Date:
September 10th 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) : 75 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 0
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
252/15:53:29
095 135
2 220
5 220
5
000/00:38:34
124 26
5 -0
5 154
0
000/00:02:26
947 -172
2 -0
9 123
8
252/18:12:11
972 -40
5 81
7 81
7
000/02:57:17
000 -32
4 0
0 171
3
000/00:00:55
284 63
2 -0
0 152
0
253/07:08:06
837 13
1 52
2 52
2
000/15:53:11
865 39
3 0
0 181
5
000/00:00:36
020 -31
7 0
0 171
5
253/18:31:07
963 -1
6 6
0 6
0
001/03:16:12
991 -4
6 0
0 181
5
000/00:00:26
472 3
5 0
0 174
8
254/06:36:41
354 -4
7 11
3 11
3
001/15:21:46
383 -6
8 0
0 182
5
000/00:00:17
097 7
8 -0
0 180
4
254/08:08:15
670 -3
6 8
9 8
9
001/16:53:20
698 -5
4 -0
1 187
5
000/00:00:14
041 6
1 -0
1 181
4
254/09:25:09
012 -1
7 2
5 2
9
001/18:10:14
040 -0
6 0
1 188
9
000/00:00:12
724 2
2 1
5 181
4
Coasting Arc #1 (begining on orbit 1)
---------------------------------------
Vector Time (GMT): 2006/252/15:26:03
287
Vector Time (MET): 000/00:11:08
315
Weight (LBS) : 257857
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4410844
07 A = 6518860
71 meter
Y = 1525923
41 meter E =
0126833
Z = 4507930
99 I = 51
91456
XDOT = 387
218434 Wp = 352
55169
YDOT = -7261
959743 meter/sec RA = 111
72318 deg
ZDOT = 2970
686163 TA = 69
41060
MA = 68
05460
Ha = 124
025 n
mi
Hp = 32
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14471273
18 X = -4449478
08
Y = 5006310
41 feet Y = 1476383
24 meter
Z = 14789799
85 Z = 4486409
12
XDOT = 1270
401687 XDOT = 453
962805
YDOT = -23825
327240 feet/sec YDOT = -7257
256242 meter/sec
ZDOT = 9746
345678 ZDOT = 2972
729942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8084752
19 X = 2464232
47
Y = -13094859
68 feet Y = -3991313
23 meter
Z = 14709877
73 Z = 4483570
73
XDOT = 13202
719701 XDOT = 4024
188965
YDOT = 18611
859442 feet/sec YDOT = 5672
894758 meter/sec
ZDOT = 9752
913079 ZDOT = 2972
687907
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 99115U 06252
69324212
00014500 00000-0 95600-4 0 9005
2 99115 51
6330 112
2271 0064615 349
6485 10
3396 16
67938876 27
Satellite: SHUTTLE
Catalog Number: 99115
Epoch time: 06252
69324212 = yrday
fracday
Element set: 900
Inclination: 51
6330 deg
RA of node: 112
2271 deg
Eccentricity:
0064615
Arg of perigee: 349
6485 deg
Mean anomaly: 10
3396 deg
Mean motion: 16
67938876 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 2
Checksum: 295
Coasting Arc #2 (begining on orbit 1)
---------------------------------------
Vector Time (GMT): 2006/252/15:54:42
569
Vector Time (MET): 000/00:39:47
597
Weight (LBS) : 252306
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2342046
26 A = 6641411
21 meter
Y = -6177413
50 meter E =
0051045
Z = 121405
71 I = 51
94717
XDOT = 4529
578392 Wp = 174
50234
YDOT = 1593
762525 meter/sec RA = 111
58747 deg
ZDOT = -6129
808370 TA = 4
16063
MA = 4
11836
Ha = 154
040 n
mi
Hp = 123
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7683878
79 X = 2410359
11
Y = -20267104
66 feet Y = -6150841
48 meter
Z = 398312
70 Z = 132949
79
XDOT = 14860
821496 XDOT = 4541
197632
YDOT = 5228
879674 feet/sec YDOT = 1644
479284 meter/sec
ZDOT = -20110
919848 ZDOT = -6107
775536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9416583
66 X = 2870174
70
Y = 19521530
84 feet Y = 5950162
60 meter
Z = 440412
43 Z = 134237
71
XDOT = -12674
084256 XDOT = -3863
060881
YDOT = 6575
893329 feet/sec YDOT = 2004
332287 meter/sec
ZDOT = -20028
646935 ZDOT = -6104
731586
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 99115U 06252
69437111
00014500 00000-0 95600-4 0 9019
2 99115 51
6325 112
2370 0042147 185
8380 174
2315 16
06455712 28
Satellite: SHUTTLE
Catalog Number: 99115
Epoch time: 06252
69437111 = yrday
fracday
Element set: 901
Inclination: 51
6325 deg
RA of node: 112
2370 deg
Eccentricity:
0042147
Arg of perigee: 185
8380 deg
Mean anomaly: 174
2315 deg
Mean motion: 16
06455712 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 2
Checksum: 270
Coasting Arc #3 (begining on orbit 3)
---------------------------------------
Vector Time (GMT): 2006/252/18:12:39
614
Vector Time (MET): 000/02:57:44
642
Weight (LBS) : 250283
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3189843
98 A = 6683608
29 meter
Y = 5730930
62 meter E =
0034669
Z = 1168220
70 I = 51
94910
XDOT = -3718
162557 Wp = 34
69557
YDOT = -3293
157038 meter/sec RA = 111
08653 deg
ZDOT = 5945
942215 TA = 338
17100
MA = 338
31837
Ha = 171
343 n
mi
Hp = 152
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10465367
39 X = -3259365
98
Y = 18802265
82 feet Y = 5694871
39 meter
Z = 3832745
09 Z = 1152555
11
XDOT = -12198
696054 XDOT = -3709
946066
YDOT = -10804
320990 feet/sec YDOT = -3334
689212 meter/sec
ZDOT = 19507
684432 ZDOT = 5927
899539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16951378
73 X = -5166780
24
Y = -13271677
46 feet Y = -4045207
29 meter
Z = 3775233
24 Z = 1150691
09
XDOT = 11612
222083 XDOT = 3539
405291
YDOT = -9248
163613 feet/sec YDOT = -2818
840269 meter/sec
ZDOT = 19440
025918 ZDOT = 5925
319900
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 99115U 06252
81939414
00014500 00000-0 95600-4 0 9027
2 99115 51
6356 111
5711 0022435 20
6884 339
5192 15
91020593 45
Satellite: SHUTTLE
Catalog Number: 99115
Epoch time: 06252
81939414 = yrday
fracday
Element set: 902
Inclination: 51
6356 deg
RA of node: 111
5711 deg
Eccentricity:
0022435
Arg of perigee: 20
6884 deg
Mean anomaly: 339
5192 deg
Mean motion: 15
91020593 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 4
Checksum: 285
Coasting Arc #4 (begining on orbit 11)
---------------------------------------
Vector Time (GMT): 2006/253/07:08:24
847
Vector Time (MET): 000/15:53:29
875
Weight (LBS) : 249001
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4147996
85 A = 6706493
89 meter
Y = -3976534
84 meter E =
0016234
Z = -3437249
48 I = 51
93855
XDOT = 1846
928078 Wp = 230
77607
YDOT = 5913
911407 meter/sec RA = 108
27964 deg
ZDOT = -4608
670363 TA = 349
91591
MA = 349
94845
Ha = 181
514 n
mi
Hp = 171
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13608913
56 X = 4208852
35
Y = -13046374
14 feet Y = -3929809
60 meter
Z = -11277065
23 Z = -3416950
35
XDOT = 6059
475323 XDOT = 1803
048845
YDOT = 19402
596481 feet/sec YDOT = 5934
319150 meter/sec
ZDOT = -15120
309589 ZDOT = -4599
804893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14309470
14 X = -4361526
50
Y = -12342442
06 feet Y = -3761976
34 meter
Z = -11202044
24 Z = -3414383
08
XDOT = 17816
268392 XDOT = 5430
398606
YDOT = -6950
352277 feet/sec YDOT = -2118
467374 meter/sec
ZDOT = -15086
451822 ZDOT = -4598
350515
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 99115U 06253
32197079
00014500 00000-0 95600-4 0 9038
2 99115 51
6354 108
9306 0020430 239
2429 120
6726 15
81250045 126
Satellite: SHUTTLE
Catalog Number: 99115
Epoch time: 06253
32197079 = yrday
fracday
Element set: 903
Inclination: 51
6354 deg
RA of node: 108
9306 deg
Eccentricity:
0020430
Arg of perigee: 239
2429 deg
Mean anomaly: 120
6726 deg
Mean motion: 15
81250045 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 12
Checksum: 277
Coasting Arc #5 (begining on orbit 19)
---------------------------------------
Vector Time (GMT): 2006/253/18:31:21
199
Vector Time (MET): 001/03:16:26
227
Weight (LBS) : 248828
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4032576
38 A = 6709234
24 meter
Y = 4023058
50 meter E =
0008043
Z = 3554391
46 I = 51
94215
XDOT = -1968
071600 Wp = 198
99528
YDOT = -5942
000881 meter/sec RA = 105
82351 deg
ZDOT = 4488
021502 TA = 203
25185
MA = 203
28826
Ha = 181
464 n
mi
Hp = 174
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13230237
47 X = -4094529
78
Y = 13199010
82 feet Y = 3977617
78 meter
Z = 11661389
30 Z = 3534650
38
XDOT = -6456
927822 XDOT = -1923
283206
YDOT = -19494
753548 feet/sec YDOT = -5963
758295 meter/sec
ZDOT = 14724
479995 ZDOT = 4478
569638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12427022
63 X = -3787756
50
Y = -14018488
45 feet Y = -4272835
28 meter
Z = 11588449
44 Z = 3532159
39
XDOT = 18810
798091 XDOT = 5733
531258
YDOT = -4520
395369 feet/sec YDOT = -1377
816508 meter/sec
ZDOT = 14688
438089 ZDOT = 4477
035930
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 99115U 06253
82760047
00014500 00000-0 95600-4 0 9045
2 99115 51
6362 106
3016 0016405 244
9431 115
0033 15
80164714 202
Satellite: SHUTTLE
Catalog Number: 99115
Epoch time: 06253
82760047 = yrday
fracday
Element set: 904
Inclination: 51
6362 deg
RA of node: 106
3016 deg
Eccentricity:
0016405
Arg of perigee: 244
9431 deg
Mean anomaly: 115
0033 deg
Mean motion: 15
80164714 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 20
Checksum: 260
Coasting Arc #6 (begining on orbit 27)
---------------------------------------
Vector Time (GMT): 2006/254/06:36:49
903
Vector Time (MET): 001/15:21:54
931
Weight (LBS) : 248550
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3348466
94 A = 6717764
33 meter
Y = 5180488
15 meter E =
0005713
Z = 2650871
38 I = 51
95267
XDOT = -3117
011096 Wp = 30
24034
YDOT = -4701
968997 meter/sec RA = 103
22378 deg
ZDOT = 5251
559578 TA = 359
85050
MA = 359
85067
Ha = 182
453 n
mi
Hp = 180
445
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10985783
93 X = -3419024
56
Y = 16996352
20 feet Y = 5142649
33 meter
Z = 8697084
57 Z = 2634432
82
XDOT = -10226
414358 XDOT = -3089
712700
YDOT = -15426
407472 feet/sec YDOT = -4736
672313 meter/sec
ZDOT = 17229
526173 ZDOT = 5236
483501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16727333
98 X = 5098491
40
Y = 11437137
62 feet Y = 3486039
55 meter
Z = 8636602
19 Z = 2632436
35
XDOT = -14835
183446 XDOT = -4521
763914
YDOT = 8729
307396 feet/sec YDOT = 2660
692894 meter/sec
ZDOT = 17172
719680 ZDOT = 5234
244958
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 99115U 06254
33363108
00014500 00000-0 95600-4 0 9050
2 99115 51
6349 103
6837 0010750 280
9520 79
0435 15
78008994 281
Satellite: SHUTTLE
Catalog Number: 99115
Epoch time: 06254
33363108 = yrday
fracday
Element set: 905
Inclination: 51
6349 deg
RA of node: 103
6837 deg
Eccentricity:
0010750
Arg of perigee: 280
9520 deg
Mean anomaly: 79
0435 deg
Mean motion: 15
78008994 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 28
Checksum: 304
Coasting Arc #7 (begining on orbit 28)
---------------------------------------
Vector Time (GMT): 2006/254/08:08:22
691
Vector Time (MET): 001/16:53:27
719
Weight (LBS) : 248331
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3384632
58 A = 6722266
65 meter
Y = 5098425
48 meter E =
0012486
Z = 2761596
89 I = 51
95339
XDOT = -3050
914817 Wp = 31
36645
YDOT = -4829
863432 meter/sec RA = 102
89768 deg
ZDOT = 5177
659918 TA =
12111
MA =
12081
Ha = 187
500 n
mi
Hp = 181
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11104437
59 X = -3454807
77
Y = 16727117
70 feet Y = 5060184
37 meter
Z = 9060357
25 Z = 2744983
58
XDOT = -10009
563048 XDOT = -3021
832208
YDOT = -15846
008634 feet/sec YDOT = -4863
817657 meter/sec
ZDOT = 16987
073222 ZDOT = 5162
909269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19656898
60 X = 5991422
69
Y = 4220852
79 feet Y = 1286515
93 meter
Z = 8999211
83 Z = 2742959
77
XDOT = -10712
318543 XDOT = -3265
114692
YDOT = 13789
304789 feet/sec YDOT = 4202
980100 meter/sec
ZDOT = 16931
460820 ZDOT = 5160
709258
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 99115U 06254
39702808
00014500 00000-0 95600-4 0 9061
2 99115 51
6361 103
3574 0010687 320
0158 40
0219 15
76331609 291
Satellite: SHUTTLE
Catalog Number: 99115
Epoch time: 06254
39702808 = yrday
fracday
Element set: 906
Inclination: 51
6361 deg
RA of node: 103
3574 deg
Eccentricity:
0010687
Arg of perigee: 320
0158 deg
Mean anomaly: 40
0219 deg
Mean motion: 15
76331609 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 29
Checksum: 285
Coasting Arc #8 (begining on orbit 28)
---------------------------------------
Vector Time (GMT): 2006/254/09:25:15
373
Vector Time (MET): 001/18:10:20
402
Weight (LBS) : 248248
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 411917
02 A = 6724565
79 meter
Y = 6306317
17 meter E =
0014847
Z = -2269300
45 I = 51
95821
XDOT = -4909
380565 Wp = 347
59776
YDOT = 2291
912908 meter/sec RA = 102
58074 deg
ZDOT = 5485
633674 TA = 346
99094
MA = 347
02920
Ha = 188
874 n
mi
Hp = 181
360
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1351433
79 X = 352392
24
Y = 20690016
97 feet Y = 6310590
56 meter
Z = -7445211
44 Z = -2267444
14
XDOT = -16106
891618 XDOT = -4961
292607
YDOT = 7519
399306 feet/sec YDOT = 2236
723430 meter/sec
ZDOT = 17997
485807 ZDOT = 5461
657539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14739702
36 X = 4492661
28
Y = -14586311
62 feet Y = -4445907
78 meter
Z = -7437407
93 Z = -2266921
94
XDOT = 15223
995445 XDOT = 4640
273812
YDOT = 6265
472992 feet/sec YDOT = 1909
716168 meter/sec
ZDOT = 17908
524977 ZDOT = 5458
518413
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 99115U 06254
39702642
00014500 00000-0 95600-4 0 9078
2 99115 51
6371 103
3577 0012560 324
4050 35
6275 15
75887774 296
Satellite: SHUTTLE
Catalog Number: 99115
Epoch time: 06254
39702642 = yrday
fracday
Element set: 907
Inclination: 51
6371 deg
RA of node: 103
3577 deg
Eccentricity:
0012560
Arg of perigee: 324
4050 deg
Mean anomaly: 35
6275 deg
Mean motion: 15
75887774 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 29
Checksum: 307
Coasting Arc #9 (begining on orbit 44)
---------------------------------------
Vector Time (GMT): 2006/255/09:30:21
108
Vector Time (MET): 002/18:15:26
136
Weight (LBS) : 248248
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4082059
79 A = 6714590
87 meter
Y = 728148
70 meter E =
0013350
Z = -5288200
17 I = 51
92992
XDOT = -1137
968181 Wp = 38
86393
YDOT = 7611
851805 meter/sec RA = 97
45258 deg
ZDOT = 180
088667 TA = 232
77786
MA = 232
89974
Ha = 189
046 n
mi
Hp = 181
121
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13392584
60 X = 4099303
46
Y = 2388939
31 feet Y = 773892
92 meter
Z = -17349738
08 Z = -5268327
49
XDOT = -3733
491408 XDOT = -1223
875224
YDOT = 24973
267078 feet/sec YDOT = 7598
646087 meter/sec
ZDOT = 590
842084 ZDOT = 174
351638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7474170
55 X = -2278127
18
Y = -11479163
39 feet Y = -3498849
00 meter
Z = -17275628
70 Z = -5265611
63
XDOT = 19947
364976 XDOT = 6079
956845
YDOT = -13794
908945 feet/sec YDOT = -4204
688246 meter/sec
ZDOT = 570
540245 ZDOT = 173
900667
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 99115U 06255
41163570
00014500 00000-0 95600-4 0 9084
2 99115 51
6371 98
1318 0012658 328
1663 31
8735 15
75936999 450
Satellite: SHUTTLE
Catalog Number: 99115
Epoch time: 06255
41163570 = yrday
fracday
Element set: 908
Inclination: 51
6371 deg
RA of node: 98
1318 deg
Eccentricity:
0012658
Arg of perigee: 328
1663 deg
Mean anomaly: 31
8735 deg
Mean motion: 15
75936999 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 45
Checksum: 327
Coasting Arc #10 (begining on orbit 60)
---------------------------------------
Vector Time (GMT): 2006/256/09:35:36
519
Vector Time (MET): 003/18:20:41
547
Weight (LBS) : 248248
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2283896
72 A = 6723737
75 meter
Y = -5761437
88 meter E =
0008322
Z = -2617658
93 I = 51
96316
XDOT = 3963
013639 Wp = 345
30606
YDOT = 3969
562106 meter/sec RA = 92
32928 deg
ZDOT = -5267
747121 TA = 224
29800
MA = 224
36463
Ha = 189
142 n
mi
Hp = 180
942
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7493099
49 X = 2360868
35
Y = -18902355
26 feet Y = -5735467
69 meter
Z = -8588119
84 Z = -2606376
78
XDOT = 13002
013252 XDOT = 3943
920804
YDOT = 13023
497722 feet/sec YDOT = 4013
772007 meter/sec
ZDOT = -17282
634912 ZDOT = -5248
541047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18638832
31 X = -5681116
09
Y = 8169812
72 feet Y = 2490158
92 meter
Z = -8546898
07 Z = -2605094
53
XDOT = 409
588130 XDOT = 124
842462
YDOT = -17110
145298 feet/sec YDOT = -5215
172287 meter/sec
ZDOT = -17210
555682 ZDOT = -5245
777372
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 99115U 06256
42622211
00014500 00000-0 95600-4 0 9099
2 99115 51
6372 92
9061 0012688 331
1831 28
8631 15
75928543 617
Satellite: SHUTTLE
Catalog Number: 99115
Epoch time: 06256
42622211 = yrday
fracday
Element set: 909
Inclination: 51
6372 deg
RA of node: 92
9061 deg
Eccentricity:
0012688
Arg of perigee: 331
1831 deg
Mean anomaly: 28
8631 deg
Mean motion: 15
75928543 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 61
Checksum: 299
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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