Date:
June 9th 2007
SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2007/159/23:38:03 976 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 81 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : -0 14745
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
160/15:12:16
976 -13
3 38
0 38
2
000/15:34:13
000 27
1 4
0 129
3
000/00:00:27
624 -23
5 -0
0 98
9
161/01:10:54
799 117
6 144
8 144
8
001/01:32:50
822 -13
4 -0
0 180
2
000/00:01:36
421 -83
3 0
0 127
9
161/15:27:52
496 -66
0 82
5 82
5
001/15:49:48
520 9
6 -0
0 179
8
000/00:00:55
486 48
6 0
1 174
2
161/17:00:44
175 -6
9 9
2 9
2
001/17:22:40
198 0
2 -0
2 181
9
000/00:00:14
397 6
1 0
1 178
3
161/18:17:37
242 -2
6 2
4 2
8
001/18:39:33
266 0
9 0
4 182
9
000/00:00:12
532 0
9 1
4 179
6
Coasting Arc #1 (Orbit 3)
---------------------------------------
Vector Time (GMT): 2007/160/02:39:42
000
Vector Time (MET): 000/03:01:38
024
Weight (LBS) : 255388
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5669979
75 A = 6573977
99 meter
Y = 945772
09 meter E =
0055905
Z = 3131575
50 I = 51
81468
XDOT = 1690
384394 Wp = 356
89453
YDOT = -5863
177573 meter/sec RA = 145
15926 deg
ZDOT = 4890
544198 TA = 40
59634
MA = 40
18079
Ha = 124
729 n
mi
Hp = 85
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18602295
76 X = -5695337
31
Y = 3102926
81 feet Y = 882286
27 meter
Z = 10274197
85 Z = 3103969
10
XDOT = 5545
880557 XDOT = 1732
001350
YDOT = -19236
146893 feet/sec YDOT = -5844
060846 meter/sec
ZDOT = 16045
092514 ZDOT = 4898
856740
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11044971
29 X = -3366507
25
Y = -15356145
43 feet Y = -4680553
13 meter
Z = 10170059
51 Z = 3099834
14
XDOT = 18543
645562 XDOT = 5652
103167
YDOT = -2820
925501 feet/sec YDOT = -859
818093 meter/sec
ZDOT = 16075
764259 ZDOT = 4899
892946
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 31600U 07024A 07160
16595721
00014500 00000-0 95600-4 0 9009
2 31600 51
6262 145
7697 0057260 343
3666 16
5646 16
29669429 40
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07160
16595721 = yrday
fracday
Element set: 900
Inclination: 51
6262 deg
RA of node: 145
7697 deg
Eccentricity:
0057260
Arg of perigee: 343
3666 deg
Mean anomaly: 16
5646 deg
Mean motion: 16
29669429 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 4
Checksum: 289
Coasting Arc #2 (Orbit 11)
---------------------------------------
Vector Time (GMT): 2007/160/15:12:30
788
Vector Time (MET): 000/15:34:26
812
Weight (LBS) : 254427
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5401894
79 A = 6589645
76 meter
Y = -451880
32 meter E =
0045690
Z = -3750308
44 I = 51
82645
XDOT = -2449
997812 Wp = 320
38695
YDOT = 6068
621989 meter/sec RA = 142
26810 deg
ZDOT = -4197
857297 TA = 265
97593
MA = 266
49834
Ha = 129
254 n
mi
Hp = 98
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17722751
93 X = 5424760
54
Y = -1482546
99 feet Y = -391403
36 meter
Z = -12304161
56 Z = -3724010
35
XDOT = -8038
050563 XDOT = -2497
218410
YDOT = 19910
177129 feet/sec YDOT = 6040
987657 meter/sec
ZDOT = -13772
497694 ZDOT = -4209
873674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11419741
52 X = -3480737
22
Y = -13722834
63 feet Y = -4182719
99 meter
Z = -12204900
11 Z = -3720053
55
XDOT = 19874
776045 XDOT = 6057
831739
YDOT = -4067
158092 feet/sec YDOT = -1239
669786 meter/sec
ZDOT = -13817
135193 ZDOT = -4211
462807
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 31600U 07024A 07160
65646552
00014500 00000-0 95600-4 0 9013
2 31600 51
6315 143
0512 0048664 313
4431 46
2713 16
23099148 125
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07160
65646552 = yrday
fracday
Element set: 901
Inclination: 51
6315 deg
RA of node: 143
0512 deg
Eccentricity:
0048664
Arg of perigee: 313
4431 deg
Mean anomaly: 46
2713 deg
Mean motion: 16
23099148 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 12
Checksum: 248
Coasting Arc #3 (Orbit 18)
---------------------------------------
Vector Time (GMT): 2007/161/01:11:43
009
Vector Time (MET): 001/01:33:39
033
Weight (LBS) : 250823
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2211396
36 A = 6665440
07 meter
Y = -5275051
17 meter E =
0075592
Z = 3324203
85 I = 51
83919
XDOT = 6196
595333 Wp = 131
42695
YDOT = -380
007960 meter/sec RA = 139
91829 deg
ZDOT = -4707
346741 TA = 8
85165
MA = 8
71910
Ha = 180
232 n
mi
Hp = 127
923
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7255237
39 X = 2254013
41
Y = -17306598
31 feet Y = -5250108
10 meter
Z = 10906180
60 Z = 3335049
97
XDOT = 20330
037181 XDOT = 6223
248399
YDOT = -1246
745276 feet/sec YDOT = -310
631497 meter/sec
ZDOT = -15444
050987 ZDOT = -4677
178695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17888806
27 X = 5452508
15
Y = 5591633
29 feet Y = 1704329
83 meter
Z = 10946498
88 Z = 3336492
86
XDOT = 3504
596415 XDOT = 1068
200987
YDOT = 18913
815003 feet/sec YDOT = 5764
930813 meter/sec
ZDOT = -15330
162586 ZDOT = -4672
633556
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 31600U 07024A 07161
08820266
00014500 00000-0 95600-4 0 9028
2 31600 51
6296 140
6698 0066583 138
4720 222
1540 15
95935495 199
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07161
08820266 = yrday
fracday
Element set: 902
Inclination: 51
6296 deg
RA of node: 140
6698 deg
Eccentricity:
0066583
Arg of perigee: 138
4720 deg
Mean anomaly: 222
1540 deg
Mean motion: 15
95935495 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 19
Checksum: 287
Coasting Arc #4 (Orbit 27)
---------------------------------------
Vector Time (GMT): 2007/161/15:28:20
239
Vector Time (MET): 001/15:50:16
263
Weight (LBS) : 248793
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1950520
54 A = 6708626
27 meter
Y = 5465969
21 meter E =
0004221
Z = -3370551
41 I = 51
85398
XDOT = -6093
362392 Wp = 123
12338
YDOT = 700
175386 meter/sec RA = 136
77701 deg
ZDOT = 4663
574738 TA = 197
18931
MA = 197
20361
Ha = 179
802 n
mi
Hp = 174
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6399345
61 X = -1995064
58
Y = 17932969
86 feet Y = 5443929
88 meter
Z = -11058239
54 Z = -3380134
82
XDOT = -19991
346430 XDOT = -6123
387257
YDOT = 2297
163340 feet/sec YDOT = 631
933342 meter/sec
ZDOT = 15300
442055 ZDOT = 4633
899967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17816288
82 X = 5430404
83
Y = -6658512
98 feet Y = -2029514
76 meter
Z = -11093770
83 Z = -3381381
35
XDOT = 14168
288015 XDOT = 4318
494187
YDOT = 12615
214963 feet/sec YDOT = 3845
117521 meter/sec
ZDOT = 15188
451132 ZDOT = 4629
439905
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 31600U 07024A 07161
65171259
00014500 00000-0 95600-4 0 9033
2 31600 51
6313 137
6863 0002635 210
7413 149
3600 15
80536768 281
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07161
65171259 = yrday
fracday
Element set: 903
Inclination: 51
6313 deg
RA of node: 137
6863 deg
Eccentricity:
0002635
Arg of perigee: 210
7413 deg
Mean anomaly: 149
3600 deg
Mean motion: 15
80536768 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 28
Checksum: 264
Coasting Arc #5 (Orbit 28)
---------------------------------------
Vector Time (GMT): 2007/161/17:00:51
373
Vector Time (MET): 001/17:22:47
397
Weight (LBS) : 248567
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2446567
76 A = 6714657
69 meter
Y = 5513543
84 meter E =
0005545
Z = -2941979
83 I = 51
86096
XDOT = -5836
744518 Wp = 347
58701
YDOT = 94
551080 meter/sec RA = 136
44620 deg
ZDOT = 5034
633952 TA = 338
53979
MA = 338
56303
Ha = 181
934 n
mi
Hp = 178
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8026797
10 X = -2493688
41
Y = 18089054
61 feet Y = 5485948
34 meter
Z = -9652164
81 Z = -2953979
32
XDOT = -19149
424273 XDOT = -5861
825323
YDOT = 310
206957 feet/sec YDOT = 29
203496 meter/sec
ZDOT = 16517
827926 ZDOT = 5006
217788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15283574
95 X = 4658433
64
Y = -12537613
39 feet Y = -3821464
56 meter
Z = -9696816
03 Z = -2955589
53
XDOT = 16392
680833 XDOT = 4996
489118
YDOT = 7299
787184 feet/sec YDOT = 2224
975134 meter/sec
ZDOT = 16410
516565 ZDOT = 5001
925449
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 31600U 07024A 07161
71493731
00014500 00000-0 95600-4 0 9043
2 31600 51
6329 137
3583 0006604 304
4783 55
5758 15
78823496 292
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07161
71493731 = yrday
fracday
Element set: 904
Inclination: 51
6329 deg
RA of node: 137
3583 deg
Eccentricity:
0006604
Arg of perigee: 304
4783 deg
Mean anomaly: 55
5758 deg
Mean motion: 15
78823496 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 29
Checksum: 295
Coasting Arc #6 (Orbit 29)
---------------------------------------
Vector Time (GMT): 2007/161/18:17:43
508
Vector Time (MET): 001/18:39:39
532
Weight (LBS) : 248485
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2893305
04 A = 6707633
47 meter
Y = 2972538
17 meter E =
0008848
Z = -5277705
80 I = 51
83422
XDOT = -5545
672503 Wp = 59
84048
YDOT = 5345
910246 meter/sec RA = 136
19649 deg
ZDOT = -24
930914 TA = 209
89837
MA = 209
94894
Ha = 182
919 n
mi
Hp = 179
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9492470
59 X = 2885521
41
Y = 9752421
82 feet Y = 3004818
67 meter
Z = -17315307
74 Z = -5263668
56
XDOT = -18194
463591 XDOT = -5604
861161
YDOT = 17539
075610 feet/sec YDOT = 5283
624437 meter/sec
ZDOT = -81
794338 ZDOT = -52
015365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8218555
32 X = -2505015
66
Y = -10932414
85 feet Y = -3332200
05 meter
Z = -17261931
11 Z = -5261436
60
XDOT = 19551
559691 XDOT = 5959
315394
YDOT = -14385
970379 feet/sec YDOT = -4384
843772 meter/sec
ZDOT = -183
439847 ZDOT = -55
912466
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 31600U 07024A 07161
77823182
00014500 00000-0 95600-4 0 9057
2 31600 51
6331 137
0321 0008646 300
3817 59
6493 15
78383181 308
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07161
77823182 = yrday
fracday
Element set: 905
Inclination: 51
6331 deg
RA of node: 137
0321 deg
Eccentricity:
0008646
Arg of perigee: 300
3817 deg
Mean anomaly: 59
6493 deg
Mean motion: 15
78383181 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 30
Checksum: 265
Coasting Arc #7 (Orbit 45)
---------------------------------------
Vector Time (GMT): 2007/162/18:20:59
616
Vector Time (MET): 002/18:42:55
639
Weight (LBS) : 248485
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5370271
81 A = 6717018
68 meter
Y = -3138400
82 meter E =
0003550
Z = -2534786
89 I = 51
88551
XDOT = 717
358978 Wp = 291
84067
YDOT = 5527
957936 meter/sec RA = 131
05306 deg
ZDOT = -5317
329715 TA = 276
82232
MA = 276
86271
Ha = 183
014 n
mi
Hp = 179
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17619001
99 X = 5417247
35
Y = -10296590
63 feet Y = -3078142
45 meter
Z = -8316229
95 Z = -2508584
01
XDOT = 2353
539954 XDOT = 681
381764
YDOT = 18136
344935 feet/sec YDOT = 5535
771847 meter/sec
ZDOT = -17445
307465 ZDOT = -5313
931417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18611880
20 X = -5672901
09
Y = 8466232
53 feet Y = 2580507
67 meter
Z = -8217634
24 Z = -2504734
92
XDOT = 4
243871 XDOT = 1
293532
YDOT = -16933
808472 feet/sec YDOT = -5161
424822 meter/sec
ZDOT = -17431
810254 ZDOT = -5313
215765
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 31600U 07024A 07162
79124379
00014500 00000-0 95600-4 0 9063
2 31600 51
6329 131
7951 0008717 302
9855 57
0472 15
78372601 465
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07162
79124379 = yrday
fracday
Element set: 906
Inclination: 51
6329 deg
RA of node: 131
7951 deg
Eccentricity:
0008717
Arg of perigee: 302
9855 deg
Mean anomaly: 57
0472 deg
Mean motion: 15
78372601 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 46
Checksum: 288
Coasting Arc #8 (Orbit 61)
---------------------------------------
Vector Time (GMT): 2007/163/18:24:21
132
Vector Time (MET): 003/18:46:17
156
Weight (LBS) : 248485
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1566591
72 A = 6716098
82 meter
Y = -5904283
07 meter E =
0007214
Z = 2789908
29 I = 51
90145
XDOT = 5655
812096 Wp = 64
82511
YDOT = -937
729810 meter/sec RA = 125
84322 deg
ZDOT = -5147
088015 TA = 83
31037
MA = 83
22827
Ha = 183
129 n
mi
Hp = 179
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5139736
61 X = 1618881
48
Y = -19371007
46 feet Y = -5886489
77 meter
Z = 9153242
43 Z = 2797644
98
XDOT = 18555
813964 XDOT = 5690
872161
YDOT = -3076
541373 feet/sec YDOT = -874
347497 meter/sec
ZDOT = -16886
771703 ZDOT = -5119
526658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6410502
11 X = -1953921
04
Y = 18974593
62 feet Y = 5783456
14 meter
Z = 9181771
55 Z = 2798603
97
XDOT = -17433
888856 XDOT = -5313
849323
YDOT = 2252
199255 feet/sec YDOT = 686
470333 meter/sec
ZDOT = -16782
769980 ZDOT = -5115
388290
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 31600U 07024A 07163
80422967
00014500 00000-0 95600-4 0 9071
2 31600 51
6330 126
5574 0008722 308
3533 51
6848 15
78457640 621
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07163
80422967 = yrday
fracday
Element set: 907
Inclination: 51
6330 deg
RA of node: 126
5574 deg
Eccentricity:
0008722
Arg of perigee: 308
3533 deg
Mean anomaly: 51
6848 deg
Mean motion: 15
78457640 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 62
Checksum: 282
Coasting Arc #9 (Orbit 77)
---------------------------------------
Vector Time (GMT): 2007/164/18:27:57
008
Vector Time (MET): 004/18:49:53
032
Weight (LBS) : 248485
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3642837
54 A = 6707391
13 meter
Y = -1974334
46 meter E =
0006805
Z = 5277960
54 I = 51
88772
XDOT = 3832
062563 Wp = 322
53720
YDOT = -6683
732469 meter/sec RA = 120
70300 deg
ZDOT = 150
078153 TA = 126
07592
MA = 126
01288
Ha = 183
305 n
mi
Hp = 178
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11951566
73 X = -3646150
83
Y = -6477475
28 feet Y = -2015051
05 meter
Z = 17316143
50 Z = 5260255
01
XDOT = 12572
383737 XDOT = 3905
715765
YDOT = -21928
256133 feet/sec YDOT = -6640
510011 meter/sec
ZDOT = 492
382391 ZDOT = 168
872173
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11807385
75 X = 3598891
18
Y = 6906755
03 feet Y = 2105178
93 meter
Z = 17249024
19 Z = 5257502
57
XDOT = -12846
492645 XDOT = -3915
610958
YDOT = 20600
885811 feet/sec YDOT = 6279
149995 meter/sec
ZDOT = 562
608079 ZDOT = 171
482943
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 31600U 07024A 07164
81719118
00014500 00000-0 95600-4 0 9081
2 31600 51
6328 121
3193 0008703 311
3912 48
6504 15
78471515 781
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07164
81719118 = yrday
fracday
Element set: 908
Inclination: 51
6328 deg
RA of node: 121
3193 deg
Eccentricity:
0008703
Arg of perigee: 311
3912 deg
Mean anomaly: 48
6504 deg
Mean motion: 15
78471515 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 78
Checksum: 272
Coasting Arc #10 (Orbit 93)
---------------------------------------
Vector Time (GMT): 2007/165/18:30:56
869
Vector Time (MET): 005/18:52:52
893
Weight (LBS) : 248485
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4265717
10 A = 6716878
28 meter
Y = 4598180
61 meter E =
0012343
Z = 2380487
84 I = 51
93336
XDOT = -2328
973288 Wp = 35
16371
YDOT = -4968
588352 meter/sec RA = 115
56030 deg
ZDOT = 5420
080037 TA = 351
62520
MA = 351
64578
Ha = 183
394 n
mi
Hp = 178
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13995134
83 X = -4328332
70
Y = 15085894
40 feet Y = 4550174
59 meter
Z = 7809999
49 Z = 2359613
73
XDOT = -7640
988477 XDOT = -2299
624316
YDOT = -16301
142886 feet/sec YDOT = -4994
444364 meter/sec
ZDOT = 17782
414821 ZDOT = 5408
836095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14123808
17 X = 4304936
73
Y = -15006119
92 feet Y = -4573865
35 meter
Z = 7731656
25 Z = 2356608
83
XDOT = 6553
599536 XDOT = 1997
537139
YDOT = 15314
846481 feet/sec YDOT = 4667
965207 meter/sec
ZDOT = 17739
360130 ZDOT = 5406
956968
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 31600U 07024A 07165
83012597
00014500 00000-0 95600-4 0 9092
2 31600 51
6322 116
0808 0008827 314
3677 45
6765 15
78533893 949
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07165
83012597 = yrday
fracday
Element set: 909
Inclination: 51
6322 deg
RA of node: 116
0808 deg
Eccentricity:
0008827
Arg of perigee: 314
3677 deg
Mean anomaly: 45
6765 deg
Mean motion: 15
78533893 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 94
Checksum: 301
Coasting Arc #11 (Orbit 108)
---------------------------------------
Vector Time (GMT): 2007/166/18:34:37
189
Vector Time (MET): 006/18:56:33
213
Weight (LBS) : 248485
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 93319
94 A = 6715770
45 meter
Y = 6089623
45 meter E =
0008912
Z = -2816770
50 I = 51
94073
XDOT = -5200
130033 Wp = 348
53533
YDOT = 2453
285360 meter/sec RA = 110
35214 deg
ZDOT = 5137
313725 TA = 339
24717
MA = 339
28333
Ha = 183
463 n
mi
Hp = 178
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 306167
79 X = 38966
77
Y = 19979079
55 feet Y = 6090362
97 meter
Z = -9241373
03 Z = -2816447
92
XDOT = -17060
794071 XDOT = -5252
106889
YDOT = 8048
836482 feet/sec YDOT = 2394
899105 meter/sec
ZDOT = 16854
703821 ZDOT = 5111
925784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -909154
61 X = -277110
33
Y = -19961616
66 feet Y = -6084300
76 meter
Z = -9239460
59 Z = -2816187
59
XDOT = 15470
479430 XDOT = 4715
402130
YDOT = -8452
915383 feet/sec YDOT = -2576
448609 meter/sec
ZDOT = 16759
043868 ZDOT = 5108
156571
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 31600U 07024A 07166
77973060
00014500 00000-0 95600-4 0 9109
2 31600 51
6317 111
1698 0008788 317
8009 42
2479 15
78554863 1091
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07166
77973060 = yrday
fracday
Element set: 910
Inclination: 51
6317 deg
RA of node: 111
1698 deg
Eccentricity:
0008788
Arg of perigee: 317
8009 deg
Mean anomaly: 42
2479 deg
Mean motion: 15
78554863 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 109
Checksum: 300
Coasting Arc #12 (Orbit 124)
---------------------------------------
Vector Time (GMT): 2007/167/18:38:19
069
Vector Time (MET): 007/19:00:15
093
Weight (LBS) : 248485
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4024151
98 A = 6707016
88 meter
Y = 979544
83 meter E =
0012007
Z = -5283874
32 I = 51
91957
XDOT = -1948
245375 Wp = 54
12128
YDOT = 7450
417296 meter/sec RA = 105
21317 deg
ZDOT = -95
845145 TA = 214
93339
MA = 215
01224
Ha = 183
567 n
mi
Hp = 178
095
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13202598
35 X = 4038578
41
Y = 3213729
76 feet Y = 1024583
50 meter
Z = -17335545
68 Z = -5264289
90
XDOT = -6391
881151 XDOT = -2030
866766
YDOT = 24443
626298 feet/sec YDOT = 7428
190376 meter/sec
ZDOT = -314
452577 ZDOT = -105
508879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13470508
07 X = -4105810
86
Y = -2397227
57 feet Y = -730674
96 meter
Z = -17261417
05 Z = -5261279
92
XDOT = 4713
530393 XDOT = 1436
684064
YDOT = -23805
362004 feet/sec YDOT = -7255
874339 meter/sec
ZDOT = -350
130926 ZDOT = -106
719906
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 31600U 07024A 07167
79261668
00014500 00000-0 95600-4 0 9117
2 31600 51
6308 105
9314 0008687 321
8890 38
1660 15
78602427 1252
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07167
79261668 = yrday
fracday
Element set: 911
Inclination: 51
6308 deg
RA of node: 105
9314 deg
Eccentricity:
0008687
Arg of perigee: 321
8890 deg
Mean anomaly: 38
1660 deg
Mean motion: 15
78602427 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 125
Checksum: 289
Coasting Arc #13 (Orbit 140)
---------------------------------------
Vector Time (GMT): 2007/168/18:41:31
079
Vector Time (MET): 008/19:03:27
103
Weight (LBS) : 248485
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2982594
33 A = 6716240
28 meter
Y = -5461368
34 meter E =
0003909
Z = -2532120
86 I = 51
95746
XDOT = 3457
423766 Wp = 346
50488
YDOT = 4359
538905 meter/sec RA = 100
07370 deg
ZDOT = -5324
941890 TA = 222
08765
MA = 222
11768
Ha = 183
612 n
mi
Hp = 177
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9785414
47 X = 3055684
56
Y = -17917875
12 feet Y = -5427638
65 meter
Z = -8307483
15 Z = -2517455
01
XDOT = 11343
253824 XDOT = 3434
332400
YDOT = 14302
949162 feet/sec YDOT = 4398
036527 meter/sec
ZDOT = -17470
281790 ZDOT = -5308
201235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8140472
32 X = -2481215
96
Y = 18746867
79 feet Y = 5714045
30 meter
Z = -8252667
46 Z = -2515413
04
XDOT = -11341
907268 XDOT = -3457
013335
YDOT = -12595
414890 feet/sec YDOT = -3839
082458 meter/sec
ZDOT = -17406
511417 ZDOT = -5305
504680
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 31600U 07024A 07168
80547674
00014500 00000-0 95600-4 0 9125
2 31600 51
6309 100
6938 0008720 325
6374 34
4227 15
78638849 1417
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07168
80547674 = yrday
fracday
Element set: 912
Inclination: 51
6309 deg
RA of node: 100
6938 deg
Eccentricity:
0008720
Arg of perigee: 325
6374 deg
Mean anomaly: 34
4227 deg
Mean motion: 15
78638849 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 141
Checksum: 292
Coasting Arc #14 (Orbit 156)
---------------------------------------
Vector Time (GMT): 2007/169/18:45:03
667
Vector Time (MET): 009/19:06:59
691
Weight (LBS) : 248485
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1593534
95 A = 6715775
35 meter
Y = -5950261
86 meter E =
0009976
Z = 2674520
80 I = 51
96029
XDOT = 4409
690785 Wp = 61
86424
YDOT = -3541
221786 meter/sec RA = 94
86625 deg
ZDOT = -5231
826388 TA = 87
75968
MA = 87
64545
Ha = 183
694 n
mi
Hp = 177
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5228133
04 X = -1539936
16
Y = -19521856
51 feet Y = -5967765
54 meter
Z = 8774674
54 Z = 2666908
80
XDOT = 14467
489453 XDOT = 4474
338906
YDOT = -11618
181713 feet/sec YDOT = -3491
595660 meter/sec
ZDOT = -17164
784737 ZDOT = -5210
247884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7667877
33 X = 2337169
01
Y = 18712451
60 feet Y = 5703555
25 meter
Z = 8745226
28 Z = 2665544
97
XDOT = -11638
050059 XDOT = -3547
277658
YDOT = 12782
630100 feet/sec YDOT = 3896
145654 meter/sec
ZDOT = -17083
616266 ZDOT = -5207
086238
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 31600U 07024A 07169
81831802
00014500 00000-0 95600-4 0 9137
2 31600 51
6311 95
4545 0008840 328
5090 31
5545 15
78684089 1570
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07169
81831802 = yrday
fracday
Element set: 913
Inclination: 51
6311 deg
RA of node: 95
4545 deg
Eccentricity:
0008840
Arg of perigee: 328
5090 deg
Mean anomaly: 31
5545 deg
Mean motion: 15
78684089 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 157
Checksum: 287
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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