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
There are no maneuvers
Coasting Arc #1 (Orbit 43)
---------------------------------------
Vector Time (GMT): 2006/255/08:07:53
000
Vector Time (MET): 002/16:52:58
028
Weight (LBS) : 211238
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2766049
04 A = 6718989
08 meter
Y = 4399939
44 meter E =
0007554
Z = -4255900
44 I = 51
94050
XDOT = -3629
598032 Wp = 17
97089
YDOT = 5760
409295 meter/sec RA = 97
72238 deg
ZDOT = 3605
084547 TA = 288
45171
MA = 288
53381
Ha = 188
967 n
mi
Hp = 181
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9074964
06 X = 2737264
50
Y = 14435496
84 feet Y = 4430742
88 meter
Z = -13962927
96 Z = -4242532
68
XDOT = -11908
130027 XDOT = -3711
323087
YDOT = 18898
980627 feet/sec YDOT = 5719
320347 meter/sec
ZDOT = 11827
705208 ZDOT = 3587
253466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9849317
13 X = 3002071
86
Y = -13969049
65 feet Y = -4257766
33 meter
Z = -13912530
43 Z = -4240539
27
XDOT = 21019
487145 XDOT = 6406
739682
YDOT = 3134
501793 feet/sec YDOT = 955
396147 meter/sec
ZDOT = 11762
105902 ZDOT = 3585
089879
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
34824594
00014500 00000-0 95600-4 0 9002
2 29391 51
6334 98
4579 0011568 331
2123 28
8403 15
75877478 448
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06255
34824594 = yrday
fracday
Element set: 900
Inclination: 51
6334 deg
RA of node: 98
4579 deg
Eccentricity:
0011568
Arg of perigee: 331
2123 deg
Mean anomaly: 28
8403 deg
Mean motion: 15
75877478 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 44
Checksum: 318
Coasting Arc #2 (Orbit 59)
---------------------------------------
Vector Time (GMT): 2006/256/08:12:48
871
Vector Time (MET): 003/16:57:53
900
Weight (LBS) : 211238
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3826977
36 A = 6717091
69 meter
Y = -2891607
46 meter E =
0015252
Z = -4713293
04 I = 51
93773
XDOT = 1841
128306 Wp = 21
34140
YDOT = 6944
696688 meter/sec RA = 92
62211 deg
ZDOT = -2754
542705 TA = 221
55638
MA = 221
67242
Ha = 189
016 n
mi
Hp = 180
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12555700
01 X = 3881957
67
Y = -9486901
13 feet Y = -2848458
54 meter
Z = -15463559
83 Z = -4694568
06
XDOT = 6040
447198 XDOT = 1776
633073
YDOT = 22784
437952 feet/sec YDOT = 6964
946266 meter/sec
ZDOT = -9037
213600 ZDOT = -2745
754809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13895842
11 X = -4235452
68
Y = -7529414
60 feet Y = -2294965
57 meter
Z = -15394221
84 Z = -4692158
82
XDOT = 17616
163942 XDOT = 5369
406770
YDOT = -14028
317407 feet/sec YDOT = -4275
831146 meter/sec
ZDOT = -9003
523675 ZDOT = -2744
274016
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
36285543
00014500 00000-0 95600-4 0 9011
2 29391 51
6340 93
2320 0011670 334
9965 25
0633 15
75938181 601
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06256
36285543 = yrday
fracday
Element set: 901
Inclination: 51
6340 deg
RA of node: 93
2320 deg
Eccentricity:
0011670
Arg of perigee: 334
9965 deg
Mean anomaly: 25
0633 deg
Mean motion: 15
75938181 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 60
Checksum: 290
Coasting Arc #3 (Orbit 75)
---------------------------------------
Vector Time (GMT): 2006/257/08:17:43
200
Vector Time (MET): 004/17:02:48
228
Weight (LBS) : 211238
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -329906
83 A = 6726680
98 meter
Y = -6719859
67 meter E =
0004991
Z = 39779
50 I = 51
97016
XDOT = 4733
888945 Wp = 65
09286
YDOT = -271
793621 meter/sec RA = 87
45432 deg
ZDOT = -6062
062651 TA = 114
47707
MA = 114
42500
Ha = 189
110 n
mi
Hp = 180
733
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1082371
48 X = -254853
05
Y = -22046783
69 feet Y = -6723132
71 meter
Z = 130510
18 Z = 38358
76
XDOT = 15531
131709 XDOT = 4766
027398
YDOT = -891
711355 feet/sec YDOT = -218
620049 meter/sec
ZDOT = -19888
656992 ZDOT = -6038
987334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19175703
47 X = -5844754
42
Y = 10932802
89 feet Y = 3332318
32 meter
Z = 124295
98 Z = 37885
42
XDOT = -7068
598731 XDOT = -2154
508893
YDOT = -12149
739776 feet/sec YDOT = -3703
240684 meter/sec
ZDOT = -19802
747405 ZDOT = -6035
877409
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
37743818
00014500 00000-0 95600-4 0 9028
2 29391 51
6342 88
0056 0011565 338
2837 21
7835 15
75930062 763
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06257
37743818 = yrday
fracday
Element set: 902
Inclination: 51
6342 deg
RA of node: 88
0056 deg
Eccentricity:
0011565
Arg of perigee: 338
2837 deg
Mean anomaly: 21
7835 deg
Mean motion: 15
75930062 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 76
Checksum: 309
Coasting Arc #4 (Orbit 91)
---------------------------------------
Vector Time (GMT): 2006/258/08:22:38
145
Vector Time (MET): 005/17:07:43
173
Weight (LBS) : 211238
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4078422
41 A = 6716661
91 meter
Y = -2460967
32 meter E =
0015251
Z = 4739101
22 I = 51
93511
XDOT = 1158
131346 Wp = 11
38602
YDOT = -7123
279276 meter/sec RA = 82
28716 deg
ZDOT = -2686
280870 TA = 104
99898
MA = 104
83013
Ha = 189
230 n
mi
Hp = 180
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13380650
94 X = -4073592
19
Y = -8074039
78 feet Y = -2506596
30 meter
Z = 15548232
35 Z = 4719299
90
XDOT = 3799
643525 XDOT = 1250
832901
YDOT = -23370
338832 feet/sec YDOT = -7109
795602 meter/sec
ZDOT = -8813
257449 ZDOT = -2680
429878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -507436
37 X = -154666
60
Y = 15693088
46 feet Y = 4783253
36 meter
Z = 15474138
10 Z = 4716517
29
XDOT = -21148
170642 XDOT = -6445
962412
YDOT = 8038
238267 feet/sec YDOT = 2450
055024 meter/sec
ZDOT = -8792
435939 ZDOT = -2679
934474
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
39199055
00014500 00000-0 95600-4 0 9030
2 29391 51
6345 82
7790 0011909 341
8843 18
1895 15
76048689 921
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06258
39199055 = yrday
fracday
Element set: 903
Inclination: 51
6345 deg
RA of node: 82
7790 deg
Eccentricity:
0011909
Arg of perigee: 341
8843 deg
Mean anomaly: 18
1895 deg
Mean motion: 15
76048689 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 92
Checksum: 339
Coasting Arc #5 (Orbit 107)
---------------------------------------
Vector Time (GMT): 2006/259/08:27:35
729
Vector Time (MET): 006/17:12:40
757
Weight (LBS) : 211238
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2347946
66 A = 6718604
93 meter
Y = 4643562
81 meter E =
0010973
Z = 4238953
98 I = 51
93618
XDOT = -4140
393228 Wp = 37
79132
YDOT = -5400
275666 meter/sec RA = 77
18468 deg
ZDOT = 3625
966009 TA = 15
54984
MA = 15
51616
Ha = 189
477 n
mi
Hp = 179
978
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7703237
07 X = -2420344
06
Y = 15234786
12 feet Y = 4616873
39 meter
Z = 13907329
33 Z = 4227372
07
XDOT = -13583
967284 XDOT = -4097
248165
YDOT = -17717
439850 feet/sec YDOT = -5446
383824 meter/sec
ZDOT = 11896
213940 ZDOT = 3605
956679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17058596
55 X = 5199460
23
Y = -1274165
27 feet Y = -388365
58 meter
Z = 13864817
52 Z = 4225996
38
XDOT = -8132
188337 XDOT = -2478
691005
YDOT = 19626
793075 feet/sec YDOT = 5982
246529 meter/sec
ZDOT = 11820
940049 ZDOT = 3603
022527
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
40651818
00014500 00000-0 95600-4 0 9044
2 29391 51
6342 77
5519 0011929 346
3255 13
7584 15
76027924 1081
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06259
40651818 = yrday
fracday
Element set: 904
Inclination: 51
6342 deg
RA of node: 77
5519 deg
Eccentricity:
0011929
Arg of perigee: 346
3255 deg
Mean anomaly: 13
7584 deg
Mean motion: 15
76027924 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 108
Checksum: 313
Coasting Arc #6 (Orbit 122)
---------------------------------------
Vector Time (GMT): 2006/260/08:32:26
440
Vector Time (MET): 007/17:17:31
468
Weight (LBS) : 211238
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2728654
89 A = 6725869
15 meter
Y = 6064023
33 meter E =
0020120
Z = -921986
07 I = 51
95315
XDOT = -4038
263427 Wp = 11
40046
YDOT = 2720
289828 meter/sec RA = 72
00287 deg
ZDOT = 5981
530680 TA = 338
55604
MA = 338
64021
Ha = 189
472 n
mi
Hp = 179
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8952279
82 X = 2665049
54
Y = 19895089
65 feet Y = 6094213
18 meter
Z = -3024888
68 Z = -908884
72
XDOT = -13248
895759 XDOT = -4097
470759
YDOT = 8924
835394 feet/sec YDOT = 2674
752067 meter/sec
ZDOT = 19624
444488 ZDOT = 5961
769225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11632388
04 X = 3545551
87
Y = -18464648
97 feet Y = -5628025
01 meter
Z = -2975255
40 Z = -906857
85
XDOT = 13470
383661 XDOT = 4105
772940
YDOT = 5357
919836 feet/sec YDOT = 1633
093966 meter/sec
ZDOT = 19551
196382 ZDOT = 5959
204657
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
35760811
00014500 00000-0 95600-4 0 9055
2 29391 51
6338 72
6516 0012037 349
0134 11
0765 15
76094094 1237
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06260
35760811 = yrday
fracday
Element set: 905
Inclination: 51
6338 deg
RA of node: 72
6516 deg
Eccentricity:
0012037
Arg of perigee: 349
0134 deg
Mean anomaly: 11
0765 deg
Mean motion: 15
76094094 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 123
Checksum: 280
Coasting Arc #7 (Orbit 138)
---------------------------------------
Vector Time (GMT): 2006/261/08:36:53
657
Vector Time (MET): 008/17:21:58
685
Weight (LBS) : 211238
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4373394
75 A = 6714885
02 meter
Y = 52583
90 meter E =
0014920
Z = -5103106
59 I = 51
90535
XDOT = 1765
214502 Wp = 52
50587
YDOT = 7319
626150 meter/sec RA = 66
85019 deg
ZDOT = 1600
273553 TA = 232
74302
MA = 232
87919
Ha = 189
579 n
mi
Hp = 179
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14348407
97 X = 4397270
24
Y = 172519
35 feet Y = 101675
39 meter
Z = -16742475
70 Z = -5081802
85
XDOT = 5791
386162 XDOT = 1675
373036
YDOT = 24014
521490 feet/sec YDOT = 7338
883915 meter/sec
ZDOT = 5250
241315 ZDOT = 1608
630700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8271050
91 X = -2521016
32
Y = -11838404
83 feet Y = -3608345
79 meter
Z = -16663101
59 Z = -5078913
36
XDOT = 15300
103755 XDOT = 4663
471624
YDOT = -18068
884678 feet/sec YDOT = -5507
396050 meter/sec
ZDOT = 5282
373794 ZDOT = 1610
067532
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
37208295
00014500 00000-0 95600-4 0 9062
2 29391 51
6328 67
4236 0012039 352
6312 7
4674 15
76129552 1390
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06261
37208295 = yrday
fracday
Element set: 906
Inclination: 51
6328 deg
RA of node: 67
4236 deg
Eccentricity:
0012039
Arg of perigee: 352
6312 deg
Mean anomaly: 7
4674 deg
Mean motion: 15
76129552 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 139
Checksum: 300
Coasting Arc #8 (Orbit 154)
---------------------------------------
Vector Time (GMT): 2006/262/08:41:56
572
Vector Time (MET): 009/17:27:01
600
Weight (LBS) : 211238
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 173912
55 A = 6720428
23 meter
Y = -5669326
01 meter E =
0013748
Z = -3620292
34 I = 51
91088
XDOT = 5539
841706 Wp = 19
54973
YDOT = 2995
022693 meter/sec RA = 61
73880 deg
ZDOT = -4416
167463 TA = 203
57518
MA = 203
63825
Ha = 189
647 n
mi
Hp = 179
240
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 570579
22 X = 254948
91
Y = -18600150
95 feet Y = -5666925
63 meter
Z = -11877599
53 Z = -3619250
56
XDOT = 18175
333680 XDOT = 5527
355566
YDOT = 9826
189939 feet/sec YDOT = 3056
968321 meter/sec
ZDOT = -14488
738397 ZDOT = -4389
285506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15072079
39 X = -4593969
80
Y = 10917756
23 feet Y = 3327732
10 meter
Z = -11874492
34 Z = -3619345
27
XDOT = -2655
586567 XDOT = -809
422786
YDOT = -19343
191935 feet/sec YDOT = -5895
804902 meter/sec
ZDOT = -14388
179448 ZDOT = -4385
517096
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
38654496
00014500 00000-0 95600-4 0 9073
2 29391 51
6319 62
1965 0012063 356
2218 3
8853 15
76129049 1551
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06262
38654496 = yrday
fracday
Element set: 907
Inclination: 51
6319 deg
RA of node: 62
1965 deg
Eccentricity:
0012063
Arg of perigee: 356
2218 deg
Mean anomaly: 3
8853 deg
Mean motion: 15
76129049 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 155
Checksum: 312
Coasting Arc #9 (Orbit 170)
---------------------------------------
Vector Time (GMT): 2006/263/08:46:30
616
Vector Time (MET): 010/17:31:35
644
Weight (LBS) : 211238
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4693966
81 A = 6724458
17 meter
Y = -4436042
87 meter E =
0014503
Z = 1876460
22 I = 51
91076
XDOT = 2192
546882 Wp = 62
77954
YDOT = -4731
916664 meter/sec RA = 56
54507 deg
ZDOT = -5662
054356 TA = 96
45801
MA = 96
29285
Ha = 189
751 n
mi
Hp = 178
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15400153
59 X = -4653075
49
Y = -14553946
42 feet Y = -4488360
39 meter
Z = 6156365
55 Z = 1853756
52
XDOT = 7193
395281 XDOT = 2272
858048
YDOT = -15524
660970 feet/sec YDOT = -4706
922927 meter/sec
ZDOT = -18576
293818 ZDOT = -5651
207793
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1225516
75 X = -373537
51
Y = 21178334
54 feet Y = 6455156
37 meter
Z = 6071176
03 Z = 1850494
45
XDOT = -15037
078016 XDOT = -4583
301379
YDOT = 4481
636085 feet/sec YDOT = 1366
002679 meter/sec
ZDOT = -18536
531056 ZDOT = -5649
934666
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
40099704
00014500 00000-0 95600-4 0 9083
2 29391 51
6324 56
9684 0012252 359
9725
1437 15
76190368 1717
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06263
40099704 = yrday
fracday
Element set: 908
Inclination: 51
6324 deg
RA of node: 56
9684 deg
Eccentricity:
0012252
Arg of perigee: 359
9725 deg
Mean anomaly:
1437 deg
Mean motion: 15
76190368 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 171
Checksum: 308
Coasting Arc #10 (Orbit 186)
---------------------------------------
Vector Time (GMT): 2006/264/08:51:19
404
Vector Time (MET): 011/17:36:24
432
Weight (LBS) : 211238
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3675473
64 A = 6714091
04 meter
Y = 2001881
76 meter E =
0013825
Z = 5248289
61 I = 51
85778
XDOT = -4381
417580 Wp = 14
37863
YDOT = -6306
567383 meter/sec RA = 51
40329 deg
ZDOT = -649
353904 TA = 81
84996
MA = 81
69316
Ha = 189
943 n
mi
Hp = 178
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12058640
55 X = -3723104
37
Y = 6567853
54 feet Y = 1960470
41 meter
Z = 17218797
94 Z = 5230318
40
XDOT = -14374
729594 XDOT = -4307
340879
YDOT = -20690
837871 feet/sec YDOT = -6355
200427 meter/sec
ZDOT = -2130
426195 ZDOT = -670
458605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13029019
49 X = 3971245
14
Y = 4591725
03 feet Y = 1399557
79 meter
Z = 17152120
19 Z = 5227966
23
XDOT = -5345
339490 XDOT = -1629
259477
YDOT = 23588
332989 feet/sec YDOT = 7189
723895 meter/sec
ZDOT = -2209
912231 ZDOT = -673
581248
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
41543392
00014500 00000-0 95600-4 0 9093
2 29391 51
6314 51
7399 0012049 4
0506 356
0754 15
76162805 1878
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06264
41543392 = yrday
fracday
Element set: 909
Inclination: 51
6314 deg
RA of node: 51
7399 deg
Eccentricity:
0012049
Arg of perigee: 4
0506 deg
Mean anomaly: 356
0754 deg
Mean motion: 15
76162805 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 187
Checksum: 299
Coasting Arc #11 (Orbit 202)
---------------------------------------
Vector Time (GMT): 2006/265/08:55:43
966
Vector Time (MET): 012/17:40:48
994
Weight (LBS) : 211238
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2384138
07 A = 6722461
58 meter
Y = 5630138
11 meter E =
0020628
Z = 2761973
32 I = 51
86735
XDOT = -5726
366769 Wp = 45
96942
YDOT = -115
956516 meter/sec RA = 46
27899 deg
ZDOT = 5169
774364 TA = 345
58967
MA = 345
64841
Ha = 189
813 n
mi
Hp = 178
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7821975
28 X = 2307519
28
Y = 18471581
71 feet Y = 5656398
55 meter
Z = 9061592
25 Z = 2773369
12
XDOT = -18787
292549 XDOT = -5749
756317
YDOT = -380
434764 feet/sec YDOT = -180
190814 meter/sec
ZDOT = 16961
201982 ZDOT = 5141
898757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7794867
68 X = 2375875
67
Y = -18461784
96 feet Y = -5627152
06 meter
Z = 9104812
81 Z = 2775146
95
XDOT = 11565
559100 XDOT = 3525
182414
YDOT = 13212
178410 feet/sec YDOT = 4027
071979 meter/sec
ZDOT = 16857
339476 ZDOT = 5138
117072
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
42984596
00014500 00000-0 95600-4 0 9102
2 29391 51
6308 46
5112 0011987 7
5915 352
5428 15
76235522 2033
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06265
42984596 = yrday
fracday
Element set: 910
Inclination: 51
6308 deg
RA of node: 46
5112 deg
Eccentricity:
0011987
Arg of perigee: 7
5915 deg
Mean anomaly: 352
5428 deg
Mean motion: 15
76235522 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 203
Checksum: 303
Coasting Arc #12 (Orbit 217)
---------------------------------------
Vector Time (GMT): 2006/266/09:00:11
428
Vector Time (MET): 013/17:45:16
456
Weight (LBS) : 211238
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5733459
13 A = 6722296
55 meter
Y = 2021052
36 meter E =
0015427
Z = -2856105
19 I = 51
84609
XDOT = 501
402080 Wp = 24
91579
YDOT = 5754
271225 meter/sec RA = 41
07740 deg
ZDOT = 5102
003745 TA = 302
34940
MA = 302
49865
Ha = 190
019 n
mi
Hp = 178
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18810561
45 X = 5724283
05
Y = 6630749
22 feet Y = 2085183
89 meter
Z = -9370423
84 Z = -2828274
18
XDOT = 1645
019948 XDOT = 412
166302
YDOT = 18878
842602 feet/sec YDOT = 5759
384927 meter/sec
ZDOT = 16738
857431 ZDOT = 5104
222546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9084609
07 X = -2768988
84
Y = -17810425
80 feet Y = -5428617
78 meter
Z = -9266472
43 Z = -2824420
80
XDOT = 10597
488175 XDOT = 3230
114396
YDOT = -14078
408796 feet/sec YDOT = -4291
099001 meter/sec
ZDOT = 16747
903625 ZDOT = 5104
761025
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 06266
38083911
00014500 00000-0 95600-4 0 9110
2 29391 51
6307 41
6095 0012014 11
8104 348
3340 15
76248518 2189
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06266
38083911 = yrday
fracday
Element set: 911
Inclination: 51
6307 deg
RA of node: 41
6095 deg
Eccentricity:
0012014
Arg of perigee: 11
8104 deg
Mean anomaly: 348
3340 deg
Mean motion: 15
76248518 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 218
Checksum: 277
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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