SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2008/152/21:02:11 970 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 69 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
163/12:58:17
648 -2
5 -0
0 3
0
010/15:56:05
677 -1
2 0
0 186
5
000/00:00:11
354 1
2 -3
0 180
5
163/13:26:14
808 1
2 1
5 1
5
010/16:24:02
838 0
9 0
0 186
6
000/00:00:05
676 -0
2 0
0 181
4
Coasting Arc #1 (Orbit 73)
---------------------------------------
Vector Time (GMT): 2008/157/10:39:24
000
Vector Time (MET): 004/13:37:12
030
Weight (LBS) : 213559
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3804333
72 A = 6712442
81 meter
Y = 1747040
56 meter E =
0002933
Z = 5248962
79 I = 51
93578
XDOT = -2363
243525 Wp = 304
61048
YDOT = -7297
655838 meter/sec RA = 76
25969 deg
ZDOT = 718
002721 TA = 138
60260
MA = 138
58037
Ha = 185
002 n
mi
Hp = 181
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12481409
85 X = -3849085
19
Y = 5731760
37 feet Y = 1704246
93 meter
Z = 17221006
53 Z = 5230373
01
XDOT = -7753
423638 XDOT = -2284
952276
YDOT = -23942
440412 feet/sec YDOT = -7323
645391 meter/sec
ZDOT = 2355
651972 ZDOT = 706
710601
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2915126
04 X = -888530
42
Y = 13512768
86 feet Y = 4118691
95 meter
Z = 17149602
12 Z = 5227198
73
XDOT = -22856
814255 XDOT = -6966
756985
YDOT = -7856
638188 feet/sec YDOT = -2394
703320 meter/sec
ZDOT = 2311
567704 ZDOT = 704
565836
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 32960U 08027A 08157
49275438
00020000 00000-0 70000-3 0 9004
2 32960 51
6385 76
6898 0005959 301
3515 58
7066 15
76755608 743
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08157
49275438 = yrday
fracday
Element set: 900
Inclination: 51
6385 deg
RA of node: 76
6898 deg
Eccentricity:
0005959
Arg of perigee: 301
3515 deg
Mean anomaly: 58
7066 deg
Mean motion: 15
76755608 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 74
Checksum: 327
Coasting Arc #2 (Orbit 89)
---------------------------------------
Vector Time (GMT): 2008/158/10:44:13
001
Vector Time (MET): 005/13:42:01
031
Weight (LBS) : 213559
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 534631
39 A = 6722675
49 meter
Y = 6389329
04 meter E =
0011993
Z = 1996063
96 I = 51
96183
XDOT = -5103
763860 Wp = 43
79043
YDOT = -1332
667604 meter/sec RA = 71
11999 deg
ZDOT = 5621
382353 TA = 338
38278
MA = 338
43337
Ha = 185
135 n
mi
Hp = 181
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1754039
98 X = 453448
70
Y = 20962365
61 feet Y = 6394853
26 meter
Z = 6548766
28 Z = 1998465
32
XDOT = -16744
632086 XDOT = -5115
789959
YDOT = -4372
269042 feet/sec YDOT = -1389
809214 meter/sec
ZDOT = 18442
855489 ZDOT = 5596
558897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18252110
04 X = 5563243
14
Y = 10451299
83 feet Y = 3185556
19 meter
Z = 6558550
08 Z = 1999046
07
XDOT = -12380
254299 XDOT = -3773
501510
YDOT = 10083
809194 feet/sec YDOT = 3073
545042 meter/sec
ZDOT = 18347
186922 ZDOT = 5592
222574
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 32960U 08027A 08158
50682933
00020000 00000-0 70000-3 0 9010
2 32960 51
6384 71
4604 0005921 305
7870 54
2743 15
76743085 908
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08158
50682933 = yrday
fracday
Element set: 901
Inclination: 51
6384 deg
RA of node: 71
4604 deg
Eccentricity:
0005921
Arg of perigee: 305
7870 deg
Mean anomaly: 54
2743 deg
Mean motion: 15
76743085 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 90
Checksum: 288
Coasting Arc #3 (Orbit 104)
---------------------------------------
Vector Time (GMT): 2008/159/10:49:09
341
Vector Time (MET): 006/13:46:57
371
Weight (LBS) : 213559
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4493189
92 A = 6719733
15 meter
Y = 3768850
20 meter E =
0004257
Z = -3275901
93 I = 51
94153
XDOT = -1459
205062 Wp = 359
73587
YDOT = 5876
692881 meter/sec RA = 65
92392 deg
ZDOT = 4763
711009 TA = 321
99514
MA = 322
02517
Ha = 185
308 n
mi
Hp = 181
253
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14741436
74 X = 4466625
72
Y = 12364994
08 feet Y = 3818947
68 meter
Z = -10747709
73 Z = -3254138
01
XDOT = -4787
418183 XDOT = -1547
951785
YDOT = 19280
488455 feet/sec YDOT = 5859
878147 meter/sec
ZDOT = 15628
973128 ZDOT = 4756
407740
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18356561
83 X = 5595080
05
Y = -5919494
30 feet Y = -1804261
86 meter
Z = -10663607
53 Z = -3250267
58
XDOT = 13271
385256 XDOT = 4045
118226
YDOT = 13074
809155 feet/sec YDOT = 3985
201831 meter/sec
ZDOT = 15601
353345 ZDOT = 4755
292499
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 32960U 08027A 08159
45751203
00020000 00000-0 70000-3 0 9023
2 32960 51
6386 66
5582 0005959 308
9607 51
1026 15
76756177 1057
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08159
45751203 = yrday
fracday
Element set: 902
Inclination: 51
6386 deg
RA of node: 66
5582 deg
Eccentricity:
0005959
Arg of perigee: 308
9607 deg
Mean anomaly: 51
1026 deg
Mean motion: 15
76756177 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 105
Checksum: 300
Coasting Arc #4 (Orbit 120)
---------------------------------------
Vector Time (GMT): 2008/160/10:54:00
397
Vector Time (MET): 007/13:51:48
427
Weight (LBS) : 213559
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3040607
73 A = 6712803
60 meter
Y = -2945945
78 meter E =
0011657
Z = -5218781
09 I = 51
90483
XDOT = 4375
198592 Wp = 59
25163
YDOT = 6257
017669 meter/sec RA = 60
80445 deg
ZDOT = -978
680613 TA = 201
42662
MA = 201
47546
Ha = 185
505 n
mi
Hp = 181
316
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9975747
14 X = 3098675
48
Y = -9665176
46 feet Y = -2911618
49 meter
Z = -17121985
20 Z = -5203869
34
XDOT = 14354
326090 XDOT = 4309
660678
YDOT = 20528
273191 feet/sec YDOT = 6305
577354 meter/sec
ZDOT = -3210
894400 ZDOT = -957
584274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3321447
91 X = -1012377
32
Y = -13559250
27 feet Y = -4132859
48 meter
Z = -17064825
23 Z = -5201358
73
XDOT = 23977
407374 XDOT = 7308
313768
YDOT = -1917
801581 feet/sec YDOT = -584
545922 meter/sec
ZDOT = -3129
149491 ZDOT = -953
764765
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 32960U 08027A 08160
47162643
00020000 00000-0 70000-3 0 9032
2 32960 51
6393 61
3292 0005997 312
4410 47
6246 15
76673032 1210
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08160
47162643 = yrday
fracday
Element set: 903
Inclination: 51
6393 deg
RA of node: 61
3292 deg
Eccentricity:
0005997
Arg of perigee: 312
4410 deg
Mean anomaly: 47
6246 deg
Mean motion: 15
76673032 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 121
Checksum: 272
Coasting Arc #5 (Orbit 136)
---------------------------------------
Vector Time (GMT): 2008/161/10:58:28
985
Vector Time (MET): 008/13:56:17
014
Weight (LBS) : 213559
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2532437
26 A = 6723393
35 meter
Y = -6003388
67 meter E =
0001968
Z = -1653803
78 I = 51
92549
XDOT = 5082
256552 Wp = 165
91290
YDOT = -558
341321 meter/sec RA = 55
65930 deg
ZDOT = -5758
843990 TA = 32
29825
MA = 32
28620
Ha = 185
608 n
mi
Hp = 181
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8308521
18 X = -2457084
36
Y = -19696157
05 feet Y = -6031286
29 meter
Z = -5425865
41 Z = -1665924
07
XDOT = 16674
070052 XDOT = 5116
097563
YDOT = -1831
828481 feet/sec YDOT = -501
318627 meter/sec
ZDOT = -18893
845113 ZDOT = -5734
072388
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21278605
19 X = -6485718
86
Y = -1917557
08 feet Y = -584471
40 meter
Z = -5473031
90 Z = -1668180
12
XDOT = 6105
873278 XDOT = 1861
070175
YDOT = -14131
588747 feet/sec YDOT = -4307
308250 meter/sec
ZDOT = -18798
523132 ZDOT = -5729
789851
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 32960U 08027A 08161
48573982
00020000 00000-0 70000-3 0 9047
2 32960 51
6397 56
1003 0006051 315
2098 44
8577 15
76668015 1379
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08161
48573982 = yrday
fracday
Element set: 904
Inclination: 51
6397 deg
RA of node: 56
1003 deg
Eccentricity:
0006051
Arg of perigee: 315
2098 deg
Mean anomaly: 44
8577 deg
Mean motion: 15
76668015 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 137
Checksum: 296
Coasting Arc #6 (Orbit 152)
---------------------------------------
Vector Time (GMT): 2008/162/11:03:08
314
Vector Time (MET): 009/14:00:56
344
Weight (LBS) : 213559
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5303001
56 A = 6718870
39 meter
Y = -1942440
83 meter E =
0009764
Z = 3637936
95 I = 51
89226
XDOT = -720
750298 Wp = 55
41689
YDOT = -6286
554154 meter/sec RA = 50
46377 deg
ZDOT = -4393
557804 TA = 81
09313
MA = 80
98260
Ha = 185
783 n
mi
Hp = 180
974
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17398299
07 X = -5298559
15
Y = -6372837
38 feet Y = -2001717
64 meter
Z = 11935488
67 Z = 3612185
55
XDOT = -2364
666331 XDOT = -629
056417
YDOT = -20625
177671 feet/sec YDOT = -6294
100769 meter/sec
ZDOT = -14414
559723 ZDOT = -4396
837254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13337415
25 X = -4065244
17
Y = 12953293
94 feet Y = 3948163
99 meter
Z = 11836185
49 Z = 3607669
34
XDOT = -18619
138810 XDOT = -5675
113509
YDOT = -5946
353879 feet/sec YDOT = -1812
448662 meter/sec
ZDOT = -14427
710273 ZDOT = -4397
566091
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 32960U 08027A 08162
49984178
00020000 00000-0 70000-3 0 9053
2 32960 51
6394 50
8715 0006070 319
8222 40
2493 15
76692869 1536
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08162
49984178 = yrday
fracday
Element set: 905
Inclination: 51
6394 deg
RA of node: 50
8715 deg
Eccentricity:
0006070
Arg of perigee: 319
8222 deg
Mean anomaly: 40
2493 deg
Mean motion: 15
76692869 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 153
Checksum: 309
Coasting Arc #7 (Orbit 168)
---------------------------------------
Vector Time (GMT): 2008/163/11:07:24
774
Vector Time (MET): 010/14:05:12
803
Weight (LBS) : 213559
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1430357
84 A = 6713691
69 meter
Y = 4190506
21 meter E =
0001965
Z = 5045508
30 I = 51
85526
XDOT = -6172
720793 Wp = 18
16715
YDOT = -4254
006769 meter/sec RA = 45
35012 deg
ZDOT = 1784
862876 TA = 54
71411
MA = 54
69573
Ha = 186
090 n
mi
Hp = 180
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4692775
05 X = -1501620
66
Y = 13748379
95 feet Y = 4174112
07 meter
Z = 16553504
91 Z = 5038387
01
XDOT = -20251
708638 XDOT = -6133
363609
YDOT = -13956
715123 feet/sec YDOT = -4322
813827 meter/sec
ZDOT = 5855
849331 ZDOT = 1754
970803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10658830
74 X = 3248811
61
Y = 9915890
01 feet Y = 3022363
28 meter
Z = 16526435
37 Z = 5037257
50
XDOT = -20217
765575 XDOT = -6162
374947
YDOT = 12174
242203 feet/sec YDOT = 3710
709023 meter/sec
ZDOT = 5740
416123 ZDOT = 1749
678834
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 32960U 08027A 08163
51400060
00020000 00000-0 70000-3 0 9061
2 32960 51
6402 45
6426 0006168 323
3833 36
6910 15
76613956 1693
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08163
51400060 = yrday
fracday
Element set: 906
Inclination: 51
6402 deg
RA of node: 45
6426 deg
Eccentricity:
0006168
Arg of perigee: 323
3833 deg
Mean anomaly: 36
6910 deg
Mean motion: 15
76613956 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 169
Checksum: 274
Coasting Arc #8 (Orbit 169)
---------------------------------------
Vector Time (GMT): 2008/163/12:58:23
325
Vector Time (MET): 010/15:56:11
354
Weight (LBS) : 213484
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5583276
94 A = 6721898
17 meter
Y = -2695743
18 meter E =
0010996
Z = 2591558
61 I = 51
88144
XDOT = 245
762702 Wp = 76
79014
YDOT = -5604
228436 meter/sec RA = 44
91784 deg
ZDOT = -5278
962996 TA = 73
85609
MA = 73
73508
Ha = 186
453 n
mi
Hp = 180
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18317837
71 X = -5565307
10
Y = -8844301
78 feet Y = -2758078
42 meter
Z = 8502488
89 Z = 2564478
29
XDOT = 806
308077 XDOT = 334
056121
YDOT = -18386
576234 feet/sec YDOT = -5600
985863 meter/sec
ZDOT = -17319
432401 ZDOT = -5277
555291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7513350
18 X = -2290069
13
Y = 18949410
80 feet Y = 5775780
41 meter
Z = 8398009
84 Z = 2559713
40
XDOT = -17022
592658 XDOT = -5188
486242
YDOT = 955
109774 feet/sec YDOT = 291
117459 meter/sec
ZDOT = -17314
476035 ZDOT = -5277
452296
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 32960U 08027A 08163
57738922
00020000 00000-0 70000-3 0 9079
2 32960 51
6403 45
3162 0006290 334
7137 25
3719 15
76619253 1707
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08163
57738922 = yrday
fracday
Element set: 907
Inclination: 51
6403 deg
RA of node: 45
3162 deg
Eccentricity:
0006290
Arg of perigee: 334
7137 deg
Mean anomaly: 25
3719 deg
Mean motion: 15
76619253 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 170
Checksum: 286
Coasting Arc #9 (Orbit 169)
---------------------------------------
Vector Time (GMT): 2008/163/13:26:17
646
Vector Time (MET): 010/16:24:05
676
Weight (LBS) : 213447
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2106292
35 A = 6713755
22 meter
Y = -3681773
16 meter E =
0012799
Z = -5214052
74 I = 51
84975
XDOT = 5931
543494 Wp = 54
58199
YDOT = 4803
232209 meter/sec RA = 44
84763 deg
ZDOT = -989
982044 TA = 205
97175
MA = 206
03604
Ha = 186
608 n
mi
Hp = 181
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6910407
99 X = 2172634
97
Y = -12079308
28 feet Y = -3657847
82 meter
Z = -17106472
26 Z = -5203659
64
XDOT = 19460
444535 XDOT = 5882
201315
YDOT = 15758
635856 feet/sec YDOT = 4869
286359 meter/sec
ZDOT = -3247
972585 ZDOT = -961
285788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13201034
58 X = -4023675
34
Y = -4555553
23 feet Y = -1388532
62 meter
Z = -17066764
22 Z = -5201949
73
XDOT = 11388
979374 XDOT = 3471
360913
YDOT = -21181
563005 feet/sec YDOT = -6456
140404 meter/sec
ZDOT = -3137
098265 ZDOT = -956
187551
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 32960U 08027A 08163
57738918
00020000 00000-0 70000-3 0 9085
2 32960 51
6391 45
3152 0006778 323
9555 36
1152 15
76339295 1703
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08163
57738918 = yrday
fracday
Element set: 908
Inclination: 51
6391 deg
RA of node: 45
3152 deg
Eccentricity:
0006778
Arg of perigee: 323
9555 deg
Mean anomaly: 36
1152 deg
Mean motion: 15
76339295 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 170
Checksum: 308
Coasting Arc #10 (Orbit 185)
---------------------------------------
Vector Time (GMT): 2008/164/13:30:45
301
Vector Time (MET): 011/16:28:33
331
Weight (LBS) : 213447
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4183987
19 A = 6724533
97 meter
Y = -5036299
27 meter E =
0001508
Z = -1531319
11 I = 51
86419
XDOT = 4621
527409 Wp = 125
46047
YDOT = -2078
310315 meter/sec RA = 39
70068 deg
ZDOT = -5796
844346 TA = 71
36955
MA = 71
35317
Ha = 186
715 n
mi
Hp = 181
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13726992
08 X = -4119920
61
Y = -16523291
57 feet Y = -5082728
60 meter
Z = -5024012
83 Z = -1551490
09
XDOT = 15162
491499 XDOT = 4672
584128
YDOT = -6818
603395 feet/sec YDOT = -2026
343526 meter/sec
ZDOT = -19018
518196 ZDOT = -5774
269063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12963337
46 X = -3951225
26
Y = 17105871
90 feet Y = 5213869
75 meter
Z = -5102078
91 Z = -1555113
65
XDOT = -8874
656144 XDOT = -2704
995193
YDOT = -12367
503334 feet/sec YDOT = -3769
615016 meter/sec
ZDOT = -18931
776184 ZDOT = -5770
405381
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 32960U 08027A 08164
59172038
00020000 00000-0 70000-3 0 9094
2 32960 51
6390 40
0885 0006734 326
7084 33
3656 15
76321989 1863
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08164
59172038 = yrday
fracday
Element set: 909
Inclination: 51
6390 deg
RA of node: 40
0885 deg
Eccentricity:
0006734
Arg of perigee: 326
7084 deg
Mean anomaly: 33
3656 deg
Mean motion: 15
76321989 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 186
Checksum: 307
Coasting Arc #11 (Orbit 201)
---------------------------------------
Vector Time (GMT): 2008/165/13:35:12
128
Vector Time (MET): 012/16:33:00
158
Weight (LBS) : 213447
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5501503
33 A = 6718985
71 meter
Y = -103131
67 meter E =
0011023
Z = 3855362
25 I = 51
82269
XDOT = -2797
169079 Wp = 45
22792
YDOT = -5866
716316 meter/sec RA = 34
50384 deg
ZDOT = -4133
639148 TA = 87
88878
MA = 87
76256
Ha = 186
825 n
mi
Hp = 181
014
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18049551
61 X = -5518670
04
Y = -338358
49 feet Y = -164749
17 meter
Z = 12648826
28 Z = 3828593
98
XDOT = -9177
063908 XDOT = -2711
277979
YDOT = -19247
756941 feet/sec YDOT = -5897
515021 meter/sec
ZDOT = -13561
808227 ZDOT = -4147
020145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4450864
92 X = 1356623
63
Y = 17569496
25 feet Y = 5355182
46 meter
Z = 12545764
58 Z = 3823949
04
XDOT = -14886
888483 XDOT = -4537
523610
YDOT = 13527
340547 feet/sec YDOT = 4123
133399 meter/sec
ZDOT = -13613
794041 ZDOT = -4149
484424
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 32960U 08027A 08165
60603617
00020000 00000-0 70000-3 0 9101
2 32960 51
6391 34
8601 0006961 330
5814 29
4957 15
76406347 2028
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08165
60603617 = yrday
fracday
Element set: 910
Inclination: 51
6391 deg
RA of node: 34
8601 deg
Eccentricity:
0006961
Arg of perigee: 330
5814 deg
Mean anomaly: 29
4957 deg
Mean motion: 15
76406347 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 202
Checksum: 279
Coasting Arc #12 (Orbit 217)
---------------------------------------
Vector Time (GMT): 2008/166/13:39:29
279
Vector Time (MET): 013/16:37:17
308
Weight (LBS) : 213447
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 226959
10 A = 6714982
42 meter
Y = 4568183
98 meter E =
0003699
Z = 4913407
04 I = 51
78257
XDOT = -7106
344511 Wp = 41
25563
YDOT = -2012
936842 meter/sec RA = 29
38965 deg
ZDOT = 2201
553709 TA = 27
43387
MA = 27
41435
Ha = 187
055 n
mi
Hp = 180
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 744616
47 X = 151991
38
Y = 14987480
25 feet Y = 4570301
99 meter
Z = 16120101
82 Z = 4914328
27
XDOT = -23314
778578 XDOT = -7094
002235
YDOT = -6604
123498 feet/sec YDOT = -2092
335408 meter/sec
ZDOT = 7222
945239 ZDOT = 2167
060359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14111420
61 X = 4301161
00
Y = -5091250
43 feet Y = -1551813
13 meter
Z = 16124009
37 Z = 4914598
06
XDOT = 287
887216 XDOT = 87
748023
YDOT = 23233
333079 feet/sec YDOT = 7081
519923 meter/sec
ZDOT = 7089
991749 ZDOT = 2161
029485
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 32960U 08027A 08166
62034503
00020000 00000-0 70000-3 0 9117
2 32960 51
6379 29
6318 0006842 335
7440 24
3401 15
76346850 2188
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08166
62034503 = yrday
fracday
Element set: 911
Inclination: 51
6379 deg
RA of node: 29
6318 deg
Eccentricity:
0006842
Arg of perigee: 335
7440 deg
Mean anomaly: 24
3401 deg
Mean motion: 15
76346850 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 218
Checksum: 275
Coasting Arc #13 (Orbit 233)
---------------------------------------
Vector Time (GMT): 2008/167/13:43:36
002
Vector Time (MET): 014/16:41:24
031
Weight (LBS) : 213447
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6003955
22 A = 6725330
66 meter
Y = 2988749
39 meter E =
0016498
Z = 334070
81 I = 51
79070
XDOT = -2401
799092 Wp = 25
56394
YDOT = 4138
389250 meter/sec RA = 24
21679 deg
ZDOT = 6046
104824 TA = 338
06614
MA = 338
13668
Ha = 187
036 n
mi
Hp = 180
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19698015
83 X = 5968465
46
Y = 9805608
24 feet Y = 3055690
56 meter
Z = 1096032
83 Z = 363152
67
XDOT = -7879
918281 XDOT = -2477
267889
YDOT = 13577
392553 feet/sec YDOT = 4111
107877 meter/sec
ZDOT = 19836
301916 ZDOT = 6034
254207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2722782
19 X = 829904
01
Y = -21828644
26 feet Y = -6653370
77 meter
Z = 1208228
17 Z = 368267
95
XDOT = 13867
708135 XDOT = 4226
877440
YDOT = 2840
933032 feet/sec YDOT = 865
916388 meter/sec
ZDOT = 19790
999636 ZDOT = 6032
296689
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 32960U 08027A 08167
63463495
00020000 00000-0 70000-3 0 9126
2 32960 51
6370 24
4034 0006802 338
4094 21
6783 15
76403291 2342
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08167
63463495 = yrday
fracday
Element set: 912
Inclination: 51
6370 deg
RA of node: 24
4034 deg
Eccentricity:
0006802
Arg of perigee: 338
4094 deg
Mean anomaly: 21
6783 deg
Mean motion: 15
76403291 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 234
Checksum: 278
Coasting Arc #14 (Orbit 248)
---------------------------------------
Vector Time (GMT): 2008/168/13:48:03
379
Vector Time (MET): 015/16:45:51
408
Weight (LBS) : 213447
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4359874
09 A = 6716282
75 meter
Y = -2304933
85 meter E =
0008032
Z = -4564298
93 I = 51
73253
XDOT = 5514
567540 Wp = 69
11368
YDOT = 4434
555687 meter/sec RA = 19
02832 deg
ZDOT = 3035
246455 TA = 230
98790
MA = 231
05944
Ha = 187
121 n
mi
Hp = 180
460
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14304048
86 X = 4407496
91
Y = -7562118
94 feet Y = -2255912
06 meter
Z = -14974734
04 Z = -4543003
27
XDOT = 18092
413190 XDOT = 5449
824982
YDOT = 14549
067213 feet/sec YDOT = 4495
860135 meter/sec
ZDOT = 9958
157662 ZDOT = 3061
880084
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12303035
60 X = -3749965
25
Y = -10624044
25 feet Y = -3238208
69 meter
Z = -14892921
64 Z = -4539362
52
XDOT = 6165
830972 XDOT = 1879
345280
YDOT = -21211
217385 feet/sec YDOT = -6465
179059 meter/sec
ZDOT = 10061
038040 ZDOT = 3066
604395
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 32960U 08027A 08168
58551754
00020000 00000-0 70000-3 0 9138
2 32960 51
6364 19
5015 0006645 342
3612 17
7320 15
76432374 2497
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08168
58551754 = yrday
fracday
Element set: 913
Inclination: 51
6364 deg
RA of node: 19
5015 deg
Eccentricity:
0006645
Arg of perigee: 342
3612 deg
Mean anomaly: 17
7320 deg
Mean motion: 15
76432374 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 249
Checksum: 285
SPACE SHUTTLE ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics 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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