 meter
Z = 12495084
15 Z = 3808501
65
XDOT = -17141
419979 XDOT = -5224
704810
YDOT = 10360
361185 feet/sec YDOT = 3157
838089 meter/sec
ZDOT = -13665
174202 ZDOT = -4165
145097
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
89176985
00014500 00000-0 95600-4 0 9005
2 29647 51
6357 330
7266 0024074 339
7737 20
2472 15
75888610 938
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06349
89176985 = yrday
fracday
Element set: 900
Inclination: 51
6357 deg
RA of node: 330
7266 deg
Eccentricity:
0024074
Arg of perigee: 339
7737 deg
Mean anomaly: 20
2472 deg
Mean motion: 15
75888610 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 93
Checksum: 340
Coasting Arc #2 (Orbit 108)
---------------------------------------
Vector Time (GMT): 2006/350/20:31:32
930
Vector Time (MET): 006/18:43:57
957
Weight (LBS) : 237695
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4165795
00 A = 6716251
01 meter
Y = 1880585
94 meter E =
0019593
Z = 4916263
58 I = 51
43728
XDOT = -4964
224050 Wp = 355
12385
YDOT = 5501
458319 meter/sec RA = 325
25733 deg
ZDOT = 2121
845213 TA = 74
37109
MA = 74
15496
Ha = 193
442 n
mi
Hp = 176
769
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13667306
43 X = 4120565
14
Y = 6169901
38 feet Y = 1926935
07 meter
Z = 16129473
68 Z = 4936391
72
XDOT = -16286
824310 XDOT = -5035
705172
YDOT = 18049
403934 feet/sec YDOT = 5445
523321 meter/sec
ZDOT = 6961
434427 ZDOT = 2097
555802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14766472
59 X = 4500820
84
Y = -2091266
77 feet Y = -637418
11 meter
Z = 16204960
97 Z = 4939272
10
XDOT = -4223
861225 XDOT = -1287
432901
YDOT = 22917
242217 feet/sec YDOT = 6985
175428 meter/sec
ZDOT = 6871
222668 ZDOT = 2094
348669
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
90640473
00014500 00000-0 95600-4 0 9018
2 29647 51
6345 325
4996 0023880 344
0204 16
0204 15
75851294 1090
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06350
90640473 = yrday
fracday
Element set: 901
Inclination: 51
6345 deg
RA of node: 325
4996 deg
Eccentricity:
0023880
Arg of perigee: 344
0204 deg
Mean anomaly: 16
0204 deg
Mean motion: 15
75851294 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 109
Checksum: 295
Coasting Arc #3 (Orbit 124)
---------------------------------------
Vector Time (GMT): 2006/351/20:36:17
942
Vector Time (MET): 007/18:48:42
969
Weight (LBS) : 237695
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5359454
07 A = 6726619
66 meter
Y = -4002120
46 meter E =
0032032
Z = 466662
67 I = 51
44906
XDOT = 2549
183314 Wp = 8
44314
YDOT = 4117
568540 meter/sec RA = 320
06272 deg
ZDOT = 6015
371496 TA = 356
66259
MA = 356
68390
Ha = 193
507 n
mi
Hp = 176
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17583510
74 X = 5401558
61
Y = -13130316
47 feet Y = -3941928
72 meter
Z = 1531045
51 Z = 492800
88
XDOT = 8363
462315 XDOT = 2473
710123
YDOT = 13509
083135 feet/sec YDOT = 4145
663139 meter/sec
ZDOT = 19735
470786 ZDOT = 6027
572964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6983417
78 X = 2128545
74
Y = -20796863
29 feet Y = -6338883
93 meter
Z = 1628346
98 Z = 496320
16
XDOT = 12956
988721 XDOT = 3949
290162
YDOT = 5904
684955 feet/sec YDOT = 1799
747974 meter/sec
ZDOT = 19781
568137 ZDOT = 6029
421968
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
92100615
00014500 00000-0 95600-4 0 9021
2 29647 51
6335 320
2728 0023818 347
5942 12
4633 15
75924468 1251
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06351
92100615 = yrday
fracday
Element set: 902
Inclination: 51
6335 deg
RA of node: 320
2728 deg
Eccentricity:
0023818
Arg of perigee: 347
5942 deg
Mean anomaly: 12
4633 deg
Mean motion: 15
75924468 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 125
Checksum: 299
Coasting Arc #4 (Orbit 139)
---------------------------------------
Vector Time (GMT): 2006/352/20:41:21
830
Vector Time (MET): 008/18:53:46
857
Weight (LBS) : 237695
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4595
69 A = 6717919
63 meter
Y = -5033691
71 meter E =
0020690
Z = -4442581
96 I = 51
39828
XDOT = 6416
374970 Wp = 14
85445
YDOT = -2811
141865 meter/sec RA = 314
84866 deg
ZDOT = 3214
814304 TA = 287
28892
MA = 287
51520
Ha = 193
577 n
mi
Hp = 176
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15077
73 X = 82486
76
Y = -16514736
57 feet Y = -5033203
78 meter
Z = -14575400
14 Z = -4442371
38
XDOT = 21051
098984 XDOT = 6431
727736
YDOT = -9222
906380 feet/sec YDOT = -2739
276488 meter/sec
ZDOT = 10547
291024 ZDOT = 3246
022181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9846001
85 X = -3001061
36
Y = -13258937
28 feet Y = -4041324
08 meter
Z = -14575179
94 Z = -4442514
85
XDOT = 10272
365230 XDOT = 3131
016922
YDOT = -19267
553400 feet/sec YDOT = -5872
750276 meter/sec
ZDOT = 10663
694754 ZDOT = 3250
294161
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
87216854
00014500 00000-0 95600-4 0 9030
2 29647 51
6326 315
3722 0023636 351
2932 8
7819 15
75979339 1407
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06352
87216854 = yrday
fracday
Element set: 903
Inclination: 51
6326 deg
RA of node: 315
3722 deg
Eccentricity:
0023636
Arg of perigee: 351
2932 deg
Mean anomaly: 8
7819 deg
Mean motion: 15
75979339 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 140
Checksum: 324
Coasting Arc #5 (Orbit 141)
---------------------------------------
Vector Time (GMT): 2006/352/22:41:47
611
Vector Time (MET): 008/20:54:12
638
Weight (LBS) : 237612
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5048898
67 A = 6717854
72 meter
Y = -112215
06 meter E =
0021141
Z = 4414977
89 I = 51
39601
XDOT = -2689
893599 Wp = 11
75812
YDOT = 6454
561021 meter/sec RA = 314
46108 deg
ZDOT = 3257
857245 TA = 45
61714
MA = 45
44419
Ha = 193
699 n
mi
Hp = 175
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16564628
20 X = 5028331
09
Y = -368159
66 feet Y = -55848
82 meter
Z = 14484835
60 Z = 4439455
73
XDOT = -8825
110234 XDOT = -2777
724408
YDOT = 21176
381303 feet/sec YDOT = 6423
977238 meter/sec
ZDOT = 10688
508021 ZDOT = 3244
577466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6069907
81 X = 1850107
90
Y = -15330312
36 feet Y = -4672679
21 meter
Z = 14576373
11 Z = 4442878
52
XDOT = 14937
992295 XDOT = 4553
100052
YDOT = 15976
074935 feet/sec YDOT = 4869
507640 meter/sec
ZDOT = 10639
567474 ZDOT = 3242
940166
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
99898980
00014500 00000-0 95600-4 0 9040
2 29647 51
6319 314
7162 0024404 350
7376 9
3335 15
75997254 1428
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06352
99898980 = yrday
fracday
Element set: 904
Inclination: 51
6319 deg
RA of node: 314
7162 deg
Eccentricity:
0024404
Arg of perigee: 350
7376 deg
Mean anomaly: 9
3335 deg
Mean motion: 15
75997254 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 142
Checksum: 335
Coasting Arc #6 (Orbit 141)
---------------------------------------
Vector Time (GMT): 2006/352/23:09:49
797
Vector Time (MET): 008/21:22:14
823
Weight (LBS) : 237378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3967773
67 A = 6720617
82 meter
Y = 5328847
02 meter E =
0025032
Z = 1109598
22 I = 51
42297
XDOT = -4486
928657 Wp = 13
26204
YDOT = -2107
981218 meter/sec RA = 314
32620 deg
ZDOT = -5870
824618 TA = 154
57366
MA = 154
45030
Ha = 193
682 n
mi
Hp = 170
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13017630
17 X = -4032480
56
Y = 17483093
91 feet Y = 5284097
32 meter
Z = 3640414
10 Z = 1090166
39
XDOT = -14720
894544 XDOT = -4434
494095
YDOT = -6915
948878 feet/sec YDOT = -2157
882169 meter/sec
ZDOT = -19261
235623 ZDOT = -5892
495392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13256913
29 X = 4040707
17
Y = 17317364
20 feet Y = 5278332
61 meter
Z = 3568337
16 Z = 1087629
17
XDOT = -9381
911832 XDOT = -2859
606727
YDOT = 11202
394441 feet/sec YDOT = 3414
489826 meter/sec
ZDOT = -19342
524640 ZDOT = -5895
601510
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
99894581
00014500 00000-0 95600-4 0 9054
2 29647 51
6319 314
7160 0032430 349
9936 10
0580 15
77882011 1423
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06352
99894581 = yrday
fracday
Element set: 905
Inclination: 51
6319 deg
RA of node: 314
7160 deg
Eccentricity:
0032430
Arg of perigee: 349
9936 deg
Mean anomaly: 10
0580 deg
Mean motion: 15
77882011 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 142
Checksum: 314
Coasting Arc #7 (Orbit 142)
---------------------------------------
Vector Time (GMT): 2006/352/23:59:48
469
Vector Time (MET): 008/22:12:13
495
Weight (LBS) : 237082
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4906413
28 A = 6714397
75 meter
Y = -4531028
63 meter E =
0030319
Z = 455209
71 I = 51
42573
XDOT = 2974
889251 Wp = 6
92785
YDOT = 3827
217474 meter/sec RA = 314
16160 deg
ZDOT = 6019
001106 TA = 358
06213
MA = 358
07385
Ha = 186
262 n
mi
Hp = 170
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16097156
43 X = 4954523
84
Y = -14865579
49 feet Y = -4475871
47 meter
Z = 1493470
17 Z = 479161
33
XDOT = 9760
135339 XDOT = 2902
614912
YDOT = 12556
487774 feet/sec YDOT = 3860
092207 meter/sec
ZDOT = 19747
378956 ZDOT = 6033
278444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13907898
39 X = -4239127
43
Y = -16923364
78 feet Y = -5158241
58 meter
Z = 1582541
88 Z = 482358
77
XDOT = 11860
658708 XDOT = 3615
128774
YDOT = -7892
264584 feet/sec YDOT = -2405
562245 meter/sec
ZDOT = 19801
209448 ZDOT = 6035
408640
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 06353
06218587
00014500 00000-0 95600-4 0 9060
2 29647 51
6339 314
3881 0022509 344
0698 15
9758 15
80239534 1430
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06353
06218587 = yrday
fracday
Element set: 906
Inclination: 51
6339 deg
RA of node: 314
3881 deg
Eccentricity:
0022509
Arg of perigee: 344
0698 deg
Mean anomaly: 15
9758 deg
Mean motion: 15
80239534 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 143
Checksum: 327
Coasting Arc #8 (Orbit 157)
---------------------------------------
Vector Time (GMT): 2006/354/00:02:22
588
Vector Time (MET): 009/22:14:47
615
Weight (LBS) : 237082
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 663
13 A = 6706915
40 meter
Y = -5266893
79 meter E =
0019495
Z = -4141753
96 I = 51
38181
XDOT = 6127
371709 Wp = 7
51350
YDOT = -2888
883136 meter/sec RA = 308
92199 deg
ZDOT = 3695
666541 TA = 300
19345
MA = 300
38640
Ha = 186
486 n
mi
Hp = 170
308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2175
63 X = 79701
74
Y = -17279835
27 feet Y = -5266443
43 meter
Z = -13588431
63 Z = -4141559
82
XDOT = 20102
925556 XDOT = 6141
279808
YDOT = -9477
963045 feet/sec YDOT = -2820
259071 meter/sec
ZDOT = 12124
890225 ZDOT = 3725
466696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17269925
51 X = -5263873
30
Y = -588202
64 feet Y = -179284
16 meter
Z = -13588299
25 Z = -4141713
61
XDOT = -8924
542043 XDOT = -2720
200415
YDOT = -19047
509034 feet/sec YDOT = -5805
680753 meter/sec
ZDOT = 12236
029938 ZDOT = 3729
541925
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
01076459
00014500 00000-0 95600-4 0 9077
2 29647 51
6342 309
4715 0022568 347
6101 12
4508 15
80245583 1580
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06354
01076459 = yrday
fracday
Element set: 907
Inclination: 51
6342 deg
RA of node: 309
4715 deg
Eccentricity:
0022568
Arg of perigee: 347
6101 deg
Mean anomaly: 12
4508 deg
Mean motion: 15
80245583 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 158
Checksum: 304
Coasting Arc #9 (Orbit 170)
---------------------------------------
Vector Time (GMT): 2006/354/18:29:18
438
Vector Time (MET): 010/16:41:43
465
Weight (LBS) : 237028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4064330
95 A = 6715376
16 meter
Y = -5305078
09 meter E =
0033539
Z = 365180
62 I = 51
39486
XDOT = 3632
482856 Wp = 10
12816
YDOT = 3201
195649 meter/sec RA = 304
95592 deg
ZDOT = 6025
864767 TA = 353
87548
MA = 353
91639
Ha = 187
897 n
mi
Hp = 169
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13334419
14 X = 4121600
50
Y = -17405111
84 feet Y = -5259290
08 meter
Z = 1198099
15 Z = 385063
20
XDOT = 11917
594671 XDOT = 3567
129595
YDOT = 10502
610398 feet/sec YDOT = 3241
465510 meter/sec
ZDOT = 19769
897529 ZDOT = 6043
353314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11501599
58 X = 3505687
55
Y = -18662144
50 feet Y = -5688221
64 meter
Z = 1271873
91 Z = 387667
17
XDOT = 11447
336056 XDOT = 3489
148030
YDOT = 8417
562424 feet/sec YDOT = 2565
673027 meter/sec
ZDOT = 19835
678541 ZDOT = 6045
914819
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
83286660
00014500 00000-0 95600-4 0 9085
2 29647 51
6352 305
2136 0024749 351
4423 8
6318 15
79907274 1716
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06354
83286660 = yrday
fracday
Element set: 908
Inclination: 51
6352 deg
RA of node: 305
2136 deg
Eccentricity:
0024749
Arg of perigee: 351
4423 deg
Mean anomaly: 8
6318 deg
Mean motion: 15
79907274 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 171
Checksum: 318
Coasting Arc #10 (Orbit 185)
---------------------------------------
Vector Time (GMT): 2006/355/18:31:43
267
Vector Time (MET): 011/16:44:08
294
Weight (LBS) : 237028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1081990
38 A = 6707236
36 meter
Y = -5031140
34 meter E =
0022327
Z = -4293890
54 I = 51
35124
XDOT = 5532
939401 Wp = 15
68060
YDOT = -4117
974967 meter/sec RA = 299
71766 deg
ZDOT = 3456
180809 TA = 289
20256
MA = 289
44404
Ha = 188
034 n
mi
Hp = 169
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3549837
21 X = -1004769
69
Y = -16506365
94 feet Y = -5042811
79 meter
Z = -14087567
39 Z = -4298960
26
XDOT = 18152
688323 XDOT = 5561
804628
YDOT = -13510
416557 feet/sec YDOT = -4055
917106 meter/sec
ZDOT = 11339
175881 ZDOT = 3483
129014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5565184
47 X = -1696268
23
Y = -15922917
23 feet Y = -4853305
17 meter
Z = -14107106
17 Z = -4299845
96
XDOT = 15041
218368 XDOT = 4584
563359
YDOT = -15318
366440 feet/sec YDOT = -4669
038091 meter/sec
ZDOT = 11439
521134 ZDOT = 3486
766042
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
78164724
00014500 00000-0 95600-4 0 9097
2 29647 51
6342 300
2972 0024696 355
0205 5
0712 15
79926385 1866
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06355
78164724 = yrday
fracday
Element set: 909
Inclination: 51
6342 deg
RA of node: 300
2972 deg
Eccentricity:
0024696
Arg of perigee: 355
0205 deg
Mean anomaly: 5
0712 deg
Mean motion: 15
79926385 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 186
Checksum: 320
Coasting Arc #11 (Orbit 201)
---------------------------------------
Vector Time (GMT): 2006/356/18:34:16
233
Vector Time (MET): 012/16:46:41
260
Weight (LBS) : 237028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4612186
98 A = 6705035
62 meter
Y = 817963
88 meter E =
0030327
Z = -4817444
20 I = 51
32988
XDOT = 1215
607930 Wp = 21
37824
YDOT = -7219
267257 meter/sec RA = 294
55022 deg
ZDOT = -2366
407038 TA = 225
29812
MA = 225
54553
Ha = 188
146 n
mi
Hp = 169
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15131847
04 X = -4597592
14
Y = 2683608
54 feet Y = 766449
78 meter
Z = -15805263
13 Z = -4839814
41
XDOT = 3988
214992 XDOT = 1307
772069
YDOT = -23685
260030 feet/sec YDOT = -7205
152276 meter/sec
ZDOT = -7763
802619 ZDOT = -2360
279122
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14437945
34 X = -4400685
74
Y = 5007057
80 feet Y = 1526151
22 meter
Z = -15888863
99 Z = -4842925
74
XDOT = 636
489397 XDOT = 194
001968
YDOT = -22971
455509 feet/sec YDOT = -7001
699639 meter/sec
ZDOT = -7741
706557 ZDOT = -2359
672159
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
79365874
00014500 00000-0 95600-4 0 9100
2 29647 51
6330 295
0534 0024627 359
0065 1
1048 15
79963060 2029
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06356
79365874 = yrday
fracday
Element set: 910
Inclination: 51
6330 deg
RA of node: 295
0534 deg
Eccentricity:
0024627
Arg of perigee: 359
0065 deg
Mean anomaly: 1
1048 deg
Mean motion: 15
79963060 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 202
Checksum: 306
Coasting Arc #12 (Orbit 217)
---------------------------------------
Vector Time (GMT): 2006/357/18:37:16
915
Vector Time (MET): 013/16:49:41
942
Weight (LBS) : 237028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2924407
57 A = 6714645
08 meter
Y = 5978459
38 meter E =
0018355
Z = -976676
28 I = 51
35222
XDOT = -3981
692425 Wp = 23
44674
YDOT = -2908
413034 meter/sec RA = 289
32676 deg
ZDOT = -5902
369761 TA = 167
26738
MA = 167
22096
Ha = 188
251 n
mi
Hp = 169
009
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9594513
01 X = -2986324
26
Y = 19614368
03 feet Y = 5945397
80 meter
Z = -3204318
51 Z = -991032
34
XDOT = -13063
295357 XDOT = -3920
188738
YDOT = -9542
037514 feet/sec YDOT = -2952
611345 meter/sec
ZDOT = -19364
730187 ZDOT = -5921
563665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5749095
27 X = -1752324
24
Y = 21056671
90 feet Y = 6418073
60 meter
Z = -3257336
68 Z = -992836
22
XDOT = -12973
018376 XDOT = -3954
176001
YDOT = -6538
066188 feet/sec YDOT = -1992
802574 meter/sec
ZDOT = -19436
885818 ZDOT = -5924
362797
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
80564083
00014500 00000-0 95600-4 0 9117
2 29647 51
6330 289
8093 0024628 2
9733 357
1581 15
80021714 2183
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06357
80564083 = yrday
fracday
Element set: 911
Inclination: 51
6330 deg
RA of node: 289
8093 deg
Eccentricity:
0024628
Arg of perigee: 2
9733 deg
Mean anomaly: 357
1581 deg
Mean motion: 15
80021714 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 218
Checksum: 307
Coasting Arc #13 (Orbit 233)
---------------------------------------
Vector Time (GMT): 2006/358/18:39:36
065
Vector Time (MET): 014/16:52:01
092
Weight (LBS) : 237028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1921418
76 A = 6708333
18 meter
Y = 5126136
17 meter E =
0029635
Z = 3885689
69 I = 51
32238
XDOT = -4515
897163 Wp = 27
66780
YDOT = 4770
651144 meter/sec RA = 284
07710 deg
ZDOT = -4022
347407 TA = 104
47953
MA = 104
15054
Ha = 188
243 n
mi
Hp = 168
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6303867
31 X = 1845056
06
Y = 16818032
07 feet Y = 5147203
48 meter
Z = 12748325
76 Z = 3894839
02
XDOT = -14815
935574 XDOT = -4549
389090
YDOT = 15651
742597 feet/sec YDOT = 4719
944905 meter/sec
ZDOT = -13196
677846 ZDOT = -4044
366104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9677888
39 X = 2949820
38
Y = 15100790
50 feet Y = 4602720
94 meter
Z = 12783166
98 Z = 3896309
29
XDOT = -9962
427878 XDOT = -3036
548017
YDOT = 17731
182697 feet/sec YDOT = 5404
464486 meter/sec
ZDOT = -13278
504587 ZDOT = -4047
288198
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 06358
81759307
00014500 00000-0 95600-4 0 9125
2 29647 51
6324 284
5637 0024449 6
5834 353
5649 15
80068094 2340
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06358
81759307 = yrday
fracday
Element set: 912
Inclination: 51
6324 deg
RA of node: 284
5637 deg
Eccentricity:
0024449
Arg of perigee: 6
5834 deg
Mean anomaly: 353
5649 deg
Mean motion: 15
80068094 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 234
Checksum: 332
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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