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
169 0
5 -1
5 1
5
008/20:54:03
196 -1
3 -0
0 192
6
000/00:00:06
392 -0
6 0
0 176
0
352/23:09:42
456 5
8 -10
0 10
0
008/21:22:07
483 2
8 -0
0 192
6
000/00:00:14
966 7
6 -0
1 170
4
352/23:52:55
314 -6
4 -9
6 9
6
008/22:05:20
341 -1
4 0
0 187
4
000/00:00:14
301 -7
0 -0
1 170
1
354/20:01:26
788 0
9 2
0 2
0
010/18:13:51
815 0
9 -0
0 188
9
000/00:00:08
504 1
6 0
0 169
5
Coasting Arc #1 (Orbit 35)
---------------------------------------
Vector Time (GMT): 2006/346/05:30:12
000
Vector Time (MET): 002/03:42:37
027
Weight (LBS) : 240427
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1001859
55 A = 6715007
27 meter
Y = 4061254
29 meter E =
0022204
Z = 5262021
29 I = 51
55459
XDOT = -7522
390542 Wp = 329
72295
YDOT = 1614
361409 meter/sec RA = 349
10245 deg
ZDOT = 205
466175 TA = 118
43566
MA = 118
21175
Ha = 192
507 n
mi
Hp = 177
857
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3286940
78 X = 930791
40
Y = 13324325
09 feet Y = 4072064
06 meter
Z = 17263849
36 Z = 5266716
11
XDOT = -24679
758996 XDOT = -7540
888425
YDOT = 5296
461315 feet/sec YDOT = 1530
104802 meter/sec
ZDOT = 674
101624 ZDOT = 168
877546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 938872
66 X = 286168
39
Y = -13668854
85 feet Y = -4166266
96 meter
Z = 17281870
24 Z = 5267514
05
XDOT = 24140
791319 XDOT = 7358
113194
YDOT = 2258
045890 feet/sec YDOT = 688
252387 meter/sec
ZDOT = 537
454996 ZDOT = 163
816283
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 06346
27715602
00014500 00000-0 95600-4 0 9009
2 29647 51
6359 349
3372 0023750 325
6813 34
2816 15
75791841 366
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06346
27715602 = yrday
fracday
Element set: 900
Inclination: 51
6359 deg
RA of node: 349
3372 deg
Eccentricity:
0023750
Arg of perigee: 325
6813 deg
Mean anomaly: 34
2816 deg
Mean motion: 15
75791841 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 36
Checksum: 312
Coasting Arc #2 (Orbit 51)
---------------------------------------
Vector Time (GMT): 2006/347/05:35:16
652
Vector Time (MET): 003/03:47:41
679
Weight (LBS) : 240427
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6338935
50 A = 6724869
34 meter
Y = -8086
82 meter E =
0024856
Z = 2198479
37 I = 51
56020
XDOT = -1890
760234 Wp = 2
80217
YDOT = 5080
129905 meter/sec RA = 343
94823 deg
ZDOT = 5492
176107 TA = 21
92797
MA = 21
82179
Ha = 192
627 n
mi
Hp = 177
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20797032
50 X = 6327874
65
Y = -26531
55 feet Y = 62764
89 meter
Z = 7212858
83 Z = 2229247
24
XDOT = -6203
281606 XDOT = -1974
129162
YDOT = 16667
092865 feet/sec YDOT = 5058
511083 meter/sec
ZDOT = 18018
950481 ZDOT = 5482
788722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20043250
85 X = -6109182
86
Y = -5395579
95 feet Y = -1644572
77 meter
Z = 7327919
85 Z = 2233549
97
XDOT = 10043
814978 XDOT = 3061
354805
YDOT = -12980
692887 feet/sec YDOT = -3956
515192 meter/sec
ZDOT = 17984
425658 ZDOT = 5481
652941
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 06347
29184183
00014500 00000-0 95600-4 0 9017
2 29647 51
6359 344
1123 0023656 329
9099 30
0705 15
75805370 523
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06347
29184183 = yrday
fracday
Element set: 901
Inclination: 51
6359 deg
RA of node: 344
1123 deg
Eccentricity:
0023656
Arg of perigee: 329
9099 deg
Mean anomaly: 30
0705 deg
Mean motion: 15
75805370 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 52
Checksum: 307
Coasting Arc #3 (Orbit 66)
---------------------------------------
Vector Time (GMT): 2006/348/05:39:57
334
Vector Time (MET): 004/03:52:22
361
Weight (LBS) : 240427
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3792049
55 A = 6721961
48 meter
Y = -4370917
34 meter E =
0021966
Z = -3394092
00 I = 51
52314
XDOT = 5971
907961 Wp = 344
36641
YDOT = 1609
654221 meter/sec RA = 338
72984 deg
ZDOT = 4613
131432 TA = 335
37283
MA = 335
47756
Ha = 192
936 n
mi
Hp = 177
470
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12441107
44 X = 3857151
28
Y = -14340279
98 feet Y = -4328131
12 meter
Z = -11135472
45 Z = -3375512
35
XDOT = 19592
873888 XDOT = 5931
047282
YDOT = 5281
017786 feet/sec YDOT = 1676
233045 meter/sec
ZDOT = 15134
945643 ZDOT = 4642
044155
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15404428
47 X = -4695269
80
Y = 11165119
43 feet Y = 3403128
40 meter
Z = -11066490
97 Z = -3373066
45
XDOT = -17009
666052 XDOT = -5184
546213
YDOT = -8405
092019 feet/sec YDOT = -2561
872047 meter/sec
ZDOT = 15243
253084 ZDOT = 4646
143540
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
24308257
00014500 00000-0 95600-4 0 9024
2 29647 51
6356 339
2146 0023719 333
3121 26
6821 15
75840887 673
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06348
24308257 = yrday
fracday
Element set: 902
Inclination: 51
6356 deg
RA of node: 339
2146 deg
Eccentricity:
0023719
Arg of perigee: 333
3121 deg
Mean anomaly: 26
6821 deg
Mean motion: 15
75840887 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 67
Checksum: 314
Coasting Arc #4 (Orbit 82)
---------------------------------------
Vector Time (GMT): 2006/349/05:44:43
625
Vector Time (MET): 005/03:57:08
652
Weight (LBS) : 240427
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3318755
04 A = 6715497
18 meter
Y = -2876198
72 meter E =
0024938
Z = -5089626
29 I = 51
47486
XDOT = 6142
543710 Wp = 9
96347
YDOT = -4386
595355 meter/sec RA = 333
59191 deg
ZDOT = -1503
331815 TA = 245
44798
MA = 245
70812
Ha = 193
007 n
mi
Hp = 177
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10888303
93 X = -3261608
52
Y = -9436347
50 feet Y = -2913005
47 meter
Z = -16698248
97 Z = -5105610
52
XDOT = 20152
702462 XDOT = 6198
460981
YDOT = -14391
717043 feet/sec YDOT = -4317
565665 meter/sec
ZDOT = -4932
190993 ZDOT = -1473
355619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8836268
62 X = 2693294
68
Y = 11292002
15 feet Y = 3441802
26 meter
Z = -16758352
53 Z = -5107945
85
XDOT = -21695
571246 XDOT = -6612
810116
YDOT = 9711
136275 feet/sec YDOT = 2959
954337 meter/sec
ZDOT = -4820
591434 ZDOT = -1469
316269
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
25771132
00014500 00000-0 95600-4 0 9033
2 29647 51
6348 333
9893 0023672 337
2569 22
7544 15
75873746 838
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06349
25771132 = yrday
fracday
Element set: 903
Inclination: 51
6348 deg
RA of node: 333
9893 deg
Eccentricity:
0023672
Arg of perigee: 337
2569 deg
Mean anomaly: 22
7544 deg
Mean motion: 15
75873746 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 83
Checksum: 338
Coasting Arc #5 (Orbit 98)
---------------------------------------
Vector Time (GMT): 2006/350/05:49:27
719
Vector Time (MET): 006/04:01:52
746
Weight (LBS) : 240427
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6059292
79 A = 6726140
89 meter
Y = 2750077
34 meter E =
0014902
Z = -1044704
49 I = 51
48577
XDOT = -1156
576422 Wp = 353
55133
YDOT = -4796
337113 meter/sec RA = 328
41085 deg
ZDOT = -5895
004293 TA = 197
88172
MA = 197
93421
Ha = 193
182 n
mi
Hp = 176
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19879569
52 X = -6084531
11
Y = 9022563
45 feet Y = 2682150
89 meter
Z = -3427508
18 Z = -1074201
92
XDOT = -3794
542067 XDOT = -1074
198404
YDOT = -15736
014151 feet/sec YDOT = -4808
814204 meter/sec
ZDOT = -19340
565267 ZDOT = -5900
423551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20989016
52 X = 6397452
24
Y = -5941294
68 feet Y = -1810906
62 meter
Z = -3537506
33 Z = -1078231
93
XDOT = 851
888302 XDOT = 259
655554
YDOT = 14580
436371 feet/sec YDOT = 4444
117006 meter/sec
ZDOT = -19361
377042 ZDOT = -5901
347722
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
27231086
00014500 00000-0 95600-4 0 9047
2 29647 51
6341 328
7632 0023632 341
6212 18
4096 15
75940104 998
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06350
27231086 = yrday
fracday
Element set: 904
Inclination: 51
6341 deg
RA of node: 328
7632 deg
Eccentricity:
0023632
Arg of perigee: 341
6212 deg
Mean anomaly: 18
4096 deg
Mean motion: 15
75940104 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 99
Checksum: 292
Coasting Arc #6 (Orbit 114)
---------------------------------------
Vector Time (GMT): 2006/351/05:54:02
645
Vector Time (MET): 007/04:06:27
672
Weight (LBS) : 240427
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1245157
92 A = 6718818
88 meter
Y = 5109081
13 meter E =
0026008
Z = 4195654
91 I = 51
43856
XDOT = -6648
699480 Wp = 7
90936
YDOT = 1373
266607 meter/sec RA = 323
19440 deg
ZDOT = -3617
352510 TA = 119
18914
MA = 118
92871
Ha = 193
299 n
mi
Hp = 176
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4085163
78 X = -1322600
61
Y = 16762077
20 feet Y = 5094717
71 meter
Z = 13765272
00 Z = 4189418
50
XDOT = -21813
318504 XDOT = -6645
994482
YDOT = 4505
467872 feet/sec YDOT = 1298
903169 meter/sec
ZDOT = -11867
954428 ZDOT = -3649
645603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6030160
37 X = 1837992
88
Y = -16183899
38 feet Y = -4932852
53 meter
Z = 13742527
97 Z = 4188722
53
XDOT = 20937
104423 XDOT = 6381
629428
YDOT = -2457
101996 feet/sec YDOT = -748
924688 meter/sec
ZDOT = -11988
567969 ZDOT = -3654
115517
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
28687906
00014500 00000-0 95600-4 0 9056
2 29647 51
6347 323
5362 0023748 345
2456 14
8012 15
76018428 1158
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06351
28687906 = yrday
fracday
Element set: 905
Inclination: 51
6347 deg
RA of node: 323
5362 deg
Eccentricity:
0023748
Arg of perigee: 345
2456 deg
Mean anomaly: 14
8012 deg
Mean motion: 15
76018428 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 115
Checksum: 311
Coasting Arc #7 (Orbit 130)
---------------------------------------
Vector Time (GMT): 2006/352/05:59:09
004
Vector Time (MET): 008/04:11:34
031
Weight (LBS) : 240427
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4662697
95 A = 6716429
24 meter
Y = 896483
21 meter E =
0019651
Z = 4740820
58 I = 51
40842
XDOT = -3801
219182 Wp = 5
34145
YDOT = 6190
981313 meter/sec RA = 318
05522 deg
ZDOT = 2586
304754 TA = 59
34524
MA = 59
15167
Ha = 193
307 n
mi
Hp = 176
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15297565
45 X = 4629292
22
Y = 2941217
88 feet Y = 948457
21 meter
Z = 15553873
31 Z = 4763391
29
XDOT = -12471
191543 XDOT = -3882
756491
YDOT = 20311
618481 feet/sec YDOT = 6148
000475 meter/sec
ZDOT = 8485
251819 ZDOT = 2567
641206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14952975
68 X = -4557666
99
Y = -4054452
52 feet Y = -1235797
13 meter
Z = 15638388
00 Z = 4766580
66
XDOT = 13685
595135 XDOT = 4171
369397
YDOT = -18243
132446 feet/sec YDOT = -5560
506770 meter/sec
ZDOT = 8416
149742 ZDOT = 2565
242441
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
30141950
00014500 00000-0 95600-4 0 9065
2 29647 51
6343 318
3096 0023615 349
3875 10
6788 15
76042057 1310
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06352
30141950 = yrday
fracday
Element set: 906
Inclination: 51
6343 deg
RA of node: 318
3096 deg
Eccentricity:
0023615
Arg of perigee: 349
3875 deg
Mean anomaly: 10
6788 deg
Mean motion: 15
76042057 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 131
Checksum: 302
Coasting Arc #8 (Orbit 141)
---------------------------------------
Vector Time (GMT): 2006/352/22:41:41
365
Vector Time (MET): 008/20:54:06
392
Weight (LBS) : 240385
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5045024
38 A = 6716813
24 meter
Y = -103846
05 meter E =
0019671
Z = 4419089
54 I = 51
39530
XDOT = -2698
919014 Wp = 11
81515
YDOT = 6454
845990 meter/sec RA = 314
45671 deg
ZDOT = 3249
335922 TA = 45
64903
MA = 45
48801
Ha = 192
616 n
mi
Hp = 175
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16551917
26 X = 5024343
49
Y = -340702
27 feet Y = -47523
78 meter
Z = 14498325
26 Z = 4443548
29
XDOT = -8854
721173 XDOT = -2786
710943
YDOT = 21177
316241 feet/sec YDOT = 6424
161459 meter/sec
ZDOT = 10660
550926 ZDOT = 3236
012392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6097205
22 X = 1858428
15
Y = -15305081
76 feet Y = -4664988
92 meter
Z = 14589792
30 Z = 4446968
69
XDOT = 14921
748727 XDOT = 4548
149012
YDOT = 16008
892319 feet/sec YDOT = 4879
510379 meter/sec
ZDOT = 10611
446780 ZDOT = 3234
368979
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
99888702
00014500 00000-0 95600-4 0 9074
2 29647 51
6312 314
7118 0023039 349
5036 10
5644 15
76357970 1427
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06352
99888702 = yrday
fracday
Element set: 907
Inclination: 51
6312 deg
RA of node: 314
7118 deg
Eccentricity:
0023039
Arg of perigee: 349
5036 deg
Mean anomaly: 10
5644 deg
Mean motion: 15
76357970 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 142
Checksum: 318
Coasting Arc #9 (Orbit 141)
---------------------------------------
Vector Time (GMT): 2006/352/23:09:49
939
Vector Time (MET): 008/21:22:14
966
Weight (LBS) : 240148
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4002917
81 A = 6719638
41 meter
Y = 5310069
70 meter E =
0023509
Z = 1060984
37 I = 51
42249
XDOT = -4445
097353 Wp = 13
49387
YDOT = -2165
513325 meter/sec RA = 314
32186 deg
ZDOT = -5883
753179 TA = 154
87904
MA = 154
76449
Ha = 192
612 n
mi
Hp = 170
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13132932
45 X = -4067175
87
Y = 17421488
52 feet Y = 5264929
36 meter
Z = 3480919
85 Z = 1041382
90
XDOT = -14583
652733 XDOT = -4391
959508
YDOT = -7104
702510 feet/sec YDOT = -2214
942372 meter/sec
ZDOT = -19303
652163 ZDOT = -5905
219038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13166578
47 X = 4013173
12
Y = 17410465
85 feet Y = 5306709
99 meter
Z = 3408206
30 Z = 1038821
28
XDOT = -9519
021792 XDOT = -2901
397842
YDOT = 11025
288160 feet/sec YDOT = 3360
507831 meter/sec
ZDOT = -19384
181251 ZDOT = -5908
298445
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
99884345
00014500 00000-0 95600-4 0 9084
2 29647 51
6313 314
7116 0031073 349
2554 10
7944 15
78243658 1429
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06352
99884345 = yrday
fracday
Element set: 908
Inclination: 51
6313 deg
RA of node: 314
7116 deg
Eccentricity:
0031073
Arg of perigee: 349
2554 deg
Mean anomaly: 10
7944 deg
Mean motion: 15
78243658 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 142
Checksum: 320
Coasting Arc #10 (Orbit 141)
---------------------------------------
Vector Time (GMT): 2006/352/23:53:02
465
Vector Time (MET): 008/22:05:27
492
Weight (LBS) : 239923
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3258865
36 A = 6713612
87 meter
Y = -5532065
22 meter E =
0028814
Z = -1900405
21 I = 51
42008
XDOT = 5170
069893 Wp = 2
70619
YDOT = 1122
529449 meter/sec RA = 314
15900 deg
ZDOT = 5629
909166 TA = 336
00582
MA = 336
13982
Ha = 187
414 n
mi
Hp = 170
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10691815
48 X = 3329739
93
Y = -18149820
29 feet Y = -5495211
44 meter
Z = -6234925
25 Z = -1884402
36
XDOT = 16962
171566 XDOT = 5129
778722
YDOT = 3682
839400 feet/sec YDOT = 1180
140680 meter/sec
ZDOT = 18470
830596 ZDOT = 5654
927986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17141649
84 X = -5224774
87
Y = -12273133
61 feet Y = -3740851
12 meter
Z = -6175695
87 Z = -1882352
10
XDOT = 4248
837548 XDOT = 1295
045684
YDOT = -15222
703118 feet/sec YDOT = -4639
879910 meter/sec
ZDOT = 18564
530858 ZDOT = 5658
469005
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
99884635
00014500 00000-0 95600-4 0 9097
2 29647 51
6331 314
7117 0023394 352
7685 7
3140 15
79996388 1427
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06352
99884635 = yrday
fracday
Element set: 909
Inclination: 51
6331 deg
RA of node: 314
7117 deg
Eccentricity:
0023394
Arg of perigee: 352
7685 deg
Mean anomaly: 7
3140 deg
Mean motion: 15
79996388 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 142
Checksum: 341
Coasting Arc #11 (Orbit 157)
---------------------------------------
Vector Time (GMT): 2006/353/23:55:27
194
Vector Time (MET): 009/22:07:52
221
Weight (LBS) : 239923
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2469599
63 A = 6703308
02 meter
Y = -3505226
36 meter E =
0024892
Z = -5160368
96 I = 51
36694
XDOT = 5430
130324 Wp = 31
30916
YDOT = -5360
475200 meter/sec RA = 308
96066 deg
ZDOT = 1065
711854 TA = 248
75740
MA = 249
02344
Ha = 187
459 n
mi
Hp = 169
742
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8102361
00 X = -2405136
10
Y = -11500086
47 feet Y = -3532492
19 meter
Z = -16930344
36 Z = -5172210
47
XDOT = 17815
388202 XDOT = 5484
514914
YDOT = -17586
860893 feet/sec YDOT = -5299
424251 meter/sec
ZDOT = 3496
429968 ZDOT = 1092
222610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11958462
35 X = -3644939
33
Y = 7306180
44 feet Y = 2226923
80 meter
Z = -16975031
90 Z = -5173989
72
XDOT = -15958
088060 XDOT = -4864
025241
YDOT = -17943
879457 feet/sec YDOT = -5469
294458 meter/sec
ZDOT = 3594
987239 ZDOT = 1095
752110
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
01081065
00014500 00000-0 95600-4 0 9100
2 29647 51
6334 309
4687 0023352 356
8355 3
2660 15
80044233 1580
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06354
01081065 = yrday
fracday
Element set: 910
Inclination: 51
6334 deg
RA of node: 309
4687 deg
Eccentricity:
0023352
Arg of perigee: 356
8355 deg
Mean anomaly: 3
2660 deg
Mean motion: 15
80044233 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 158
Checksum: 287
Coasting Arc #12 (Orbit 171)
---------------------------------------
Vector Time (GMT): 2006/354/20:01:31
040
Vector Time (MET): 010/18:13:56
067
Weight (LBS) : 239867
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4224617
48 A = 6715922
12 meter
Y = -5144086
56 meter E =
0035326
Z = 693541
03 I = 51
39021
XDOT = 3349
422195 Wp = 17
32620
YDOT = 3563
914725 meter/sec RA = 304
62210 deg
ZDOT = 5987
176956 TA = 350
29467
MA = 350
36273
Ha = 188
916 n
mi
Hp = 169
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13860293
56 X = 4278479
04
Y = -16876924
40 feet Y = -5096524
55 meter
Z = 2275397
09 Z = 714194
03
XDOT = 10988
917964 XDOT = 3280
220342
YDOT = 11692
633613 feet/sec YDOT = 3600
996462 meter/sec
ZDOT = 19642
969017 ZDOT = 6003
281112
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3962112
02 X = 1207651
74
Y = -21468236
34 feet Y = -6543518
44 meter
Z = 2352072
21 Z = 716911
61
XDOT = 13611
336603 XDOT = 4148
735397
YDOT = 4686
201009 feet/sec YDOT = 1428
354068 meter/sec
ZDOT = 19703
612951 ZDOT = 6005
661228
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
89627916
00014500 00000-0 95600-4 0 9118
2 29647 51
6321 304
8810 0025480
1566 359
9604 15
79657975 1726
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06354
89627916 = yrday
fracday
Element set: 911
Inclination: 51
6321 deg
RA of node: 304
8810 deg
Eccentricity:
0025480
Arg of perigee:
1566 deg
Mean anomaly: 359
9604 deg
Mean motion: 15
79657975 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 172
Checksum: 331
Coasting Arc #13 (Orbit 186)
---------------------------------------
Vector Time (GMT): 2006/355/20:04:07
747
Vector Time (MET): 011/18:16:32
774
Weight (LBS) : 239867
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -811435
40 A = 6708627
76 meter
Y = -5241640
81 meter E =
0024392
Z = -4099787
57 I = 51
35022
XDOT = 5576
489392 Wp = 21
58255
YDOT = -3779
359295 meter/sec RA = 299
38047 deg
ZDOT = 3757
682920 TA = 286
87522
MA = 287
14256
Ha = 188
996 n
mi
Hp = 169
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2662189
63 X = -732822
97
Y = -17196984
29 feet Y = -5250277
82 meter
Z = -13450746
63 Z = -4103539
60
XDOT = 18295
568870 XDOT = 5600
098791
YDOT = -12399
472754 feet/sec YDOT = -3716
843696 meter/sec
ZDOT = 12328
356038 ZDOT = 3784
829985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10970014
42 X = -3343660
40
Y = -13494014
41 feet Y = -4112975
59 meter
Z = -13465380
26 Z = -4104247
90
XDOT = 8409
400942 XDOT = 2563
185407
YDOT = -19143
350740 feet/sec YDOT = -5834
893306 meter/sec
ZDOT = 12429
484121 ZDOT = 3788
506760
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
84519628
00014500 00000-0 95600-4 0 9125
2 29647 51
6316 299
9654 0025321 3
9857 356
1506 15
79690690 1875
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06355
84519628 = yrday
fracday
Element set: 912
Inclination: 51
6316 deg
RA of node: 299
9654 deg
Eccentricity:
0025321
Arg of perigee: 3
9857 deg
Mean anomaly: 356
1506 deg
Mean motion: 15
79690690 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 187
Checksum: 347
Coasting Arc #14 (Orbit 202)
---------------------------------------
Vector Time (GMT): 2006/356/20:06:52
598
Vector Time (MET): 012/18:19:17
625
Weight (LBS) : 239867
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4537365
94 A = 6705159
32 meter
Y = 451957
15 meter E =
0032623
Z = -4938514
49 I = 51
32578
XDOT = 1497
291775 Wp = 29
37419
YDOT = -7269
010336 meter/sec RA = 294
21277 deg
ZDOT = -2018
508381 TA = 220
86018
MA = 221
10520
Ha = 189
084 n
mi
Hp = 168
766
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14886371
21 X = -4518094
17
Y = 1482799
04 feet Y = 401306
24 meter
Z = -16202475
36 Z = -4960509
92
XDOT = 4912
374591 XDOT = 1588
301406
YDOT = -23848
459108 feet/sec YDOT = -7251
750677 meter/sec
ZDOT = -6622
402825 ZDOT = -2011
014862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11726098
08 X = -3574114
70
Y = 9144920
94 feet Y = 2787371
90 meter
Z = -16284716
55 Z = -4963581
61
XDOT = -7864
270051 XDOT = -2397
029511
YDOT = -21958
507119 feet/sec YDOT = -6692
952970 meter/sec
ZDOT = -6595
203790 ZDOT = -2010
218115
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
85735468
00014500 00000-0 95600-4 0 9130
2 29647 51
6314 294
7229 0025285 8
2254 351
9322 15
79740672 2036
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06356
85735468 = yrday
fracday
Element set: 913
Inclination: 51
6314 deg
RA of node: 294
7229 deg
Eccentricity:
0025285
Arg of perigee: 8
2254 deg
Mean anomaly: 351
9322 deg
Mean motion: 15
79740672 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 203
Checksum: 323
Coasting Arc #15 (Orbit 218)
---------------------------------------
Vector Time (GMT): 2006/357/20:09:48
788
Vector Time (MET): 013/18:22:13
815
Weight (LBS) : 239867
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3037350
14 A = 6715004
42 meter
Y = 5883049
80 meter E =
0020645
Z = -1196796
30 I = 51
34930
XDOT = -3853
945242 Wp = 31
55364
YDOT = -3173
728384 meter/sec RA = 288
99486 deg
ZDOT = -5848
262933 TA = 161
61200
MA = 161
53727
Ha = 189
185 n
mi
Hp = 168
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9965059
52 X = -3097121
84
Y = 19301344
50 feet Y = 5848736
77 meter
Z = -3926497
06 Z = -1211695
84
XDOT = -12644
177302 XDOT = -3789
745919
YDOT = -10412
494699 feet/sec YDOT = -3216
482526 meter/sec
ZDOT = -19187
214347 ZDOT = -5866
829736
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2530589
64 X = 771323
72
Y = 21563974
36 feet Y = 6572699
38 meter
Z = -3981559
49 Z = -1213579
33
XDOT = -14642
777792 XDOT = -4463
118671
YDOT = -1820
391519 feet/sec YDOT = -554
855335 meter/sec
ZDOT = -19257
055140 ZDOT = -5869
550407
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
86948530
00014500 00000-0 95600-4 0 9149
2 29647 51
6313 289
4789 0025454 11
9622 348
2143 15
79819316 2194
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06357
86948530 = yrday
fracday
Element set: 914
Inclination: 51
6313 deg
RA of node: 289
4789 deg
Eccentricity:
0025454
Arg of perigee: 11
9622 deg
Mean anomaly: 348
2143 deg
Mean motion: 15
79819316 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 219
Checksum: 340
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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