Date:
June 3rd 2008
SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2008/152/21:02:11 970 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 69 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
153/14:25:24
974 11
5 17
6 17
8
000/17:23:13
004 7
5 -2
7 181
4
000/00:00:25
114 -11
3 -0
0 171
8
153/23:28:10
958 2
5 4
1 4
1
001/02:25:58
987 0
7 -0
0 183
5
000/00:00:18
051 -3
2 0
0 172
4
154/13:45:06
962 -4
1 7
3 7
3
001/16:42:54
992 3
0 -0
0 183
2
000/00:00:11
862 5
2 0
0 176
5
154/15:16:32
927 -5
0 8
9 8
9
001/18:14:20
957 3
7 -0
0 183
9
000/00:00:13
913 6
4 -0
1 180
4
154/16:33:26
474 -1
3 2
5 3
0
001/19:31:14
503 2
2 0
1 184
5
000/00:00:13
007 1
5 1
6 182
1
Coasting Arc #1 (Orbit 10)
---------------------------------------
Vector Time (GMT): 2008/153/11:52:42
000
Vector Time (MET): 000/14:50:30
030
Weight (LBS) : 249029
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2341113
86 A = 6697127
74 meter
Y = 5065190
99 meter E =
0013753
Z = -3710367
92 I = 51
96562
XDOT = -3976
983607 Wp = 70
47208
YDOT = 4993
177485 meter/sec RA = 96
53586 deg
ZDOT = 4324
419909 TA = 244
86082
MA = 245
00355
Ha = 177
550 n
mi
Hp = 165
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7680819
75 X = 2302324
78
Y = 16618080
67 feet Y = 5091154
33 meter
Z = -12173123
10 Z = -3699088
01
XDOT = -13047
846479 XDOT = -4053
530226
YDOT = 16381
815897 feet/sec YDOT = 4948
275943 meter/sec
ZDOT = 14187
729361 ZDOT = 4304
914105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18315004
92 X = 5582413
50
Y = -884418
10 feet Y = -269570
64 meter
Z = -12129258
94 Z = -3696998
12
XDOT = 10130
410171 XDOT = 3087
749020
YDOT = 17016
155198 feet/sec YDOT = 5186
524104 meter/sec
ZDOT = 14113
138505 ZDOT = 4301
684616
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 00124U 08153
50277131
00020000 00000-0 70000-3 0 9004
2 00124 51
6412 97
2990 0009288 50
9267 309
2726 15
84257678 114
Satellite: SHUTTLE
Catalog Number: 00124
Epoch time: 08153
50277131 = yrday
fracday
Element set: 900
Inclination: 51
6412 deg
RA of node: 97
2990 deg
Eccentricity:
0009288
Arg of perigee: 50
9267 deg
Mean anomaly: 309
2726 deg
Mean motion: 15
84257678 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 11
Checksum: 265
Coasting Arc #2 (Orbit 12)
---------------------------------------
Vector Time (GMT): 2008/153/14:25:37
531
Vector Time (MET): 000/17:23:25
561
Weight (LBS) : 248595
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2174881
00 A = 6710785
58 meter
Y = -6032765
57 meter E =
0014357
Z = -1956113
41 I = 51
97746
XDOT = 4092
179857 Wp = 152
14873
YDOT = 3297
027226 meter/sec RA = 96
02620 deg
ZDOT = -5647
255795 TA = 49
58924
MA = 49
46407
Ha = 181
445 n
mi
Hp = 171
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7135436
36 X = 2251681
34
Y = -19792537
97 feet Y = -6008015
10 meter
Z = -6417694
92 Z = -1945361
97
XDOT = 13425
786931 XDOT = 4082
441777
YDOT = 10817
018459 feet/sec YDOT = 3342
734733 meter/sec
ZDOT = -18527
742108 ZDOT = -5627
398703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21005100
37 X = -6402354
59
Y = -1402489
21 feet Y = -427478
71 meter
Z = -6376880
26 Z = -1943673
10
XDOT = 6538
577307 XDOT = 1992
958363
YDOT = -14468
132156 feet/sec YDOT = -4409
886681 meter/sec
ZDOT = -18451
039492 ZDOT = -5623
876837
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 00124U 08153
62897454
00020000 00000-0 70000-3 0 9014
2 00124 51
6380 96
6393 0007680 162
2458 197
8978 15
80965511 131
Satellite: SHUTTLE
Catalog Number: 00124
Epoch time: 08153
62897454 = yrday
fracday
Element set: 901
Inclination: 51
6380 deg
RA of node: 96
6393 deg
Eccentricity:
0007680
Arg of perigee: 162
2458 deg
Mean anomaly: 197
8978 deg
Mean motion: 15
80965511 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 13
Checksum: 292
Coasting Arc #3 (Orbit 18)
---------------------------------------
Vector Time (GMT): 2008/153/23:28:19
983
Vector Time (MET): 001/02:26:08
013
Weight (LBS) : 248477
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1057171
56 A = 6714292
94 meter
Y = -6575468
36 meter E =
0021003
Z = -752814
40 I = 51
98148
XDOT = 4617
029957 Wp = 156
22180
YDOT = 1422
754721 meter/sec RA = 94
06357 deg
ZDOT = -6019
705239 TA = 31
97502
MA = 31
84774
Ha = 183
516 n
mi
Hp = 172
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3468410
63 X = 1134278
02
Y = -21573058
92 feet Y = -6563215
21 meter
Z = -2469863
51 Z = -747492
34
XDOT = 15147
736080 XDOT = 4630
020605
YDOT = 4667
830448 feet/sec YDOT = 1474
458621 meter/sec
ZDOT = -19749
689105 ZDOT = -5997
243430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17446690
96 X = 5317751
40
Y = 13158173
57 feet Y = 4010611
30 meter
Z = -2449982
14 Z = -746754
56
XDOT = -10297
096909 XDOT = -3138
555138
YDOT = 10038
943571 feet/sec YDOT = 3059
870000 meter/sec
ZDOT = -19663
135001 ZDOT = -5993
323548
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 00124U 08154
00824156
00020000 00000-0 70000-3 0 9027
2 00124 51
6363 94
6663 0011195 170
9798 189
1572 15
80228018 193
Satellite: SHUTTLE
Catalog Number: 00124
Epoch time: 08154
00824156 = yrday
fracday
Element set: 902
Inclination: 51
6363 deg
RA of node: 94
6663 deg
Eccentricity:
0011195
Arg of perigee: 170
9798 deg
Mean anomaly: 189
1572 deg
Mean motion: 15
80228018 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 19
Checksum: 267
Coasting Arc #4 (Orbit 27)
---------------------------------------
Vector Time (GMT): 2008/154/13:45:12
893
Vector Time (MET): 001/16:43:00
923
Weight (LBS) : 248299
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1615827
90 A = 6716267
62 meter
Y = 6138259
09 meter E =
0003137
Z = -2199241
36 I = 51
97754
XDOT = -4369
361788 Wp = 103
74528
YDOT = 3125
646813 meter/sec RA = 90
97107 deg
ZDOT = 5519
463593 TA = 231
69846
MA = 231
72668
Ha = 183
192 n
mi
Hp = 176
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5301272
65 X = 1557752
56
Y = 20138645
30 feet Y = 6156003
89 meter
Z = -7215358
81 Z = -2191531
44
XDOT = -14335
176469 XDOT = -4430
801611
YDOT = 10254
746761 feet/sec YDOT = 3076
441554 meter/sec
ZDOT = 18108
476354 ZDOT = 5498
088144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19343740
75 X = 5895972
18
Y = -7741016
12 feet Y = -2359461
71 meter
Z = -7185143
86 Z = -2190031
85
XDOT = 11362
828592 XDOT = 3463
390155
YDOT = 11679
822684 feet/sec YDOT = 3560
009954 meter/sec
ZDOT = 18026
506205 ZDOT = 5494
479091
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 00124U 08154
57739489
00020000 00000-0 70000-3 0 9034
2 00124 51
6378 91
7213 0005427 191
7372 168
3668 15
78864584 284
Satellite: SHUTTLE
Catalog Number: 00124
Epoch time: 08154
57739489 = yrday
fracday
Element set: 903
Inclination: 51
6378 deg
RA of node: 91
7213 deg
Eccentricity:
0005427
Arg of perigee: 191
7372 deg
Mean anomaly: 168
3668 deg
Mean motion: 15
78864584 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 28
Checksum: 305
Coasting Arc #5 (Orbit 28)
---------------------------------------
Vector Time (GMT): 2008/154/15:16:39
884
Vector Time (MET): 001/18:14:27
913
Weight (LBS) : 248082
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1570152
57 A = 6721183
58 meter
Y = 6185546
85 meter E =
0006094
Z = -2097126
30 I = 51
97933
XDOT = -4391
992952 Wp = 1
39137
YDOT = 3002
441241 meter/sec RA = 90
64490 deg
ZDOT = 5573
739048 TA = 335
26238
MA = 335
29159
Ha = 183
858 n
mi
Hp = 180
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5151419
21 X = 1511055
78
Y = 20293788
86 feet Y = 6202775
16 meter
Z = -6880335
65 Z = -2089640
73
XDOT = -14409
425696 XDOT = -4452
317048
YDOT = 9850
529007 feet/sec YDOT = 2952
989124 meter/sec
ZDOT = 18286
545432 ZDOT = 5552
256353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15010670
37 X = 4575252
33
Y = -14610196
68 feet Y = -4453187
95 meter
Z = -6850980
43 Z = -2088178
84
XDOT = 14705
903277 XDOT = 4482
359319
YDOT = 6582
470803 feet/sec YDOT = 2006
337101 meter/sec
ZDOT = 18204
150714 ZDOT = 5548
625138
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 00124U 08154
64068684
00020000 00000-0 70000-3 0 9045
2 00124 51
6390 91
3941 0004253 286
1724 73
8973 15
77198658 299
Satellite: SHUTTLE
Catalog Number: 00124
Epoch time: 08154
64068684 = yrday
fracday
Element set: 904
Inclination: 51
6390 deg
RA of node: 91
3941 deg
Eccentricity:
0004253
Arg of perigee: 286
1724 deg
Mean anomaly: 73
8973 deg
Mean motion: 15
77198658 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 29
Checksum: 291
Coasting Arc #6 (Orbit 29)
---------------------------------------
Vector Time (GMT): 2008/154/16:33:32
977
Vector Time (MET): 001/19:31:21
007
Weight (LBS) : 247997
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4069833
06 A = 6712670
96 meter
Y = 1198515
84 meter E =
0008306
Z = -5208979
03 I = 51
94540
XDOT = -878
656907 Wp = 88
98745
YDOT = 7575
742445 meter/sec RA = 90
38036 deg
ZDOT = 1058
154668 TA = 191
05480
MA = 191
07306
Ha = 184
493 n
mi
Hp = 182
059
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13352470
67 X = 4081433
36
Y = 3932138
59 feet Y = 1244092
90 meter
Z = -17089826
21 Z = -5189178
98
XDOT = -2882
732634 XDOT = -968
445172
YDOT = 24854
798047 feet/sec YDOT = 7565
414567 meter/sec
ZDOT = 3471
636050 ZDOT = 1053
669409
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7602180
00 X = -2317144
46
Y = -11771107
13 feet Y = -3587833
45 meter
Z = -17013531
17 Z = -5185724
30
XDOT = 17593
496226 XDOT = 5362
497650
YDOT = -16348
743762 feet/sec YDOT = -4983
097099 meter/sec
ZDOT = 3455
052196 ZDOT = 1053
099909
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 00124U 08154
70404612
00020000 00000-0 70000-3 0 9058
2 00124 51
6382 91
0669 0006426 289
8886 70
1586 15
76740437 306
Satellite: SHUTTLE
Catalog Number: 00124
Epoch time: 08154
70404612 = yrday
fracday
Element set: 905
Inclination: 51
6382 deg
RA of node: 91
0669 deg
Eccentricity:
0006426
Arg of perigee: 289
8886 deg
Mean anomaly: 70
1586 deg
Mean motion: 15
76740437 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 30
Checksum: 271
Coasting Arc #7 (Orbit 45)
---------------------------------------
Vector Time (GMT): 2008/155/16:37:52
000
Vector Time (MET): 002/19:35:40
030
Weight (LBS) : 247997
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2047669
91 A = 6720024
99 meter
Y = -5546749
73 meter E =
0002317
Z = -3194310
35 I = 51
96885
XDOT = 4153
538245 Wp = 318
89582
YDOT = 4320
639484 meter/sec RA = 85
26590 deg
ZDOT = -4836
314770 TA = 258
22125
MA = 258
24724
Ha = 184
592 n
mi
Hp = 181
980
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6718077
15 X = 2125059
95
Y = -18197997
80 feet Y = -5523418
11 meter
Z = -10480020
83 Z = -3184175
85
XDOT = 13627
093981 XDOT = 4128
409741
YDOT = 14175
326390 feet/sec YDOT = 4366
947276 meter/sec
ZDOT = -15867
174442 ZDOT = -4816
196690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16681549
82 X = -5084536
39
Y = 9941399
06 feet Y = 3030138
43 meter
Z = -10441503
80 Z = -3182570
36
XDOT = -1090
073714 XDOT = -332
254468
YDOT = -18425
509002 feet/sec YDOT = -5616
095144 meter/sec
ZDOT = -15789
377755 ZDOT = -4812
602340
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 00124U 08155
71811984
00020000 00000-0 70000-3 0 9065
2 00124 51
6381 85
8384 0006523 292
8308 67
2167 15
76726259 466
Satellite: SHUTTLE
Catalog Number: 00124
Epoch time: 08155
71811984 = yrday
fracday
Element set: 906
Inclination: 51
6381 deg
RA of node: 85
8384 deg
Eccentricity:
0006523
Arg of perigee: 292
8308 deg
Mean anomaly: 67
2167 deg
Mean motion: 15
76726259 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 46
Checksum: 288
Coasting Arc #8 (Orbit 61)
---------------------------------------
Vector Time (GMT): 2008/156/16:42:40
683
Vector Time (MET): 003/19:40:28
713
Weight (LBS) : 247997
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2703132
27 A = 6722320
37 meter
Y = -5770031
77 meter E =
0007669
Z = 2132562
14 I = 51
97386
XDOT = 3741
322441 Wp = 103
07901
YDOT = -3810
469527 meter/sec RA = 80
07077 deg
ZDOT = -5552
703945 TA = 53
16094
MA = 53
09063
Ha = 184
763 n
mi
Hp = 181
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8868544
18 X = -2648769
62
Y = -18930550
42 feet Y = -5799956
27 meter
Z = 6996594
93 Z = 2119560
96
XDOT = 12274
679925 XDOT = 3810
627845
YDOT = -12501
540442 feet/sec YDOT = -3768
243143 meter/sec
ZDOT = -18217
532628 ZDOT = -5534
361008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4130878
36 X = -1259091
72
Y = 20509929
70 feet Y = 6251426
57 meter
Z = 6946062
44 Z = 2117159
83
XDOT = -15895
091782 XDOT = -4844
823975
YDOT = 2961
157375 feet/sec YDOT = 902
560768 meter/sec
ZDOT = -18147
262204 ZDOT = -5531
285520
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 00124U 08156
73218158
00020000 00000-0 70000-3 0 9073
2 00124 51
6385 80
6091 0006529 298
1405 61
9099 15
76787718 621
Satellite: SHUTTLE
Catalog Number: 00124
Epoch time: 08156
73218158 = yrday
fracday
Element set: 907
Inclination: 51
6385 deg
RA of node: 80
6091 deg
Eccentricity:
0006529
Arg of perigee: 298
1405 deg
Mean anomaly: 61
9099 deg
Mean motion: 15
76787718 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 62
Checksum: 291
Coasting Arc #9 (Orbit 77)
---------------------------------------
Vector Time (GMT): 2008/157/16:47:24
474
Vector Time (MET): 004/19:45:12
504
Weight (LBS) : 247997
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4126537
34 A = 6712677
16 meter
Y = 546332
75 meter E =
0005296
Z = 5269183
70 I = 51
93272
XDOT = -1625
265849 Wp = 324
05668
YDOT = -7513
852929 meter/sec RA = 74
93464 deg
ZDOT = -489
800223 TA = 130
59881
MA = 130
55272
Ha = 185
182 n
mi
Hp = 181
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13538508
33 X = -4157936
54
Y = 1792430
27 feet Y = 500010
72 meter
Z = 17287348
10 Z = 5249060
85
XDOT = -5332
237039 XDOT = -1538
744611
YDOT = -24651
748454 feet/sec YDOT = -7531
543708 meter/sec
ZDOT = -1606
956112 ZDOT = -497
487263
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12262767
29 X = 3737691
47
Y = 6228881
94 feet Y = 1898563
22 meter
Z = 17209938
59 Z = 5245589
28
XDOT = -9087
968349 XDOT = -2770
012753
YDOT = 22450
807707 feet/sec YDOT = 6843
006189 meter/sec
ZDOT = -1637
182137 ZDOT = -499
013115
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 00124U 08157
74630416
00020000 00000-0 70000-3 0 9081
2 00124 51
6377 75
3796 0006518 300
4827 59
5693 15
76644931 787
Satellite: SHUTTLE
Catalog Number: 00124
Epoch time: 08157
74630416 = yrday
fracday
Element set: 908
Inclination: 51
6377 deg
RA of node: 75
3796 deg
Eccentricity:
0006518
Arg of perigee: 300
4827 deg
Mean anomaly: 59
5693 deg
Mean motion: 15
76644931 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 78
Checksum: 295
Coasting Arc #10 (Orbit 93)
---------------------------------------
Vector Time (GMT): 2008/158/16:51:58
123
Vector Time (MET): 005/19:49:46
152
Weight (LBS) : 247997
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -120526
71 A = 6721054
68 meter
Y = 6088602
79 meter E =
0009675
Z = 2829372
84 I = 51
95147
XDOT = -5190
155008 Wp = 53
27767
YDOT = -2488
141920 meter/sec RA = 69
81097 deg
ZDOT = 5126
889926 TA = 339
07018
MA = 339
10976
Ha = 185
199 n
mi
Hp = 181
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -395428
84 X = -202345
97
Y = 19975730
93 feet Y = 6086796
95 meter
Z = 9282719
28 Z = 2828589
80
XDOT = -17028
067610 XDOT = -5186
851823
YDOT = -8163
195276 feet/sec YDOT = -2546
163761 meter/sec
ZDOT = 16820
505005 ZDOT = 5101
683819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11049503
02 X = 3367888
52
Y = -16647554
86 feet Y = -5074174
72 meter
Z = 9280219
16 Z = 2828610
80
XDOT = 8901
409565 XDOT = 2713
149636
YDOT = 15242
123291 feet/sec YDOT = 4645
799179 meter/sec
ZDOT = 16723
263969 ZDOT = 5097
250858
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 00124U 08158
76042275
00020000 00000-0 70000-3 0 9095
2 00124 51
6365 70
1497 0006623 303
0592 56
9936 15
76696834 948
Satellite: SHUTTLE
Catalog Number: 00124
Epoch time: 08158
76042275 = yrday
fracday
Element set: 909
Inclination: 51
6365 deg
RA of node: 70
1497 deg
Eccentricity:
0006623
Arg of perigee: 303
0592 deg
Mean anomaly: 56
9936 deg
Mean motion: 15
76696834 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 94
Checksum: 290
Coasting Arc #11 (Orbit 108)
---------------------------------------
Vector Time (GMT): 2008/159/16:56:34
749
Vector Time (MET): 006/19:54:22
778
Weight (LBS) : 247997
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4355770
95 A = 6721962
11 meter
Y = 4390669
76 meter E =
0007063
Z = -2621775
20 I = 51
94095
XDOT = -2090
820979 Wp = 349
24573
YDOT = 5218
414275 meter/sec RA = 64
61278 deg
ZDOT = 5270
119025 TA = 341
03921
MA = 341
06549
Ha = 185
579 n
mi
Hp = 181
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14290587
10 X = 4319086
07
Y = 14405084
53 feet Y = 4439173
83 meter
Z = -8601624
68 Z = -2600703
37
XDOT = -6859
648881 XDOT = -2174
619798
YDOT = 17120
781741 feet/sec YDOT = 5194
564059 meter/sec
ZDOT = 17290
416750 ZDOT = 5259
759255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5165497
31 X = -1574443
58
Y = -19658083
63 feet Y = -5991783
89 meter
Z = -8520133
36 Z = -2596936
65
XDOT = 13181
746701 XDOT = 4017
796395
YDOT = -10934
082122 feet/sec YDOT = -3332
708231 meter/sec
ZDOT = 17250
974195 ZDOT = 5258
096935
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 00124U 08159
71116015
00020000 00000-0 70000-3 0 9107
2 00124 51
6356 65
2465 0006576 305
9800 54
0755 15
76558258 1090
Satellite: SHUTTLE
Catalog Number: 00124
Epoch time: 08159
71116015 = yrday
fracday
Element set: 910
Inclination: 51
6356 deg
RA of node: 65
2465 deg
Eccentricity:
0006576
Arg of perigee: 305
9800 deg
Mean anomaly: 54
0755 deg
Mean motion: 15
76558258 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 109
Checksum: 264
Coasting Arc #12 (Orbit 124)
---------------------------------------
Vector Time (GMT): 2008/160/17:00:51
090
Vector Time (MET): 007/19:58:39
120
Weight (LBS) : 247997
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3362152
37 A = 6712812
19 meter
Y = -2447642
00 meter E =
0011165
Z = -5278238
66 I = 51
89582
XDOT = 4144
376033 Wp = 64
04294
YDOT = 6477
013504 meter/sec RA = 59
48733 deg
ZDOT = -359
444443 TA = 202
53058
MA = 202
57965
Ha = 185
650 n
mi
Hp = 181
655
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11030683
63 X = 3414912
95
Y = -8030321
53 feet Y = -2409748
70 meter
Z = -17317055
98 Z = -5261777
65
XDOT = 13597
034229 XDOT = 4073
387132
YDOT = 21250
044304 feet/sec YDOT = 6522
961424 meter/sec
ZDOT = -1179
279669 ZDOT = -339
482667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13599428
03 X = -4145105
66
Y = 1844272
56 feet Y = 562134
28 meter
Z = -17253889
10 Z = -5258985
40
XDOT = -1860
999289 XDOT = -567
232583
YDOT = -24160
616363 feet/sec YDOT = -7364
155867 meter/sec
ZDOT = -1101
883903 ZDOT = -335
854214
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 00124U 08160
72533959
00020000 00000-0 70000-3 0 9111
2 00124 51
6350 60
0174 0006450 310
1410 49
9189 15
76576766 1256
Satellite: SHUTTLE
Catalog Number: 00124
Epoch time: 08160
72533959 = yrday
fracday
Element set: 911
Inclination: 51
6350 deg
RA of node: 60
0174 deg
Eccentricity:
0006450
Arg of perigee: 310
1410 deg
Mean anomaly: 49
9189 deg
Mean motion: 15
76576766 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 125
Checksum: 254
Coasting Arc #13 (Orbit 140)
---------------------------------------
Vector Time (GMT): 2008/161/17:05:01
482
Vector Time (MET): 008/20:02:49
511
Weight (LBS) : 247997
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2322810
04 A = 6722926
69 meter
Y = -5972037
04 meter E =
0000582
Z = -2032758
95 I = 51
91472
XDOT = 5287
755465 Wp = 221
90736
YDOT = -151
801644 meter/sec RA = 54
35143 deg
ZDOT = -5595
789211 TA = 340
68494
MA = 340
68715
Ha = 185
766 n
mi
Hp = 181
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7620767
83 X = -2245982
41
Y = -19593297
38 feet Y = -5997582
20 meter
Z = -6669156
67 Z = -2043857
29
XDOT = 17348
279084 XDOT = 5316
243148
YDOT = -498
036889 feet/sec YDOT = -92
510918 meter/sec
ZDOT = -18358
888488 ZDOT = -5570
032227
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1795127
88 X = -547154
98
Y = 20932569
17 feet Y = 6380247
08 meter
Z = -6712385
51 Z = -2045935
10
XDOT = -14370
923360 XDOT = -4380
257440
YDOT = -7088
225404 feet/sec YDOT = -2160
491103 meter/sec
ZDOT = -18259
738568 ZDOT = -5565
568315
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 00124U 08161
73950798
00020000 00000-0 70000-3 0 9128
2 00124 51
6353 54
7885 0006545 314
8996 45
1637 15
76616932 1417
Satellite: SHUTTLE
Catalog Number: 00124
Epoch time: 08161
73950798 = yrday
fracday
Element set: 912
Inclination: 51
6353 deg
RA of node: 54
7885 deg
Eccentricity:
0006545
Arg of perigee: 314
8996 deg
Mean anomaly: 45
1637 deg
Mean motion: 15
76616932 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 141
Checksum: 292
Coasting Arc #14 (Orbit 156)
---------------------------------------
Vector Time (GMT): 2008/162/17:09:46
768
Vector Time (MET): 009/20:07:34
797
Weight (LBS) : 247997
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5389122
56 A = 6720389
66 meter
Y = -2234459
99 meter E =
0009401
Z = 3333557
36 I = 51
88614
XDOT = -391
210448 Wp = 61
42734
YDOT = -6089
988246 meter/sec RA = 49
15218 deg
ZDOT = -4700
169636 TA = 79
48063
MA = 79
37472
Ha = 186
080 n
mi
Hp = 181
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17680848
29 X = -5379929
75
Y = -7330905
49 feet Y = -2294673
25 meter
Z = 10936867
99 Z = 3307399
07
XDOT = -1283
498846 XDOT = -300
249605
YDOT = -19980
276398 feet/sec YDOT = -6093
853825 meter/sec
ZDOT = -15420
504055 ZDOT = -4701
849933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13256189
12 X = 4040486
44
Y = 13886135
55 feet Y = 4232494
12 meter
Z = 10835974
47 Z = 3302805
02
XDOT = -5982
803133 XDOT = -1823
558395
YDOT = 17787
224024 feet/sec YDOT = 5421
545882 meter/sec
ZDOT = -15427
480517 ZDOT = -4702
296061
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 00124U 08162
75368135
00020000 00000-0 70000-3 0 9130
2 00124 51
6350 49
5588 0006510 317
1736 42
8920 15
76481765 1576
Satellite: SHUTTLE
Catalog Number: 00124
Epoch time: 08162
75368135 = yrday
fracday
Element set: 913
Inclination: 51
6350 deg
RA of node: 49
5588 deg
Eccentricity:
0006510
Arg of perigee: 317
1736 deg
Mean anomaly: 42
8920 deg
Mean motion: 15
76481765 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 157
Checksum: 273
SPACE SHUTTLE ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics 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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