Date:
July 14th 2006
SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2006/185/18:37:54 951 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 79 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 22 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 19144
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
196/10:37:01
471 0
0 0
0 0
0
010/15:59:06
520 0
0 0
0 190
2
000/00:00:00
000 0
0 0
0 176
9
196/11:04:57
051 -0
7 1
0 1
0
010/16:27:02
100 -0
7 -0
0 190
8
000/00:00:04
199 -0
0 -0
0 176
9
196/19:24:12
063 0
0 0
0 0
0
011/00:46:17
111 0
0 0
0 190
7
000/00:00:00
000 0
0 0
0 176
5
197/09:47:56
548 0
7 -0
8 0
8
011/15:10:01
596 0
3 0
0 190
3
000/00:00:03
193 -0
2 -0
0 176
3
197/17:58:54
947 -31
7 -49
0 49
0
011/23:20:59
996 11
9 -0
0 188
1
000/00:00:32
191 35
4 0
9 151
6
Coasting Arc #1 (begining on orbit 141)
---------------------------------------
Vector Time (GMT): 2006/194/15:40:41
000
Vector Time (MET): 008/21:02:46
049
Weight (LBS) : 218928
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2726802
98 A = 6713704
11 meter
Y = -3190960
81 meter E =
0025310
Z = -5261560
84 I = 51
85235
XDOT = 5250
144885 Wp = 79
70506
YDOT = 5574
498640 meter/sec RA = 50
58685 deg
ZDOT = -658
105465 TA = 184
03395
MA = 184
05439
Ha = 190
364 n
mi
Hp = 176
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8946204
00 X = 2787885
28
Y = -10469031
52 feet Y = -3160087
20 meter
Z = -17262338
71 Z = -5248166
57
XDOT = 17224
884793 XDOT = 5190
538136
YDOT = 18289
037532 feet/sec YDOT = 5632
948367 meter/sec
ZDOT = -2159
138664 ZDOT = -632
744622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11329037
08 X = -3453090
50
Y = 7936576
90 feet Y = 2419068
64 meter
Z = -17212994
82 Z = -5246520
82
XDOT = -11655
037589 XDOT = -3552
455457
YDOT = -21126
564919 feet/sec YDOT = -6439
376987 meter/sec
ZDOT = -2064
304337 ZDOT = -629
199962
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 29251U 06028A 06194
67019726
00014500 00000-0 95600-4 0 9009
2 29251 51
6296 51
0599 0010598 72
8047 287
4277 15
76297678 1422
Satellite: SHUTTLE
Catalog Number: 29251
Epoch time: 06194
67019726 = yrday
fracday
Element set: 900
Inclination: 51
6296 deg
RA of node: 51
0599 deg
Eccentricity:
0010598
Arg of perigee: 72
8047 deg
Mean anomaly: 287
4277 deg
Mean motion: 15
76297678 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 142
Checksum: 328
Coasting Arc #2 (begining on orbit 157)
---------------------------------------
Vector Time (GMT): 2006/195/15:45:43
190
Vector Time (MET): 009/21:07:48
239
Weight (LBS) : 236960
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3243711
03 A = 6723745
36 meter
Y = -5539716
53 meter E =
0014718
Z = -2006973
41 I = 51
86770
XDOT = 5176
749065 Wp = 99
48902
YDOT = -1013
929313 meter/sec RA = 45
44259 deg
ZDOT = -5605
116400 TA = 102
80456
MA = 102
64006
Ha = 190
292 n
mi
Hp = 176
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10642096
56 X = -3171696
95
Y = -18174923
01 feet Y = -5575631
31 meter
Z = -6584558
42 Z = -2022556
97
XDOT = 16984
084860 XDOT = 5214
943624
YDOT = -3326
539742 feet/sec YDOT = -955
753092 meter/sec
ZDOT = -18389
489501 ZDOT = -5579
875663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6621472
34 X = 2018224
77
Y = 19974080
56 feet Y = 6088099
75 meter
Z = -6643091
53 Z = -2024814
30
XDOT = -15946
987465 XDOT = -4860
641779
YDOT = -758
422115 feet/sec YDOT = -231
167061 meter/sec
ZDOT = -18295
897458 ZDOT = -5576
589545
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 29251U 06028A 06195
68454493
00014500 00000-0 95600-4 0 9016
2 29251 51
6296 45
8303 0010539 75
7073 284
5261 15
76334684 1589
Satellite: SHUTTLE
Catalog Number: 29251
Epoch time: 06195
68454493 = yrday
fracday
Element set: 901
Inclination: 51
6296 deg
RA of node: 45
8303 deg
Eccentricity:
0010539
Arg of perigee: 75
7073 deg
Mean anomaly: 284
5261 deg
Mean motion: 15
76334684 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 158
Checksum: 312
Coasting Arc #3 (begining on orbit 169)
---------------------------------------
Vector Time (GMT): 2006/196/10:37:01
471
Vector Time (MET): 010/15:59:06
520
Weight (LBS) : 236917
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5622431
07 A = 6724784
02 meter
Y = 3349485
68 meter E =
0017175
Z = -1532166
14 I = 51
85743
XDOT = -1345
110678 Wp = 56
63267
YDOT = 4885
954638 meter/sec RA = 41
37789 deg
ZDOT = 5800
839485 TA = 286
51908
MA = 286
70769
Ha = 190
166 n
mi
Hp = 176
890
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18446296
16 X = 5591954
02
Y = 10989126
25 feet Y = 3412266
89 meter
Z = -5026791
81 Z = -1504926
39
XDOT = -4413
092777 XDOT = -1427
893044
YDOT = 16030
034902 feet/sec YDOT = 4870
429834 meter/sec
ZDOT = 19031
625608 ZDOT = 5794
104666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10444226
60 X = 3183400
27
Y = -18787108
61 feet Y = -5726310
70 meter
Z = -4925246
65 Z = -1501215
18
XDOT = 14785
158736 XDOT = 4506
516383
YDOT = 3285
310459 feet/sec YDOT = 1001
362628 meter/sec
ZDOT = 19007
215087 ZDOT = 5793
399158
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 29251U 06028A 06196
44529607
00014500 00000-0 95600-4 0 9022
2 29251 51
6329 41
9144 0009733 73
7752 286
4483 15
76252375 1709
Satellite: SHUTTLE
Catalog Number: 29251
Epoch time: 06196
44529607 = yrday
fracday
Element set: 902
Inclination: 51
6329 deg
RA of node: 41
9144 deg
Eccentricity:
0009733
Arg of perigee: 73
7752 deg
Mean anomaly: 286
4483 deg
Mean motion: 15
76252375 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 170
Checksum: 308
Coasting Arc #4 (begining on orbit 170)
---------------------------------------
Vector Time (GMT): 2006/196/11:04:59
151
Vector Time (MET): 010/16:27:04
199
Weight (LBS) : 236890
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3051234
47 A = 6714238
31 meter
Y = 2825933
17 meter E =
0013083
Z = 5260573
10 I = 51
81954
XDOT = -5585
483577 Wp = 74
59182
YDOT = -5307
361446 meter/sec RA = 41
28886 deg
ZDOT = -384
423511 TA = 19
06723
MA = 19
01830
Ha = 190
787 n
mi
Hp = 176
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10010611
79 X = -3108201
11
Y = 9271434
28 feet Y = 2791450
33 meter
Z = 17259098
11 Z = 5245612
49
XDOT = -18325
077352 XDOT = -5523
778437
YDOT = -17412
603168 feet/sec YDOT = -5369
553874 meter/sec
ZDOT = -1261
231991 ZDOT = -411
408202
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10690945
23 X = 3258600
11
Y = 8589410
69 feet Y = 2618052
38 meter
Z = 17203895
60 Z = 5243747
38
XDOT = -13820
452580 XDOT = -4212
473946
YDOT = 19957
631064 feet/sec YDOT = 6083
085948 meter/sec
ZDOT = -1362
068545 ZDOT = -415
158493
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 29251U 06028A 06196
50870155
00014500 00000-0 95600-4 0 9037
2 29251 51
6327 41
5875 0010468 75
9847 284
2480 15
76073793 1719
Satellite: SHUTTLE
Catalog Number: 29251
Epoch time: 06196
50870155 = yrday
fracday
Element set: 903
Inclination: 51
6327 deg
RA of node: 41
5875 deg
Eccentricity:
0010468
Arg of perigee: 75
9847 deg
Mean anomaly: 284
2480 deg
Mean motion: 15
76073793 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 171
Checksum: 313
Coasting Arc #5 (begining on orbit 175)
---------------------------------------
Vector Time (GMT): 2006/196/19:24:12
063
Vector Time (MET): 011/00:46:17
111
Weight (LBS) : 236869
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1893134
76 A = 6714075
77 meter
Y = -3779535
32 meter E =
0025610
Z = -5238430
37 I = 51
81309
XDOT = 6294
351583 Wp = 81
74790
YDOT = 4327
527564 meter/sec RA = 39
51602 deg
ZDOT = -847
497210 TA = 180
18650
MA = 180
18746
Ha = 190
662 n
mi
Hp = 176
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6211072
05 X = 1960756
75
Y = -12400050
25 feet Y = -3757959
53 meter
Z = -17186451
33 Z = -5229069
93
XDOT = 20650
759787 XDOT = 6249
548313
YDOT = 14197
925080 feet/sec YDOT = 4397
751634 meter/sec
ZDOT = -2780
502658 ZDOT = -817
027938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4038644
21 X = 1230978
76
Y = 13311859
85 feet Y = 4057454
88 meter
Z = -17152157
65 Z = -5227977
65
XDOT = -23769
817557 XDOT = -7245
040391
YDOT = 3774
903414 feet/sec YDOT = 1150
590561 meter/sec
ZDOT = -2666
847979 ZDOT = -812
855264
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 29251U 06028A 06196
82573206
00014500 00000-0 95600-4 0 9040
2 29251 51
6331 39
9520 0010905 79
9085 280
3309 15
76197382 1769
Satellite: SHUTTLE
Catalog Number: 29251
Epoch time: 06196
82573206 = yrday
fracday
Element set: 904
Inclination: 51
6331 deg
RA of node: 39
9520 deg
Eccentricity:
0010905
Arg of perigee: 79
9085 deg
Mean anomaly: 280
3309 deg
Mean motion: 15
76197382 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 176
Checksum: 306
Coasting Arc #6 (begining on orbit 185)
---------------------------------------
Vector Time (GMT): 2006/197/09:47:58
144
Vector Time (MET): 011/15:10:03
193
Weight (LBS) : 236848
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -249147
63 A = 6715052
25 meter
Y = 4590514
78 meter E =
0016028
Z = 4881529
11 I = 51
80508
XDOT = -6816
640609 Wp = 95
76813
YDOT = -2803
579094 meter/sec RA = 36
44633 deg
ZDOT = 2280
590659 TA = 332
09607
MA = 332
18193
Ha = 190
335 n
mi
Hp = 176
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -817413
48 X = -324238
21
Y = 15060744
03 feet Y = 4587304
15 meter
Z = 16015515
45 Z = 4880137
00
XDOT = -22364
306461 XDOT = -6795
822348
YDOT = -9198
094141 feet/sec YDOT = -2879
785447 meter/sec
ZDOT = 7482
252818 ZDOT = 2247
525992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14696563
14 X = 4479512
44
Y = 3413628
75 feet Y = 1040474
04 meter
Z = 16010905
08 Z = 4880123
87
XDOT = -12569
816445 XDOT = -3831
280052
YDOT = 19477
616963 feet/sec YDOT = 5936
777650 meter/sec
ZDOT = 7359
148463 ZDOT = 2243
068452
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 29251U 06028A 06197
45972805
00014500 00000-0 95600-4 0 9059
2 29251 51
6336 36
6870 0010582 80
3547 279
8813 15
76354903 1864
Satellite: SHUTTLE
Catalog Number: 29251
Epoch time: 06197
45972805 = yrday
fracday
Element set: 905
Inclination: 51
6336 deg
RA of node: 36
6870 deg
Eccentricity:
0010582
Arg of perigee: 80
3547 deg
Mean anomaly: 279
8813 deg
Mean motion: 15
76354903 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 186
Checksum: 320
Coasting Arc #7 (begining on orbit 190)
---------------------------------------
Vector Time (GMT): 2006/197/17:59:11
043
Vector Time (MET): 011/23:21:16
091
Weight (LBS) : 235710
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3992083
93 A = 6697219
81 meter
Y = -4920007
04 meter E =
0044118
Z = -2255491
22 I = 51
82423
XDOT = 5132
894448 Wp = 42
93752
YDOT = -1673
353437 meter/sec RA = 34
69049 deg
ZDOT = -5465
581324 TA = 162
31552
MA = 162
16146
Ha = 188
075 n
mi
Hp = 151
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13097388
21 X = -3925745
09
Y = -16141755
38 feet Y = -4964332
75 meter
Z = -7399905
59 Z = -2274724
12
XDOT = 16840
204881 XDOT = 5177
797714
YDOT = -5490
004715 feet/sec YDOT = -1615
630793 meter/sec
ZDOT = -17931
697258 ZDOT = -5440
537136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18410754
33 X = 5611597
92
Y = 9595369
32 feet Y = 2924668
57 meter
Z = -7471911
40 Z = -2277438
59
XDOT = -12644
039721 XDOT = -3853
903307
YDOT = 10447
121411 feet/sec YDOT = 3184
282606 meter/sec
ZDOT = -17838
916020 ZDOT = -5437
301603
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 29251U 06028A 06197
77657068
00014500 00000-0 95600-4 0 9066
2 29251 51
6330 35
0477 0044827 35
7901 324
6258 15
85547133 1918
Satellite: SHUTTLE
Catalog Number: 29251
Epoch time: 06197
77657068 = yrday
fracday
Element set: 906
Inclination: 51
6330 deg
RA of node: 35
0477 deg
Eccentricity:
0044827
Arg of perigee: 35
7901 deg
Mean anomaly: 324
6258 deg
Mean motion: 15
85547133 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 191
Checksum: 311
Coasting Arc #8 (begining on orbit 206)
---------------------------------------
Vector Time (GMT): 2006/198/18:04:07
138
Vector Time (MET): 012/23:26:12
187
Weight (LBS) : 235710
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5948750
35 A = 6699371
86 meter
Y = -3103282
89 meter E =
0045937
Z = 280908
62 I = 51
80731
XDOT = 1951
639135 Wp = 55
28737
YDOT = -4352
957280 meter/sec RA = 29
43720 deg
ZDOT = -6037
934724 TA = 121
66170
MA = 121
21284
Ha = 188
095 n
mi
Hp = 151
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19516897
49 X = -5914927
25
Y = -10181374
30 feet Y = -3169698
82 meter
Z = 921616
21 Z = 252091
44
XDOT = 6403
015536 XDOT = 2029
560917
YDOT = -14281
355906 feet/sec YDOT = -4330
668582 meter/sec
ZDOT = -19809
497125 ZDOT = -6028
265111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22006101
92 X = 6707459
86
Y = 698228
88 feet Y = 212820
16 meter
Z = 814248
93 Z = 248183
07
XDOT = 383
749972 XDOT = 116
966991
YDOT = 14087
493346 feet/sec YDOT = 4293
867972 meter/sec
ZDOT = -19774
121400 ZDOT = -6027
152203
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 29251U 06028A 06198
78500170
00014500 00000-0 95600-4 0 9070
2 29251 51
6330 29
7790 0044775 39
5768 320
8656 15
85580543 2071
Satellite: SHUTTLE
Catalog Number: 29251
Epoch time: 06198
78500170 = yrday
fracday
Element set: 907
Inclination: 51
6330 deg
RA of node: 29
7790 deg
Eccentricity:
0044775
Arg of perigee: 39
5768 deg
Mean anomaly: 320
8656 deg
Mean motion: 15
85580543 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 207
Checksum: 318
Coasting Arc #9 (begining on orbit 222)
---------------------------------------
Vector Time (GMT): 2006/199/18:08:04
867
Vector Time (MET): 013/23:30:09
916
Weight (LBS) : 235710
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5972404
83 A = 6695326
96 meter
Y = -69302
13 meter E =
0053829
Z = 3025695
38 I = 51
76836
XDOT = -2486
048665 Wp = 54
35154
YDOT = -5381
626930 meter/sec RA = 24
18619 deg
ZDOT = -4938
557548 TA = 90
52824
MA = 89
91142
Ha = 188
128 n
mi
Hp = 151
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19594504
02 X = -5985882
32
Y = -227369
20 feet Y = -136248
21 meter
Z = 9926822
11 Z = 2996648
79
XDOT = -8156
327642 XDOT = -2401
619784
YDOT = -17656
256331 feet/sec YDOT = -5408
988475 meter/sec
ZDOT = -16202
616627 ZDOT = -4950
430600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17501766
58 X = 5334538
45
Y = -8933874
26 feet Y = -2723044
87 meter
Z = 9818968
33 Z = 2992821
55
XDOT = 14699
581794 XDOT = 4480
432531
YDOT = 10604
951091 feet/sec YDOT = 3232
389093 meter/sec
ZDOT = -16247
344302 ZDOT = -4952
190543
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 29251U 06028A 06199
79339382
00014500 00000-0 95600-4 0 9088
2 29251 51
6331 24
5102 0044765 43
4108 317
0572 15
85639200 2231
Satellite: SHUTTLE
Catalog Number: 29251
Epoch time: 06199
79339382 = yrday
fracday
Element set: 908
Inclination: 51
6331 deg
RA of node: 24
5102 deg
Eccentricity:
0044765
Arg of perigee: 43
4108 deg
Mean anomaly: 317
0572 deg
Mean motion: 15
85639200 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 223
Checksum: 286
Coasting Arc #10 (begining on orbit 237)
---------------------------------------
Vector Time (GMT): 2006/200/18:11:55
371
Vector Time (MET): 014/23:34:00
419
Weight (LBS) : 235710
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3642563
57 A = 6688616
40 meter
Y = 2791680
00 meter E =
0051325
Z = 4845231
87 I = 51
72034
XDOT = -6194
673011 Wp = 47
87528
YDOT = -4033
812012 meter/sec RA = 18
96054 deg
ZDOT = -2283
639376 TA = 64
47571
MA = 63
94585
Ha = 188
035 n
mi
Hp = 150
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11950667
87 X = -3697085
34
Y = 9159055
12 feet Y = 2750589
80 meter
Z = 15896430
04 Z = 4827404
50
XDOT = -20323
730352 XDOT = -6137
955248
YDOT = -13234
291379 feet/sec YDOT = -4102
852753 meter/sec
ZDOT = -7492
255170 ZDOT = -2313
596016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5929731
34 X = 1807382
11
Y = -13915264
69 feet Y = -4241372
68 meter
Z = 15830569
66 Z = 4825157
63
XDOT = 23158
925226 XDOT = 7058
840409
YDOT = 1033
592270 feet/sec YDOT = 315
038924 meter/sec
ZDOT = -7603
962463 ZDOT = -2317
687759
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 29251U 06028A 06200
80174032
00014500 00000-0 95600-4 0 9093
2 29251 51
6335 19
2404 0044666 46
9254 313
5640 15
85750293 2380
Satellite: SHUTTLE
Catalog Number: 29251
Epoch time: 06200
80174032 = yrday
fracday
Element set: 909
Inclination: 51
6335 deg
RA of node: 19
2404 deg
Eccentricity:
0044666
Arg of perigee: 46
9254 deg
Mean anomaly: 313
5640 deg
Mean motion: 15
85750293 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 238
Checksum: 280
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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