SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2006/252/15:14:56 000 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 0
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
252/15:53:30
893 136
9 221
7 221
8
000/00:38:34
893 22
3 -0
1 154
1
000/00:02:27
786 -173
0 -6
0 123
7
252/18:10:01
000 -46
7 83
4 83
4
000/02:55:05
000 -21
7 0
0 171
2
000/00:00:56
341 65
6 -0
0 153
7
253/07:05:49
269 21
8 48
8 49
2
000/15:50:53
269 27
2 -1
6 181
5
000/00:04:01
496 -34
7 -5
9 171
2
253/18:27:01
504 -2
5 6
0 6
0
001/03:12:05
504 -3
3 0
0 181
5
000/00:00:26
467 4
3 0
0 174
4
254/06:36:41
135 -5
1 12
5 12
5
001/15:21:45
135 -7
5 0
0 182
5
000/00:00:18
533 8
6 -0
0 180
8
254/08:08:15
448 -3
7 8
9 8
9
001/16:53:19
448 -5
3 -0
1 187
5
000/00:00:14
016 6
2 -0
3 181
3
254/09:25:08
911 -1
7 2
5 2
9
001/18:10:12
911 -0
7 0
1 188
9
000/00:00:12
942 2
3 1
5 181
4
Coasting Arc #1 (begining on orbit 1)
---------------------------------------
Vector Time (GMT): 2006/252/15:25:25
000
Vector Time (MET): 000/00:10:29
000
Weight (LBS) : 257857
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4420985
54 A = 6518741
46 meter
Y = 1795751
38 meter E =
0127675
Z = 4392309
05 I = 51
91530
XDOT = 145
900014 Wp = 352
20423
YDOT = -7170
724269 meter/sec RA = 111
72760 deg
ZDOT = 3214
401463 TA = 67
16100
MA = 65
81768
Ha = 123
974 n
mi
Hp = 31
470
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14504545
74 X = -4462074
39
Y = 5891572
78 feet Y = 1746084
07 meter
Z = 14410462
76 Z = 4370731
93
XDOT = 478
674586 XDOT = 210
458185
YDOT = -23525
998257 feet/sec YDOT = -7168
731529 meter/sec
ZDOT = 10545
936557 ZDOT = 3215
267598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7586354
79 X = 2312320
94
Y = -13778299
08 feet Y = -4199625
56 meter
Z = 14330373
67 Z = 4367897
89
XDOT = 13527
432649 XDOT = 4123
161472
YDOT = 17952
784679 feet/sec YDOT = 5472
008770 meter/sec
ZDOT = 10548
131849 ZDOT = 3215
070587
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 99115U 06252
69318985
00014500 00000-0 95600-4 0 9005
2 99115 51
6321 112
2274 0057068 348
9940 11
0025 16
70601030 22
Satellite: SHUTTLE
Catalog Number: 99115
Epoch time: 06252
69318985 = yrday
fracday
Element set: 900
Inclination: 51
6321 deg
RA of node: 112
2274 deg
Eccentricity:
0057068
Arg of perigee: 348
9940 deg
Mean anomaly: 11
0025 deg
Mean motion: 16
70601030 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 2
Checksum: 270
Coasting Arc #2 (begining on orbit 1)
---------------------------------------
Vector Time (GMT): 2006/252/15:54:44
786
Vector Time (MET): 000/00:39:48
786
Weight (LBS) : 252279
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2354894
88 A = 6641376
47 meter
Y = -6172682
71 meter E =
0051219
Z = 103987
85 I = 51
94715
XDOT = 4520
393192 Wp = 174
73396
YDOT = 1618
214498 meter/sec RA = 111
58793 deg
ZDOT = -6130
382535 TA = 4
12083
MA = 4
07882
Ha = 154
082 n
mi
Hp = 123
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7726033
06 X = 2423238
49
Y = -20251583
70 feet Y = -6145966
84 meter
Z = 341167
49 Z = 115594
42
XDOT = 14830
686327 XDOT = 4531
742479
YDOT = 5309
102684 feet/sec YDOT = 1668
827034 meter/sec
ZDOT = -20112
803591 ZDOT = -6108
394980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9379252
60 X = 2858796
19
Y = 19540142
59 feet Y = 5955835
46 meter
Z = 383500
60 Z = 116890
98
XDOT = -12709
032812 XDOT = -3873
713201
YDOT = 6503
832466 feet/sec YDOT = 1982
368136 meter/sec
ZDOT = -20030
695774 ZDOT = -6105
356072
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 99115U 06252
69436307
00014500 00000-0 95600-4 0 9015
2 99115 51
6324 112
2375 0042349 185
9994 174
0684 16
06469124 27
Satellite: SHUTTLE
Catalog Number: 99115
Epoch time: 06252
69436307 = yrday
fracday
Element set: 901
Inclination: 51
6324 deg
RA of node: 112
2375 deg
Eccentricity:
0042349
Arg of perigee: 185
9994 deg
Mean anomaly: 174
0684 deg
Mean motion: 16
06469124 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 2
Checksum: 305
Coasting Arc #3 (begining on orbit 3)
---------------------------------------
Vector Time (GMT): 2006/252/18:10:29
171
Vector Time (MET): 000/02:55:33
171
Weight (LBS) : 250215
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2675001
91 A = 6684993
74 meter
Y = 6090396
74 meter E =
0032877
Z = 389175
01 I = 51
95082
XDOT = -4234
205767 Wp = 14
05379
YDOT = -2253
191754 meter/sec RA = 111
08736 deg
ZDOT = 6083
456420 TA = 350
19959
MA = 350
26356
Ha = 171
221 n
mi
Hp = 153
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8776252
97 X = -2744797
29
Y = 19981616
59 feet Y = 6060093
17 meter
Z = 1276820
90 Z = 376009
84
XDOT = -13891
751203 XDOT = -4238
247978
YDOT = -7392
361396 feet/sec YDOT = -2300
563140 meter/sec
ZDOT = 19958
846521 ZDOT = 6062
876947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18267494
95 X = -5567932
46
Y = -11945998
67 feet Y = -3641140
40 meter
Z = 1228671
51 Z = 374499
07
XDOT = 8720
940136 XDOT = 2658
142553
YDOT = -11264
983754 feet/sec YDOT = -3433
567048 meter/sec
ZDOT = 19881
890925 ZDOT = 6060
000354
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 99115U 06252
81939306
00014500 00000-0 95600-4 0 9027
2 99115 51
6356 111
5717 0023371 355
4991 4
5967 15
90714097 46
Satellite: SHUTTLE
Catalog Number: 99115
Epoch time: 06252
81939306 = yrday
fracday
Element set: 902
Inclination: 51
6356 deg
RA of node: 111
5717 deg
Eccentricity:
0023371
Arg of perigee: 355
4991 deg
Mean anomaly: 4
5967 deg
Mean motion: 15
90714097 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 4
Checksum: 306
Coasting Arc #4 (begining on orbit 11)
---------------------------------------
Vector Time (GMT): 2006/253/07:07:50
017
Vector Time (MET): 000/15:52:54
017
Weight (LBS) : 248950
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4058581
62 A = 6706536
33 meter
Y = -4237421
51 meter E =
0017275
Z = -3224140
55 I = 51
93765
XDOT = 2094
325894 Wp = 222
49799
YDOT = 5667
361325 meter/sec RA = 108
28024 deg
ZDOT = -4809
828144 TA = 355
21076
MA = 355
22727
Ha = 181
540 n
mi
Hp = 171
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13315556
51 X = 4121325
78
Y = -13902301
54 feet Y = -4191685
58 meter
Z = -10577888
94 Z = -3204271
19
XDOT = 6871
147945 XDOT = 2054
162423
YDOT = 18593
705136 feet/sec YDOT = 5690
556371 meter/sec
ZDOT = -15780
276062 ZDOT = -4799
751769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15102145
97 X = -4603134
09
Y = -12002096
34 feet Y = -3658238
96 meter
Z = -10504505
61 Z = -3201773
31
XDOT = 16979
120142 XDOT = 5175
235819
YDOT = -7580
315637 feet/sec YDOT = -2310
480206 meter/sec
ZDOT = -15741
944396 ZDOT = -4798
144652
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 99115U 06253
32209355
00014500 00000-0 95600-4 0 9039
2 99115 51
6324 108
9289 0020225 233
3453 126
5855 15
81453931 124
Satellite: SHUTTLE
Catalog Number: 99115
Epoch time: 06253
32209355 = yrday
fracday
Element set: 903
Inclination: 51
6324 deg
RA of node: 108
9289 deg
Eccentricity:
0020225
Arg of perigee: 233
3453 deg
Mean anomaly: 126
5855 deg
Mean motion: 15
81453931 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 12
Checksum: 286
Coasting Arc #5 (begining on orbit 19)
---------------------------------------
Vector Time (GMT): 2006/253/18:27:14
738
Vector Time (MET): 001/03:12:18
738
Weight (LBS) : 248778
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3375769
74 A = 6711881
45 meter
Y = 5332966
59 meter E =
0003832
Z = 2290697
17 I = 51
94986
XDOT = -3206
370828 Wp = 198
99413
YDOT = -4378
435156 meter/sec RA = 105
83073 deg
ZDOT = 5467
232003 TA = 186
67889
MA = 186
68400
Ha = 181
454 n
mi
Hp = 174
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11075360
03 X = -3446280
68
Y = 17496609
55 feet Y = 5294822
73 meter
Z = 7515410
66 Z = 2274126
03
XDOT = -10519
589332 XDOT = -3183
731269
YDOT = -14364
944736 feet/sec YDOT = -4414
163707 meter/sec
ZDOT = 17937
112872 ZDOT = 5451
710562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16620857
33 X = -5066037
31
Y = -12387673
35 feet Y = -3775762
84 meter
Z = 7454461
33 Z = 2272119
81
XDOT = 14212
094176 XDOT = 4331
846305
YDOT = -8307
964922 feet/sec YDOT = -2532
267708 meter/sec
ZDOT = 17878
691364 ZDOT = 5449
425128
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 99115U 06253
82765735
00014500 00000-0 95600-4 0 9044
2 99115 51
6331 106
2993 0016625 241
8410 118
1077 15
80358346 206
Satellite: SHUTTLE
Catalog Number: 99115
Epoch time: 06253
82765735 = yrday
fracday
Element set: 904
Inclination: 51
6331 deg
RA of node: 106
2993 deg
Eccentricity:
0016625
Arg of perigee: 241
8410 deg
Mean anomaly: 118
1077 deg
Mean motion: 15
80358346 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 20
Checksum: 293
Coasting Arc #6 (begining on orbit 27)
---------------------------------------
Vector Time (GMT): 2006/254/06:36:50
402
Vector Time (MET): 001/15:21:54
402
Weight (LBS) : 248472
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3350038
10 A = 6717778
05 meter
Y = 5177934
90 meter E =
0005895
Z = 2653643
57 I = 51
94966
XDOT = -3114
892272 Wp = 35
53021
YDOT = -4706
062617 meter/sec RA = 103
22101 deg
ZDOT = 5249
313749 TA = 354
59718
MA = 354
60354
Ha = 182
458 n
mi
Hp = 180
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10990938
66 X = -3420580
52
Y = 16987975
40 feet Y = 5140078
60 meter
Z = 8706179
68 Z = 2637197
41
XDOT = -10219
462836 XDOT = -3087
537348
YDOT = -15439
837983 feet/sec YDOT = -4740
741922 meter/sec
ZDOT = 17222
157968 ZDOT = 5234
248103
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16719251
14 X = 5096027
75
Y = 11441532
25 feet Y = 3487379
03 meter
Z = 8645668
66 Z = 2635199
81
XDOT = -14847
760574 XDOT = -4525
597423
YDOT = 8723
155842 feet/sec YDOT = 2658
817901 meter/sec
ZDOT = 17165
389743 ZDOT = 5232
010794
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 99115U 06254
33363069
00014500 00000-0 95600-4 0 9056
2 99115 51
6319 103
6810 0010187 280
8234 79
1784 15
78001970 289
Satellite: SHUTTLE
Catalog Number: 99115
Epoch time: 06254
33363069 = yrday
fracday
Element set: 905
Inclination: 51
6319 deg
RA of node: 103
6810 deg
Eccentricity:
0010187
Arg of perigee: 280
8234 deg
Mean anomaly: 79
1784 deg
Mean motion: 15
78001970 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 28
Checksum: 298
Coasting Arc #7 (begining on orbit 28)
---------------------------------------
Vector Time (GMT): 2006/254/08:08:22
456
Vector Time (MET): 001/16:53:26
456
Weight (LBS) : 248254
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3383857
33 A = 6722279
49 meter
Y = 5099468
15 meter E =
0012653
Z = 2760391
54 I = 51
95042
XDOT = -3052
185536 Wp = 33
43299
YDOT = -4828
747863 meter/sec RA = 102
89492 deg
ZDOT = 5178
123982 TA = 358
04118
MA = 358
04613
Ha = 187
480 n
mi
Hp = 181
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11101894
13 X = -3454038
38
Y = 16730538
54 feet Y = 5061235
68 meter
Z = 9056402
68 Z = 2743781
98
XDOT = -10013
732074 XDOT = -3023
117561
YDOT = -15842
348631 feet/sec YDOT = -4862
716380 meter/sec
ZDOT = 16988
595741 ZDOT = 5163
367124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19659064
08 X = 5992082
73
Y = 4217546
09 feet Y = 1285508
05 meter
Z = 8995271
38 Z = 2741758
72
XDOT = -10707
880755 XDOT = -3263
762054
YDOT = 13791
496722 feet/sec YDOT = 4203
648201 meter/sec
ZDOT = 16932
960380 ZDOT = 5161
166324
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 99115U 06254
39702786
00014500 00000-0 95600-4 0 9066
2 99115 51
6331 103
3546 0010305 321
6398 38
4033 15
76328145 293
Satellite: SHUTTLE
Catalog Number: 99115
Epoch time: 06254
39702786 = yrday
fracday
Element set: 906
Inclination: 51
6331 deg
RA of node: 103
3546 deg
Eccentricity:
0010305
Arg of perigee: 321
6398 deg
Mean anomaly: 38
4033 deg
Mean motion: 15
76328145 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 29
Checksum: 292
Coasting Arc #8 (begining on orbit 28)
---------------------------------------
Vector Time (GMT): 2006/254/09:25:15
382
Vector Time (MET): 001/18:10:19
382
Weight (LBS) : 248169
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 412133
14 A = 6724595
06 meter
Y = 6306623
62 meter E =
0014678
Z = -2269035
57 I = 51
95523
XDOT = -4909
446942 Wp = 349
33637
YDOT = 2291
367400 meter/sec RA = 102
57796 deg
ZDOT = 5485
484752 TA = 345
25525
MA = 345
29801
Ha = 188
873 n
mi
Hp = 181
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1352142
83 X = 352603
63
Y = 20691022
38 feet Y = 6310899
40 meter
Z = -7444342
41 Z = -2267178
22
XDOT = -16107
109391 XDOT = -4961
352156
YDOT = 7517
609580 feet/sec YDOT = 2236
177218 meter/sec
ZDOT = 17996
997217 ZDOT = 5461
508311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14739992
99 X = 4492749
86
Y = -14587511
28 feet Y = -4446273
44 meter
Z = -7436534
99 Z = -2266655
87
XDOT = 15222
699509 XDOT = 4639
878810
YDOT = 6266
774792 feet/sec YDOT = 1910
112957 meter/sec
ZDOT = 17908
035173 ZDOT = 5458
369121
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 99115U 06254
39702620
00014500 00000-0 95600-4 0 9074
2 99115 51
6341 103
3549 0012227 325
9976 34
0403 15
75877614 293
Satellite: SHUTTLE
Catalog Number: 99115
Epoch time: 06254
39702620 = yrday
fracday
Element set: 907
Inclination: 51
6341 deg
RA of node: 103
3549 deg
Eccentricity:
0012227
Arg of perigee: 325
9976 deg
Mean anomaly: 34
0403 deg
Mean motion: 15
75877614 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 29
Checksum: 300
Coasting Arc #9 (begining on orbit 44)
---------------------------------------
Vector Time (GMT): 2006/255/09:30:16
736
Vector Time (MET): 002/18:15:20
736
Weight (LBS) : 248169
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4087985
79 A = 6714618
60 meter
Y = 691412
34 meter E =
0013616
Z = -5289039
98 I = 51
92692
XDOT = -1111
762613 Wp = 40
51908
YDOT = 7616
013049 meter/sec RA = 97
45008 deg
ZDOT = 146
638264 TA = 230
80694
MA = 230
92794
Ha = 189
036 n
mi
Hp = 181
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13412026
88 X = 4105643
90
Y = 2268413
20 feet Y = 737225
15 meter
Z = -17352493
39 Z = -5269137
51
XDOT = -3647
515135 XDOT = -1197
555638
YDOT = 24986
919452 feet/sec YDOT = 7603
101013 meter/sec
ZDOT = 481
096668 ZDOT = 141
028819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7571814
69 X = -2307889
12
Y = -11413409
46 feet Y = -3478807
20 meter
Z = -17278278
18 Z = -5266419
19
XDOT = 19907
548799 XDOT = 6067
820874
YDOT = -13853
712334 feet/sec YDOT = -4222
611519 meter/sec
ZDOT = 461
270545 ZDOT = 140
595262
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 99115U 06255
41164195
00014500 00000-0 95600-4 0 9088
2 99115 51
6341 98
1287 0012323 329
7310 30
3141 15
75926605 455
Satellite: SHUTTLE
Catalog Number: 99115
Epoch time: 06255
41164195 = yrday
fracday
Element set: 908
Inclination: 51
6341 deg
RA of node: 98
1287 deg
Eccentricity:
0012323
Arg of perigee: 329
7310 deg
Mean anomaly: 30
3141 deg
Mean motion: 15
75926605 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 45
Checksum: 286
Coasting Arc #10 (begining on orbit 60)
---------------------------------------
Vector Time (GMT): 2006/256/09:35:00
396
Vector Time (MET): 003/18:20:04
396
Weight (LBS) : 248169
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2134879
37 A = 6724198
87 meter
Y = -5903469
30 meter E =
0007348
Z = -2420139
36 I = 51
96165
XDOT = 4070
786707 Wp = 347
16167
YDOT = 3685
986247 meter/sec RA = 92
32693 deg
ZDOT = -5390
183563 TA = 220
01404
MA = 220
06820
Ha = 189
125 n
mi
Hp = 180
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7004197
42 X = 2212490
77
Y = -19368337
59 feet Y = -5879161
93 meter
Z = -7940089
75 Z = -2409579
59
XDOT = 13355
599431 XDOT = 4055
451623
YDOT = 12093
130732 feet/sec YDOT = 3731
422338 meter/sec
ZDOT = -17684
329274 ZDOT = -5370
444799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18638424
75 X = -5680991
86
Y = 8798323
45 feet Y = 2681728
99 meter
Z = -7901578
02 Z = -2408400
98
XDOT = -403
485869 XDOT = -122
982493
YDOT = -16700
109432 feet/sec YDOT = -5090
193355 meter/sec
ZDOT = -17610
305348 ZDOT = -5367
621070
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 99115U 06256
42623490
00014500 00000-0 95600-4 0 9099
2 99115 51
6342 92
9028 0012335 332
7277 27
3238 15
75916913 612
Satellite: SHUTTLE
Catalog Number: 99115
Epoch time: 06256
42623490 = yrday
fracday
Element set: 909
Inclination: 51
6342 deg
RA of node: 92
9028 deg
Eccentricity:
0012335
Arg of perigee: 332
7277 deg
Mean anomaly: 27
3238 deg
Mean motion: 15
75916913 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 61
Checksum: 304
Coasting Arc #11 (begining on orbit 76)
---------------------------------------
Vector Time (GMT): 2006/257/09:39:33
466
Vector Time (MET): 004/18:24:37
466
Weight (LBS) : 248169
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2784225
81 A = 6721988
47 meter
Y = -5204984
54 meter E =
0013527
Z = 3221043
48 I = 51
95510
XDOT = 3522
666868 Wp = 36
43047
YDOT = -4872
044326 meter/sec RA = 87
13540 deg
ZDOT = -4807
050560 TA = 106
10762
MA = 105
95865
Ha = 189
261 n
mi
Hp = 180
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9134599
11 X = -2741463
29
Y = -17076720
92 feet Y = -5235880
25 meter
Z = 10567727
95 Z = 3207621
48
XDOT = 11557
305997 XDOT = 3600
236739
YDOT = -15984
397395 feet/sec YDOT = -4832
218125 meter/sec
ZDOT = -15771
163255 ZDOT = -4789
749083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4794756
38 X = -1461441
74
Y = 18791879
73 feet Y = 5727764
94 meter
Z = 10517021
43 Z = 3205588
13
XDOT = -18020
712109 XDOT = -5492
713051
YDOT = 4231
317441 feet/sec YDOT = 1289
705556 meter/sec
ZDOT = -15707
390178 ZDOT = -4787
612526
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 99115U 06257
44080270
00014500 00000-0 95600-4 0 9107
2 99115 51
6344 87
6761 0012561 337
3405 22
7203 15
76011043 773
Satellite: SHUTTLE
Catalog Number: 99115
Epoch time: 06257
44080270 = yrday
fracday
Element set: 910
Inclination: 51
6344 deg
RA of node: 87
6761 deg
Eccentricity:
0012561
Arg of perigee: 337
3405 deg
Mean anomaly: 22
7203 deg
Mean motion: 15
76011043 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 77
Checksum: 273
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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