Date:
September 14th 2006
SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2006/252/15:14:54 972 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 12 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 16339
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
265/19:25:00
000 0
0 0
0 0
0
013/04:10:05
028 0
0 0
0 190
0
000/00:00:00
000 0
0 0
0 178
2
Coasting Arc #1 (Orbit 51)
---------------------------------------
Vector Time (GMT): 2006/255/19:25:00
000
Vector Time (MET): 003/04:10:05
028
Weight (LBS) : 210939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4035357
42 A = 6714769
38 meter
Y = -1089492
66 meter E =
0011449
Z = 5258572
19 I = 51
92818
XDOT = 1205
908285 Wp = 345
86646
YDOT = -7580
117193 meter/sec RA = 95
32663 deg
ZDOT = -634
506776 TA = 110
20225
MA = 110
07909
Ha = 188
798 n
mi
Hp = 181
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13239361
63 X = -4048406
50
Y = -3574451
00 feet Y = -1134739
57 meter
Z = 17252533
43 Z = 5238936
55
XDOT = 3956
392012 XDOT = 1293
753058
YDOT = -24869
150897 feet/sec YDOT = -7566
125981 meter/sec
ZDOT = -2081
715145 ZDOT = -628
435331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 680351
11 X = 207371
02
Y = -13788314
78 feet Y = -4202678
34 meter
Z = 17179255
04 Z = 5236236
94
XDOT = 24140
944328 XDOT = 7358
159831
YDOT = -1419
046438 feet/sec YDOT = -432
525354 meter/sec
ZDOT = -2060
158065 ZDOT = -627
936178
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 29391U 06036A 06255
85555484
00014500 00000-0 95600-4 0 9007
2 29391 51
6335 95
8413 0011240 331
2175 28
8367 15
75918432 525
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06255
85555484 = yrday
fracday
Element set: 900
Inclination: 51
6335 deg
RA of node: 95
8413 deg
Eccentricity:
0011240
Arg of perigee: 331
2175 deg
Mean anomaly: 28
8367 deg
Mean motion: 15
75918432 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 52
Checksum: 300
Coasting Arc #2 (Orbit 67)
---------------------------------------
Vector Time (GMT): 2006/256/19:29:25
539
Vector Time (MET): 004/04:14:30
568
Weight (LBS) : 210939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2118669
88 A = 6723571
81 meter
Y = 5778490
07 meter E =
0015642
Z = 2680603
05 I = 51
95927
XDOT = -4081
359252 Wp = 33
79420
YDOT = -3925
568547 meter/sec RA = 90
21088 deg
ZDOT = 5234
684410 TA = 356
67097
MA = 356
68137
Ha = 188
944 n
mi
Hp = 180
927
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6951016
67 X = -2196218
78
Y = 18958300
77 feet Y = 5754338
50 meter
Z = 8794629
42 Z = 2670122
43
XDOT = -13390
286261 XDOT = -4062
541596
YDOT = -12879
161898 feet/sec YDOT = -3971
152123 meter/sec
ZDOT = 17174
161450 ZDOT = 5214
902610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20098802
54 X = -6126115
01
Y = -2107856
82 feet Y = -642474
76 meter
Z = 8756391
01 Z = 2668947
98
XDOT = 9002
329658 XDOT = 2743
910080
YDOT = -14778
857638 feet/sec YDOT = -4504
595808 meter/sec
ZDOT = 17099
943781 ZDOT = 5212
062864
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 29391U 06036A 06256
87015931
00014500 00000-0 95600-4 0 9019
2 29391 51
6334 90
6157 0011238 335
4660 24
5968 15
75934062 688
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06256
87015931 = yrday
fracday
Element set: 901
Inclination: 51
6334 deg
RA of node: 90
6157 deg
Eccentricity:
0011238
Arg of perigee: 335
4660 deg
Mean anomaly: 24
5968 deg
Mean motion: 15
75934062 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 68
Checksum: 305
Coasting Arc #3 (Orbit 82)
---------------------------------------
Vector Time (GMT): 2006/257/19:34:41
705
Vector Time (MET): 005/04:19:46
734
Weight (LBS) : 210939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2660378
43 A = 6723288
67 meter
Y = 5506177
38 meter E =
0013097
Z = -2775964
51 I = 51
95686
XDOT = -3678
916307 Wp = 359
76231
YDOT = 4377
333315 meter/sec RA = 85
01833 deg
ZDOT = 5169
508153 TA = 328
57903
MA = 328
65721
Ha = 189
121 n
mi
Hp = 180
648
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8728275
70 X = 2612029
05
Y = 18064886
43 feet Y = 5535688
43 meter
Z = -9107495
12 Z = -2763157
55
XDOT = -12069
935390 XDOT = -3752
755007
YDOT = 14361
329774 feet/sec YDOT = 4335
736238 meter/sec
ZDOT = 16960
328585 ZDOT = 5151
456864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14808052
19 X = -4513494
31
Y = 13569259
33 feet Y = 4135910
24 meter
Z = -9059038
45 Z = -2761194
92
XDOT = -16245
881975 XDOT = -4951
744826
YDOT = -6478
563852 feet/sec YDOT = -1974
666262 meter/sec
ZDOT = 16893
691113 ZDOT = 5149
197051
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 29391U 06036A 06257
82132541
00014500 00000-0 95600-4 0 9023
2 29391 51
6330 85
7171 0011427 338
8473 21
2217 15
75954410 831
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06257
82132541 = yrday
fracday
Element set: 902
Inclination: 51
6330 deg
RA of node: 85
7171 deg
Eccentricity:
0011427
Arg of perigee: 338
8473 deg
Mean anomaly: 21
2217 deg
Mean motion: 15
75954410 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 83
Checksum: 282
Coasting Arc #4 (Orbit 98)
---------------------------------------
Vector Time (GMT): 2006/258/19:39:38
672
Vector Time (MET): 006/04:24:43
700
Weight (LBS) : 210939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3968757
83 A = 6714522
75 meter
Y = -1278912
02 meter E =
0016600
Z = -5273551
59 I = 51
92321
XDOT = 1731
183001 Wp = 43
76622
YDOT = 7481
233390 meter/sec RA = 79
89888 deg
ZDOT = -500
667800 TA = 221
42977
MA = 221
55575
Ha = 189
225 n
mi
Hp = 180
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13020859
03 X = 4008396
39
Y = -4195905
57 feet Y = -1234261
77 meter
Z = -17301678
43 Z = -5254175
23
XDOT = 5679
734256 XDOT = 1649
740938
YDOT = 24544
728971 feet/sec YDOT = 7500
157236 meter/sec
ZDOT = -1642
610894 ZDOT = -492
455215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8200681
08 X = 2499567
59
Y = 11062711
71 feet Y = 3371914
53 meter
Z = -17229675
26 Z = -5251605
02
XDOT = -20592
931714 XDOT = -6276
725586
YDOT = 12700
924514 feet/sec YDOT = 3871
241792 meter/sec
ZDOT = -1610
998368 ZDOT = -491
032302
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 29391U 06036A 06258
83587560
00014500 00000-0 95600-4 0 9031
2 29391 51
6324 80
4908 0011488 342
8066 17
2708 15
75988666 991
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06258
83587560 = yrday
fracday
Element set: 903
Inclination: 51
6324 deg
RA of node: 80
4908 deg
Eccentricity:
0011488
Arg of perigee: 342
8066 deg
Mean anomaly: 17
2708 deg
Mean motion: 15
75988666 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 99
Checksum: 340
Coasting Arc #5 (Orbit 114)
---------------------------------------
Vector Time (GMT): 2006/259/19:44:20
324
Vector Time (MET): 007/04:29:25
353
Weight (LBS) : 210939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -189091
83 A = 6724682
47 meter
Y = -6443255
55 meter E =
0006176
Z = -1930239
48 I = 51
95201
XDOT = 4997
610428 Wp = 17
86495
YDOT = 1544
073652 meter/sec RA = 74
76527 deg
ZDOT = -5642
779905 TA = 183
49775
MA = 183
50207
Ha = 189
278 n
mi
Hp = 179
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -620380
03 X = -107574
94
Y = -21139289
88 feet Y = -6444916
00 meter
Z = -6332806
69 Z = -1930960
30
XDOT = 16396
359673 XDOT = 5007
365281
YDOT = 5065
858438 feet/sec YDOT = 1600
074039 meter/sec
ZDOT = -18513
057432 ZDOT = -5618
477953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19529245
09 X = 5952513
90
Y = -8112822
89 feet Y = -2472788
42 meter
Z = -6336369
57 Z = -1931325
44
XDOT = 582
987025 XDOT = 177
694445
YDOT = 15794
367735 feet/sec YDOT = 4814
123286 meter/sec
ZDOT = -18422
315848 ZDOT = -5615
121871
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 29391U 06036A 06259
85039672
00014500 00000-0 95600-4 0 9041
2 29391 51
6325 75
2639 0011564 347
6774 12
4105 15
76062676 1151
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06259
85039672 = yrday
fracday
Element set: 904
Inclination: 51
6325 deg
RA of node: 75
2639 deg
Eccentricity:
0011564
Arg of perigee: 347
6774 deg
Mean anomaly: 12
4105 deg
Mean motion: 15
76062676 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 115
Checksum: 310
Coasting Arc #6 (Orbit 130)
---------------------------------------
Vector Time (GMT): 2006/260/19:49:00
468
Vector Time (MET): 008/04:34:05
496
Weight (LBS) : 210939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4351414
70 A = 6720661
32 meter
Y = -3677300
26 meter E =
0015995
Z = 3567781
77 I = 51
93040
XDOT = 1466
524844 Wp = 39
91340
YDOT = -6094
994812 meter/sec RA = 69
57396 deg
ZDOT = -4470
455466 TA = 97
69622
MA = 97
51455
Ha = 189
389 n
mi
Hp = 179
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14276294
96 X = -4327258
31
Y = -12064633
41 feet Y = -3725876
89 meter
Z = 11705320
77 Z = 3546701
41
XDOT = 4811
433214 XDOT = 1556
359799
YDOT = -19996
702138 feet/sec YDOT = -6078
074946 meter/sec
ZDOT = -14666
848642 ZDOT = -4463
113048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5462127
50 X = 1664856
46
Y = -17926994
82 feet Y = -5464148
02 meter
Z = 11626286
23 Z = 3543692
04
XDOT = 19003
716619 XDOT = 5792
332825
YDOT = -3753
845226 feet/sec YDOT = -1144
172025 meter/sec
ZDOT = -14640
325432 ZDOT = -4462
371192
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 29391U 06036A 06260
86488748
00014500 00000-0 95600-4 0 9057
2 29391 51
6327 70
0367 0011768 350
8978 9
1971 15
76128060 1314
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06260
86488748 = yrday
fracday
Element set: 905
Inclination: 51
6327 deg
RA of node: 70
0367 deg
Eccentricity:
0011768
Arg of perigee: 350
8978 deg
Mean anomaly: 9
1971 deg
Mean motion: 15
76128060 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 131
Checksum: 319
Coasting Arc #7 (Orbit 146)
---------------------------------------
Vector Time (GMT): 2006/261/19:53:39
648
Vector Time (MET): 009/04:38:44
676
Weight (LBS) : 210939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2772756
07 A = 6714976
30 meter
Y = 3415346
10 meter E =
0009280
Z = 5068360
94 I = 51
89969
XDOT = -4397
836143 Wp = 20
21198
YDOT = -6096
073207 meter/sec RA = 64
46498 deg
ZDOT = 1709
551799 TA = 53
46238
MA = 53
37698
Ha = 189
611 n
mi
Hp = 179
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9096968
72 X = -2835402
14
Y = 11205203
74 feet Y = 3383955
95 meter
Z = 16628480
77 Z = 5054738
83
XDOT = -14428
596270 XDOT = -4337
573563
YDOT = -20000
240182 feet/sec YDOT = -6144
967333 meter/sec
ZDOT = 5608
765744 ZDOT = 1688
333708
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14055851
47 X = -4284223
53
Y = -3523381
97 feet Y = -1073926
83 meter
Z = 16578197
20 Z = 5053034
51
XDOT = 11653
003211 XDOT = 3551
835379
YDOT = -20590
701126 feet/sec YDOT = -6276
045703 meter/sec
ZDOT = 5528
885450 ZDOT = 1685
204285
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 29391U 06036A 06261
87936444
00014500 00000-0 95600-4 0 9061
2 29391 51
6323 64
8095 0011722 355
5556 4
5502 15
76124258 1474
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06261
87936444 = yrday
fracday
Element set: 906
Inclination: 51
6323 deg
RA of node: 64
8095 deg
Eccentricity:
0011722
Arg of perigee: 355
5556 deg
Mean anomaly: 4
5502 deg
Mean motion: 15
76124258 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 147
Checksum: 303
Coasting Arc #8 (Orbit 162)
---------------------------------------
Vector Time (GMT): 2006/262/19:58:38
365
Vector Time (MET): 010/04:43:43
393
Weight (LBS) : 210939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2685162
98 A = 6725813
04 meter
Y = 6067951
71 meter E =
0022789
Z = 1005737
41 I = 51
92234
XDOT = -4768
695697 Wp = 29
86220
YDOT = 1115
912745 meter/sec RA = 59
30992 deg
ZDOT = 5961
104912 TA = 341
11236
MA = 341
19676
Ha = 189
844 n
mi
Hp = 179
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8809589
84 X = 2612152
44
Y = 19907978
06 feet Y = 6097602
05 meter
Z = 3299663
40 Z = 1018604
35
XDOT = -15645
327090 XDOT = -4809
789997
YDOT = 3661
131053 feet/sec YDOT = 1062
299858 meter/sec
ZDOT = 19557
430813 ZDOT = 5937
838906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13594957
76 X = -4143743
13
Y = 16993804
49 feet Y = 5179711
61 meter
Z = 3348428
68 Z = 1020601
06
XDOT = -9285
014324 XDOT = -2830
072366
YDOT = -11288
618271 feet/sec YDOT = -3440
770849 meter/sec
ZDOT = 19470
904538 ZDOT = 5934
731703
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 29391U 06036A 06262
89383204
00014500 00000-0 95600-4 0 9075
2 29391 51
6323 59
5821 0012019
2594 359
8574 15
76083312 1636
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06262
89383204 = yrday
fracday
Element set: 907
Inclination: 51
6323 deg
RA of node: 59
5821 deg
Eccentricity:
0012019
Arg of perigee:
2594 deg
Mean anomaly: 359
8574 deg
Mean motion: 15
76083312 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 163
Checksum: 299
Coasting Arc #9 (Orbit 177)
---------------------------------------
Vector Time (GMT): 2006/263/20:03:03
429
Vector Time (MET): 011/04:48:08
458
Weight (LBS) : 210939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5037878
20 A = 6718228
66 meter
Y = 1255538
35 meter E =
0012447
Z = -4265227
06 I = 51
88272
XDOT = 1358
478074 Wp = 43
52210
YDOT = 6679
092170 meter/sec RA = 54
12546 deg
ZDOT = 3585
647468 TA = 262
69035
MA = 262
83184
Ha = 189
903 n
mi
Hp = 178
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16528471
79 X = 5044168
18
Y = 4119220
30 feet Y = 1311969
76 meter
Z = -13993527
10 Z = -4240737
90
XDOT = 4456
949061 XDOT = 1266
192456
YDOT = 21913
032054 feet/sec YDOT = 6693
783202 meter/sec
ZDOT = 11763
935262 ZDOT = 3592
022517
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4622432
98 X = 1408917
57
Y = 16472440
66 feet Y = 5020799
91 meter
Z = -13902121
01 Z = -4237366
48
XDOT = -15680
670118 XDOT = -4779
468252
YDOT = 14307
629620 feet/sec YDOT = 4360
965508 meter/sec
ZDOT = 11788
598052 ZDOT = 3593
164686
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 29391U 06036A 06263
84488092
00014500 00000-0 95600-4 0 9083
2 29391 51
6334 54
6815 0011950 3
5329 356
5918 15
76150238 1786
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06263
84488092 = yrday
fracday
Element set: 908
Inclination: 51
6334 deg
RA of node: 54
6815 deg
Eccentricity:
0011950
Arg of perigee: 3
5329 deg
Mean anomaly: 356
5918 deg
Mean motion: 15
76150238 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 178
Checksum: 317
Coasting Arc #10 (Orbit 193)
---------------------------------------
Vector Time (GMT): 2006/264/20:07:31
985
Vector Time (MET): 012/04:52:37
014
Weight (LBS) : 210939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 696049
97 A = 6716493
12 meter
Y = -4792136
01 meter E =
0019466
Z = -4671372
39 I = 51
85969
XDOT = 6135
752580 Wp = 37
16178
YDOT = 3665
929616 meter/sec RA = 49
02005 deg
ZDOT = -2837
388608 TA = 204
81378
MA = 204
90752
Ha = 189
870 n
mi
Hp = 178
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2283628
52 X = 772334
28
Y = -15722231
01 feet Y = -4783917
34 meter
Z = -15326024
89 Z = -4667805
45
XDOT = 20130
421849 XDOT = 6108
042674
YDOT = 12027
328136 feet/sec YDOT = 3734
460874 meter/sec
ZDOT = -9309
017743 ZDOT = -2807
648562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14619222
09 X = 4455938
89
Y = -6250517
18 feet Y = -1905157
64 meter
Z = -15313390
44 Z = -4667521
41
XDOT = -77
924946 XDOT = -23
751523
YDOT = 22424
530923 feet/sec YDOT = 6834
997025 meter/sec
ZDOT = -9197
723391 ZDOT = -2803
466090
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 29391U 06036A 06264
85931418
00014500 00000-0 95600-4 0 9091
2 29391 51
6335 49
4540 0011926 7
3894 352
7444 15
76188254 1945
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06264
85931418 = yrday
fracday
Element set: 909
Inclination: 51
6335 deg
RA of node: 49
4540 deg
Eccentricity:
0011926
Arg of perigee: 7
3894 deg
Mean anomaly: 352
7444 deg
Mean motion: 15
76188254 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 194
Checksum: 324
Coasting Arc #11 (Orbit 208)
---------------------------------------
Vector Time (GMT): 2006/265/19:25:00
000
Vector Time (MET): 013/04:10:05
028
Weight (LBS) : 210939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5168969
50 A = 6725675
52 meter
Y = 4225158
80 meter E =
0022082
Z = -703412
00 I = 51
87187
XDOT = -2546
883227 Wp = 24
16830
YDOT = 4102
792750 meter/sec RA = 44
00655 deg
ZDOT = 6014
064611 TA = 328
17690
MA = 328
31015
Ha = 190
012 n
mi
Hp = 178
247
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16958561
35 X = 5124705
06
Y = 13862069
56 feet Y = 4282774
87 meter
Z = -2307782
17 Z = -678408
72
XDOT = -8355
916099 XDOT = -2621
835893
YDOT = 13460
606134 feet/sec YDOT = 4073
862513 meter/sec
ZDOT = 19731
183106 ZDOT = 6001
509513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6481269
54 X = -1975490
96
Y = 20932431
92 feet Y = 6380205
25 meter
Z = -2214062
49 Z = -674846
25
XDOT = -14126
581056 XDOT = -4305
781906
YDOT = -2322
814509 feet/sec YDOT = -707
993862 meter/sec
ZDOT = 19684
969532 ZDOT = 5999
978713
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 29391U 06036A 06265
81032527
00014500 00000-0 95600-4 0 9103
2 29391 51
6335 44
5531 0012082 10
7069 349
4351 15
76218753 2092
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06265
81032527 = yrday
fracday
Element set: 910
Inclination: 51
6335 deg
RA of node: 44
5531 deg
Eccentricity:
0012082
Arg of perigee: 10
7069 deg
Mean anomaly: 349
4351 deg
Mean motion: 15
76218753 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 209
Checksum: 283
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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