SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2007/220/22:36:41 953 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : -0 16242
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
There are no maneuvers
Coasting Arc #1 (Orbit 178)
---------------------------------------
Vector Time (GMT): 2007/232/04:32:46
000
Vector Time (MET): 011/05:56:04
047
Weight (LBS) : 232369
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5405535
84 A = 6725068
79 meter
Y = -3337783
34 meter E =
0006898
Z = -2192020
83 I = 51
88311
XDOT = 1022
768219 Wp = 216
64211
YDOT = 5280
706849 meter/sec RA = 132
59931 deg
ZDOT = -5515
336923 TA = 347
85040
MA = 347
86703
Ha = 185
555 n
mi
Hp = 184
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17734697
64 X = 5453067
29
Y = -10950732
73 feet Y = -3277134
13 meter
Z = -7191669
37 Z = -2165645
31
XDOT = 3355
538775 XDOT = 990
497713
YDOT = 17325
153705 feet/sec YDOT = 5291
951668 meter/sec
ZDOT = -18094
937413 ZDOT = -5510
446702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8080555
99 X = 2462953
47
Y = -19250078
05 feet Y = -5867423
79 meter
Z = -7092056
56 Z = -2161658
84
XDOT = 11491
063255 XDOT = 3502
476080
YDOT = 11487
176357 feet/sec YDOT = 3501
291354 meter/sec
ZDOT = -18075
716869 ZDOT = -5509
478502
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 32008U 07035A 07232
21686823
00014500 00000-0 95600-4 0 9004
2 32008 51
6329 133
3483 0008307 263
8881 96
1337 15
75783427 1795
Satellite: SHUTTLE
Catalog Number: 32008
Epoch time: 07232
21686823 = yrday
fracday
Element set: 900
Inclination: 51
6329 deg
RA of node: 133
3483 deg
Eccentricity:
0008307
Arg of perigee: 263
8881 deg
Mean anomaly: 96
1337 deg
Mean motion: 15
75783427 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 179
Checksum: 297
Coasting Arc #2 (Orbit 194)
---------------------------------------
Vector Time (GMT): 2007/233/04:37:55
578
Vector Time (MET): 012/06:01:13
625
Weight (LBS) : 232369
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1146898
99 A = 6722239
72 meter
Y = -5746876
32 meter E =
0004455
Z = 3289103
50 I = 51
89212
XDOT = 5867
584558 Wp = 96
26628
YDOT = -1547
281993 meter/sec RA = 127
40344 deg
ZDOT = -4744
510908 TA = 45
26957
MA = 45
23331
Ha = 184
427 n
mi
Hp = 184
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3762791
98 X = 1195030
43
Y = -18854581
11 feet Y = -5733795
86 meter
Z = 10791021
98 Z = 3294791
94
XDOT = 19250
605506 XDOT = 5907
480793
YDOT = -5076
384492 feet/sec YDOT = -1481
513936 meter/sec
ZDOT = -15565
980669 ZDOT = -4715
909351
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8652311
83 X = -2637224
65
Y = -17156365
77 feet Y = -5229260
29 meter
Z = 10811873
15 Z = 3295458
93
XDOT = 10897
584597 XDOT = 3321
583785
YDOT = -15247
525860 feet/sec YDOT = -4647
445882 meter/sec
ZDOT = -15457
686274 ZDOT = -4711
502776
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 32008U 07035A 07233
23153800
00014500 00000-0 95600-4 0 9012
2 32008 51
6322 128
1226 0008309 269
2298 90
7914 15
75830186 1953
Satellite: SHUTTLE
Catalog Number: 32008
Epoch time: 07233
23153800 = yrday
fracday
Element set: 901
Inclination: 51
6322 deg
RA of node: 128
1226 deg
Eccentricity:
0008309
Arg of perigee: 269
2298 deg
Mean anomaly: 90
7914 deg
Mean motion: 15
75830186 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 195
Checksum: 273
Coasting Arc #3 (Orbit 210)
---------------------------------------
Vector Time (GMT): 2007/234/04:43:01
764
Vector Time (MET): 013/06:06:19
811
Weight (LBS) : 232369
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4157890
16 A = 6715464
25 meter
Y = -1024084
50 meter E =
0005313
Z = 5177638
04 I = 51
88492
XDOT = 3218
725252 Wp = 248
88940
YDOT = -6887
741791 meter/sec RA = 122
28901 deg
ZDOT = 1221
589920 TA = 189
47282
MA = 189
48284
Ha = 184
897 n
mi
Hp = 184
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13641371
93 X = -4171294
29
Y = -3359857
27 feet Y = -1070606
14 meter
Z = 16987001
45 Z = 5157406
50
XDOT = 10560
122219 XDOT = 3289
490394
YDOT = -22597
578056 feet/sec YDOT = -6851
391102 meter/sec
ZDOT = 4007
840944 ZDOT = 1237
398108
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12667591
56 X = -3861081
91
Y = 6285991
22 feet Y = 1915970
12 meter
Z = 16910124
95 Z = 5154206
08
XDOT = -6052
262512 XDOT = -1844
729614
YDOT = -23144
936564 feet/sec YDOT = -7054
576665 meter/sec
ZDOT = 4066
945745 ZDOT = 1239
605063
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 32008U 07035A 07234
24620289
00014500 00000-0 95600-4 0 9025
2 32008 51
6316 122
8965 0008337 273
0890 86
9320 15
75806800 2112
Satellite: SHUTTLE
Catalog Number: 32008
Epoch time: 07234
24620289 = yrday
fracday
Element set: 902
Inclination: 51
6316 deg
RA of node: 122
8965 deg
Eccentricity:
0008337
Arg of perigee: 273
0890 deg
Mean anomaly: 86
9320 deg
Mean motion: 15
75806800 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 211
Checksum: 275
Coasting Arc #4 (Orbit 225)
---------------------------------------
Vector Time (GMT): 2007/235/04:43:11
692
Vector Time (MET): 014/06:06:29
739
Weight (LBS) : 232369
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2787447
81 A = 6726755
06 meter
Y = 6102813
84 meter E =
0009331
Z = -388109
18 I = 51
93833
XDOT = -4473
424877 Wp = 356
27272
YDOT = -1658
533236 meter/sec RA = 117
14457 deg
ZDOT = 6050
159341 TA = 359
52098
MA = 359
52188
Ha = 185
251 n
mi
Hp = 184
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9145169
97 X = -2853525
95
Y = 20022355
11 feet Y = 6071306
98 meter
Z = -1273324
07 Z = -401810
78
XDOT = -14676
590804 XDOT = -4483
957039
YDOT = -5441
382008 feet/sec YDOT = -1708
563656 meter/sec
ZDOT = 19849
604137 ZDOT = 6028
401960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6299633
08 X = 1920128
16
Y = 21088157
68 feet Y = 6427670
46 meter
Z = -1324545
58 Z = -403721
49
XDOT = -13176
639310 XDOT = -4016
239662
YDOT = 5177
585840 feet/sec YDOT = 1578
128164 meter/sec
ZDOT = 19766
852906 ZDOT = 6024
936766
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 32008U 07035A 07235
19744003
00014500 00000-0 95600-4 0 9032
2 32008 51
6319 117
9983 0008291 275
6749 84
3469 15
75881468 2265
Satellite: SHUTTLE
Catalog Number: 32008
Epoch time: 07235
19744003 = yrday
fracday
Element set: 903
Inclination: 51
6319 deg
RA of node: 117
9983 deg
Eccentricity:
0008291
Arg of perigee: 275
6749 deg
Mean anomaly: 84
3469 deg
Mean motion: 15
75881468 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 226
Checksum: 315
Coasting Arc #5 (Orbit 241)
---------------------------------------
Vector Time (GMT): 2007/236/04:48:13
578
Vector Time (MET): 015/06:11:31
625
Weight (LBS) : 232369
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2590653
90 A = 6716631
78 meter
Y = 3814472
21 meter E =
0003985
Z = -4887458
70 I = 51
91538
XDOT = -4346
597942 Wp = 117
96057
YDOT = 5919
693440 meter/sec RA = 111
98216 deg
ZDOT = 2315
722761 TA = 174
50317
MA = 174
49879
Ha = 185
868 n
mi
Hp = 184
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8499520
67 X = 2571595
00
Y = 12514672
61 feet Y = 3843305
39 meter
Z = -16034969
48 Z = -4874919
61
XDOT = -14260
491935 XDOT = -4423
649486
YDOT = 19421
566404 feet/sec YDOT = 5870
708376 meter/sec
ZDOT = 7597
515620 ZDOT = 2294
420271
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14840180
60 X = 4523287
05
Y = 3188506
16 feet Y = 971856
68 meter
Z = -15986919
54 Z = -4872813
08
XDOT = 3189
024479 XDOT = 972
014661
YDOT = 22855
850098 feet/sec YDOT = 6966
463110 meter/sec
ZDOT = 7517
423829 ZDOT = 2291
310783
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 32008U 07035A 07236
21208280
00014500 00000-0 95600-4 0 9049
2 32008 51
6315 112
7720 0008444 281
5013 78
5203 15
75827219 2426
Satellite: SHUTTLE
Catalog Number: 32008
Epoch time: 07236
21208280 = yrday
fracday
Element set: 904
Inclination: 51
6315 deg
RA of node: 112
7720 deg
Eccentricity:
0008444
Arg of perigee: 281
5013 deg
Mean anomaly: 78
5203 deg
Mean motion: 15
75827219 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 242
Checksum: 253
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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