SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2009/241/03:59:36 958 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 70 ET - UTC (sec) : 66 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
253/00:08:53
330 1
9 -0
1 17
0
011/20:09:16
372 -12
3 0
0 192
2
000/00:00:12
743 11
6 -17
0 179
7
Coasting Arc #1 (Orbit 173)
---------------------------------------
Vector Time (GMT): 2009/252/01:17:33
000
Vector Time (MET): 010/21:17:56
042
Weight (LBS) : 232963
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 892721
90 A = 6720683
13 meter
Y = -4955723
76 meter E =
0014557
Z = 4436770
51 I = 51
35322
XDOT = 5816
102699 Wp = 73
56579
YDOT = 3921
277495 meter/sec RA = 235
41838 deg
ZDOT = 3205
078749 TA = 344
26271
MA = 344
30791
Ha = 191
423 n
mi
Hp = 179
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2928877
61 X = 926518
04
Y = -16258936
21 feet Y = -4945551
65 meter
Z = 14556333
68 Z = 4441189
71
XDOT = 19081
701767 XDOT = 5756
252168
YDOT = 12865
083645 feet/sec YDOT = 3985
982078 meter/sec
ZDOT = 10515
350226 ZDOT = 3233
188121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 884619
68 X = 269632
08
Y = -16481845
82 feet Y = -5023666
60 meter
Z = 14573413
72 Z = 4441976
50
XDOT = 19216
807981 XDOT = 5857
283073
YDOT = 10440
525344 feet/sec YDOT = 3182
272125 meter/sec
ZDOT = 10626
192794 ZDOT = 3238
863564
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 00128U 09252
10718062
00020000 00000-0 20000-3 0 9003
2 00128 51
6377 236
0350 0009354 36
2501 323
9295 15
75011526 1747
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09252
10718062 = yrday
fracday
Element set: 900
Inclination: 51
6377 deg
RA of node: 236
0350 deg
Eccentricity:
0009354
Arg of perigee: 36
2501 deg
Mean anomaly: 323
9295 deg
Mean motion: 15
75011526 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 174
Checksum: 242
Coasting Arc #2 (Orbit 188)
---------------------------------------
Vector Time (GMT): 2009/253/00:08:59
701
Vector Time (MET): 011/20:09:22
743
Weight (LBS) : 232573
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 808735
33 A = 6719922
34 meter
Y = -4810264
88 meter E =
0013859
Z = 4609096
78 I = 51
36713
XDOT = 6083
301623 Wp = 46
62690
YDOT = 3770
920422 meter/sec RA = 230
50035 deg
ZDOT = 2872
100456 TA = 14
92023
MA = 14
87938
Ha = 192
225 n
mi
Hp = 179
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2653331
12 X = 840074
03
Y = -15781708
94 feet Y = -4801045
80 meter
Z = 15121708
60 Z = 4613101
89
XDOT = 19958
338659 XDOT = 6026
730116
YDOT = 12371
786160 feet/sec YDOT = 3838
631236 meter/sec
ZDOT = 9422
901757 ZDOT = 2901
515954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5095123
94 X = 1552993
78
Y = -15155012
11 feet Y = -4619247
69 meter
Z = 15137169
29 Z = 4613809
20
XDOT = 16523
391029 XDOT = 5036
329586
YDOT = 15069
725366 feet/sec YDOT = 4593
252292 meter/sec
ZDOT = 9538
882064 ZDOT = 2907
451253
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 00128U 09253
05893100
00020000 00000-0 20000-3 0 9016
2 00128 51
6367 231
1401 0013431 11
5174 348
6294 15
75038481 1890
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09253
05893100 = yrday
fracday
Element set: 901
Inclination: 51
6367 deg
RA of node: 231
1401 deg
Eccentricity:
0013431
Arg of perigee: 11
5174 deg
Mean anomaly: 348
6294 deg
Mean motion: 15
75038481 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 189
Checksum: 248
Coasting Arc #3 (Orbit 203)
---------------------------------------
Vector Time (GMT): 2009/254/00:09:02
517
Vector Time (MET): 012/20:09:25
560
Weight (LBS) : 232573
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5536503
35 A = 6727109
21 meter
Y = -3118083
34 meter E =
0019071
Z = -2182974
04 I = 51
41263
XDOT = 863
166142 Wp = 24
45877
YDOT = -5347
356352 meter/sec RA = 225
29772 deg
ZDOT = 5482
905350 TA = 310
97977
MA = 311
14459
Ha = 192
330 n
mi
Hp = 179
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18164381
07 X = -5490620
33
Y = -10229932
21 feet Y = -3179739
23 meter
Z = -7161988
31 Z = -2209759
15
XDOT = 2831
909916 XDOT = 896
261852
YDOT = -17543
820054 feet/sec YDOT = -5337
518861 meter/sec
ZDOT = 17988
534614 ZDOT = 5487
179051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16443921
51 X = -5012107
28
Y = -12754212
62 feet Y = -3887484
01 meter
Z = -7267587
96 Z = -2215160
81
XDOT = 4316
624481 XDOT = 1315
707142
YDOT = -15762
150908 feet/sec YDOT = -4804
303597 meter/sec
ZDOT = 18005
019844 ZDOT = 5487
930048
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 00128U 09254
01065643
00020000 00000-0 20000-3 0 9027
2 00128 51
6379 226
2454 0013443 15
8435 344
3146 15
75028082 2049
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09254
01065643 = yrday
fracday
Element set: 902
Inclination: 51
6379 deg
RA of node: 226
2454 deg
Eccentricity:
0013443
Arg of perigee: 15
8435 deg
Mean anomaly: 344
3146 deg
Mean motion: 15
75028082 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 204
Checksum: 248
Coasting Arc #4 (Orbit 219)
---------------------------------------
Vector Time (GMT): 2009/255/00:09:06
343
Vector Time (MET): 013/20:09:29
385
Weight (LBS) : 232573
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -765658
53 A = 6718567
08 meter
Y = 4512001
05 meter E =
0023296
Z = -4938424
64 I = 51
40597
XDOT = -6578
837356 Wp = 46
48489
YDOT = -3392
535581 meter/sec RA = 220
17532 deg
ZDOT = -2069
927449 TA = 203
30667
MA = 203
41246
Ha = 192
495 n
mi
Hp = 179
085
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2512003
05 X = -792065
51
Y = 14803153
04 feet Y = 4503291
41 meter
Z = -16202180
56 Z = -4942208
32
XDOT = -21584
112060 XDOT = -6530
357101
YDOT = -11130
366079 feet/sec YDOT = -3465
832918 meter/sec
ZDOT = -6791
100555 ZDOT = -2101
769870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4291755
21 X = -1308126
99
Y = 14371872
45 feet Y = 4380546
72 meter
Z = -16216789
87 Z = -4942877
55
XDOT = -18894
830942 XDOT = -5759
144471
YDOT = -13482
732322 feet/sec YDOT = -4109
536812 meter/sec
ZDOT = -6916
634007 ZDOT = -2108
190045
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 00128U 09255
02581758
00020000 00000-0 20000-3 0 9030
2 00128 51
6380 221
0246 0013507 19
8066 340
3619 15
75062476 2202
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09255
02581758 = yrday
fracday
Element set: 903
Inclination: 51
6380 deg
RA of node: 221
0246 deg
Eccentricity:
0013507
Arg of perigee: 19
8066 deg
Mean anomaly: 340
3619 deg
Mean motion: 15
75062476 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 220
Checksum: 254
Coasting Arc #5 (Orbit 235)
---------------------------------------
Vector Time (GMT): 2009/256/00:14:11
069
Vector Time (MET): 014/20:14:34
111
Weight (LBS) : 232573
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5328635
52 A = 6729007
80 meter
Y = 4096931
01 meter E =
0013665
Z = -378555
86 I = 51
46477
XDOT = -3186
007154 Wp = 73
74113
YDOT = 3605
418594 meter/sec RA = 214
98407 deg
ZDOT = -6002
526428 TA = 110
38116
MA = 110
23432
Ha = 192
546 n
mi
Hp = 178
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17482400
01 X = 5284265
85
Y = 13441374
71 feet Y = 4156270
87 meter
Z = -1241981
16 Z = -352777
08
XDOT = -10452
779375 XDOT = -3196
927594
YDOT = 11828
801161 feet/sec YDOT = 3569
729799 meter/sec
ZDOT = -19693
328175 ZDOT = -6018
030529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16227142
10 X = 4946032
91
Y = 14940785
25 feet Y = 4553951
34 meter
Z = -1140253
06 Z = -347549
13
XDOT = -10257
465325 XDOT = -3126
475431
YDOT = 9680
820789 feet/sec YDOT = 2950
714176 meter/sec
ZDOT = -19754
127197 ZDOT = -6021
057970
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 00128U 09256
04096566
00020000 00000-0 20000-3 0 9042
2 00128 51
6374 215
8016 0013519 23
3313 336
8461 15
75092891 2365
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09256
04096566 = yrday
fracday
Element set: 904
Inclination: 51
6374 deg
RA of node: 215
8016 deg
Eccentricity:
0013519
Arg of perigee: 23
3313 deg
Mean anomaly: 336
8461 deg
Mean motion: 15
75092891 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 236
Checksum: 269
Coasting Arc #6 (Orbit 251)
---------------------------------------
Vector Time (GMT): 2009/257/00:14:19
852
Vector Time (MET): 015/20:14:42
894
Weight (LBS) : 232573
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2951947
37 A = 6717285
08 meter
Y = -3072176
14 meter E =
0016497
Z = 5187166
71 I = 51
45137
XDOT = 6245
680239 Wp = 33
79985
YDOT = 4423
629728 meter/sec RA = 209
81568 deg
ZDOT = -919
461501 TA = 65
05840
MA = 64
88707
Ha = 192
576 n
mi
Hp = 178
742
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9684866
71 X = 2960883
39
Y = -10079318
03 feet Y = -3039115
75 meter
Z = 17018263
50 Z = 5201528
91
XDOT = 20491
076898 XDOT = 6200
216810
YDOT = 14513
220894 feet/sec YDOT = 4493
218396 meter/sec
ZDOT = -3016
605975 ZDOT = -889
230579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10276731
48 X = 3132347
75
Y = -9373218
27 feet Y = -2856956
93 meter
Z = 17074605
62 Z = 5204339
79
XDOT = 18742
900201 XDOT = 5712
835981
YDOT = 15182
904564 feet/sec YDOT = 4627
749311 meter/sec
ZDOT = -2897
313770 ZDOT = -883
101237
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 00128U 09257
05610257
00020000 00000-0 20000-3 0 9054
2 00128 51
6383 210
5800 0013527 27
4545 332
7331 15
75078399 2525
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09257
05610257 = yrday
fracday
Element set: 905
Inclination: 51
6383 deg
RA of node: 210
5800 deg
Eccentricity:
0013527
Arg of perigee: 27
4545 deg
Mean anomaly: 332
7331 deg
Mean motion: 15
75078399 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 252
Checksum: 261
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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