SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2009/074/23:43:43 983 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 40 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
086/20:15:50
217 21
1 -15
6 21
9
011/20:32:06
234 4
4 -0
0 189
1
000/00:00:14
468 4
0 -15
4 182
7
Coasting Arc #1 (Orbit 178)
---------------------------------------
Vector Time (GMT): 2009/086/05:13:54
000
Vector Time (MET): 011/05:30:10
017
Weight (LBS) : 211584
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2871687
38 A = 6726338
71 meter
Y = 3580376
12 meter E =
0010687
Z = 4907273
84 I = 51
66431
XDOT = -6933
868191 Wp = 109
74528
YDOT = -2539
036920 meter/sec RA = 6
45445 deg
ZDOT = -2204
809541 TA = 1
64869
MA = 1
64517
Ha = 195
201 n
mi
Hp = 184
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9421546
52 X = -2935349
09
Y = 11746640
80 feet Y = 3547907
78 meter
Z = 16099979
80 Z = 4893168
12
XDOT = -22748
911388 XDOT = -6894
250287
YDOT = -8330
173621 feet/sec YDOT = -2616
354185 meter/sec
ZDOT = -7233
627104 ZDOT = -2238
397962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10401950
41 X = -3170514
48
Y = -10968651
84 feet Y = -3343245
08 meter
Z = 16045141
42 Z = 4890559
10
XDOT = 10427
729425 XDOT = 3178
371929
YDOT = -20664
111342 feet/sec YDOT = -6298
421137 meter/sec
ZDOT = -7364
945953 ZDOT = -2244
835527
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 34541U 09012A 09086
26182858
00010596 00000-0 82463-4 0 9002
2 34541 51
6420 6
7459 0008492 147
9537 212
2144 15
72392198 1797
Satellite: SHUTTLE
Catalog Number: 34541
Epoch time: 09086
26182858 = yrday
fracday
Element set: 900
Inclination: 51
6420 deg
RA of node: 6
7459 deg
Eccentricity:
0008492
Arg of perigee: 147
9537 deg
Mean anomaly: 212
2144 deg
Mean motion: 15
72392198 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 179
Checksum: 317
Coasting Arc #2 (Orbit 188)
---------------------------------------
Vector Time (GMT): 2009/086/20:15:57
451
Vector Time (MET): 011/20:32:13
468
Weight (LBS) : 211128
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3195245
59 A = 6719351
78 meter
Y = 3786550
83 meter E =
0012415
Z = 4546771
22 I = 51
64901
XDOT = -6766
396610 Wp = 188
89680
YDOT = 2031
148679 meter/sec RA = 3
28221 deg
ZDOT = 3052
609967 TA = 230
66458
MA = 230
77468
Ha = 189
128 n
mi
Hp = 182
740
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10483089
21 X = 3130578
69
Y = 12423067
02 feet Y = 3821920
76 meter
Z = 14917228
43 Z = 4562136
44
XDOT = -22199
463942 XDOT = -6803
435510
YDOT = 6663
873619 feet/sec YDOT = 1955
276067 meter/sec
ZDOT = 10015
124564 ZDOT = 3019
648393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3217445
65 X = 980677
43
Y = -15876864
46 feet Y = -4839268
29 meter
Z = 14977472
28 Z = 4565133
55
XDOT = 17940
334912 XDOT = 5468
214081
YDOT = 12995
831554 feet/sec YDOT = 3961
129458 meter/sec
ZDOT = 9886
560912 ZDOT = 3013
423766
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 34541U 09012A 09086
89726615
00010596 00000-0 82463-4 0 9017
2 34541 51
6404 3
4846 0013090 228
5349 131
4691 15
75323382 1892
Satellite: SHUTTLE
Catalog Number: 34541
Epoch time: 09086
89726615 = yrday
fracday
Element set: 901
Inclination: 51
6404 deg
RA of node: 3
4846 deg
Eccentricity:
0013090
Arg of perigee: 228
5349 deg
Mean anomaly: 131
4691 deg
Mean motion: 15
75323382 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 189
Checksum: 307
Coasting Arc #3 (Orbit 203)
---------------------------------------
Vector Time (GMT): 2009/087/20:16:13
354
Vector Time (MET): 012/20:32:29
371
Weight (LBS) : 211128
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6069624
76 A = 6726450
20 meter
Y = -1921640
79 meter E =
0006840
Z = -2171970
64 I = 51
64398
XDOT = 3317
148545 Wp = 240
66696
YDOT = 4243
670673 meter/sec RA = 358
09462 deg
ZDOT = 5499
040017 TA = 95
01832
MA = 94
94024
Ha = 188
944 n
mi
Hp = 183
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19913467
07 X = 6101212
92
Y = -6304595
77 feet Y = -1853590
23 meter
Z = -7125887
93 Z = -2142407
22
XDOT = 10883
033285 XDOT = 3242
734926
YDOT = 13922
804045 feet/sec YDOT = 4280
349259 meter/sec
ZDOT = 18041
469872 ZDOT = 5514
973869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17591263
58 X = -5361817
14
Y = -11334526
48 feet Y = -3454763
67 meter
Z = -7010587
17 Z = -2136826
97
XDOT = 3009
490511 XDOT = 917
292708
YDOT = -15901
846086 feet/sec YDOT = -4846
882687 meter/sec
ZDOT = 18103
957696 ZDOT = 5518
086306
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 34541U 09012A 09087
84881995
00010596 00000-0 82463-4 0 9027
2 34541 51
6415 358
5890 0012977 231
6774 128
3224 15
75313472 2041
Satellite: SHUTTLE
Catalog Number: 34541
Epoch time: 09087
84881995 = yrday
fracday
Element set: 902
Inclination: 51
6415 deg
RA of node: 358
5890 deg
Eccentricity:
0012977
Arg of perigee: 231
6774 deg
Mean anomaly: 128
3224 deg
Mean motion: 15
75313472 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 204
Checksum: 326
Coasting Arc #4 (Orbit 219)
---------------------------------------
Vector Time (GMT): 2009/088/20:16:17
240
Vector Time (MET): 013/20:32:33
257
Weight (LBS) : 211128
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2658745
09 A = 6717483
25 meter
Y = -3648043
44 meter E =
0004454
Z = -4975251
53 I = 51
58468
XDOT = 7033
828646 Wp = 152
77871
YDOT = -2442
020589 meter/sec RA = 352
98350 deg
ZDOT = -1972
840326 TA = 98
16653
MA = 98
11600
Ha = 188
560 n
mi
Hp = 183
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8722916
95 X = -2593585
30
Y = -11968646
47 feet Y = -3677410
94 meter
Z = -16323003
72 Z = -4988009
45
XDOT = 23076
865637 XDOT = 7070
196769
YDOT = -8011
878574 feet/sec YDOT = -2363
160949 meter/sec
ZDOT = -6472
573248 ZDOT = -1938
581159
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3454176
84 X = -1052833
10
Y = 14344691
64 feet Y = 4372262
01 meter
Z = -16373048
36 Z = -4990505
14
XDOT = -20094
813829 XDOT = -6124
899255
YDOT = -12056
985303 feet/sec YDOT = -3674
969120 meter/sec
ZDOT = -6338
971852 ZDOT = -1932
118621
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 34541U 09012A 09088
86379667
00010596 00000-0 82463-4 0 9039
2 34541 51
6416 353
3674 0012922 236
0094 123
9843 15
75347731 2200
Satellite: SHUTTLE
Catalog Number: 34541
Epoch time: 09088
86379667 = yrday
fracday
Element set: 903
Inclination: 51
6416 deg
RA of node: 353
3674 deg
Eccentricity:
0012922
Arg of perigee: 236
0094 deg
Mean anomaly: 123
9843 deg
Mean motion: 15
75347731 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 220
Checksum: 317
Coasting Arc #5 (Orbit 235)
---------------------------------------
Vector Time (GMT): 2009/089/20:16:28
322
Vector Time (MET): 014/20:32:44
339
Weight (LBS) : 211128
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6186453
91 A = 6727717
44 meter
Y = 2321960
57 meter E =
0013964
Z = 1214239
92 I = 51
58935
XDOT = -2720
118560 Wp = 177
46935
YDOT = -4179
705724 meter/sec RA = 347
80519 deg
ZDOT = -5877
185758 TA = 349
19539
MA = 349
22536
Ha = 188
380 n
mi
Hp = 183
248
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20296764
79 X = -6217857
28
Y = 7617980
87 feet Y = 2252604
47 meter
Z = 3983726
78 Z = 1184109
55
XDOT = -8924
273491 XDOT = -2644
627655
YDOT = -13712
945288 feet/sec YDOT = -4209
701657 meter/sec
ZDOT = -19282
105504 ZDOT = -5890
216793
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19205874
28 X = 5853950
48
Y = 10101930
21 feet Y = 3079068
33 meter
Z = 3866234
83 Z = 1178428
38
XDOT = -3638
348167 XDOT = -1108
968521
YDOT = 14302
100087 feet/sec YDOT = 4359
280107 meter/sec
ZDOT = -19333
247395 ZDOT = -5892
773806
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 34541U 09012A 09089
87875746
00010596 00000-0 82463-4 0 9041
2 34541 51
6412 348
1440 0013016 239
8509 120
1366 15
75356342 2360
Satellite: SHUTTLE
Catalog Number: 34541
Epoch time: 09089
87875746 = yrday
fracday
Element set: 904
Inclination: 51
6412 deg
RA of node: 348
1440 deg
Eccentricity:
0013016
Arg of perigee: 239
8509 deg
Mean anomaly: 120
1366 deg
Mean motion: 15
75356342 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 236
Checksum: 309
Coasting Arc #6 (Orbit 251)
---------------------------------------
Vector Time (GMT): 2009/090/20:16:45
477
Vector Time (MET): 015/20:33:01
494
Weight (LBS) : 211128
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2023697
00 A = 6716251
64 meter
Y = 3717246
18 meter E =
0011464
Z = 5223316
46 I = 51
52355
XDOT = -7117
874212 Wp = 231
53565
YDOT = 2833
327940 meter/sec RA = 342
67005 deg
ZDOT = 735
412644 TA = 211
41922
MA = 211
48775
Ha = 187
913 n
mi
Hp = 183
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6639425
85 X = 1956605
68
Y = 12195689
57 feet Y = 3739501
18 meter
Z = 17136865
02 Z = 5232984
68
XDOT = -23352
605682 XDOT = -7152
600459
YDOT = 9295
695342 feet/sec YDOT = 2753
537555 meter/sec
ZDOT = 2412
771142 ZDOT = 700
749513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4513420
10 X = 1375690
45
Y = -13082148
78 feet Y = -3987438
95 meter
Z = 17174847
44 Z = 5234893
50
XDOT = 21735
352556 XDOT = 6624
935459
YDOT = 10514
443737 feet/sec YDOT = 3204
802451 meter/sec
ZDOT = 2277
609430 ZDOT = 694
215354
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 34541U 09012A 09090
89370130
00010596 00000-0 82463-4 0 9053
2 34541 51
6422 342
9211 0013022 244
3559 115
6260 15
75407790 2526
Satellite: SHUTTLE
Catalog Number: 34541
Epoch time: 09090
89370130 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 342
9211 deg
Eccentricity:
0013022
Arg of perigee: 244
3559 deg
Mean anomaly: 115
6260 deg
Mean motion: 15
75407790 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 252
Checksum: 277
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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