SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2007/296/15:38:18 960 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 77 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : -0 21018
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
310/19:54:47
174 22
5 -99
9 100
0
014/04:16:28
214 -91
4 -0
0 188
1
000/00:00:56
428 -33
5 3
2 124
7
Coasting Arc #1 (Orbit 206)
---------------------------------------
Vector Time (GMT): 2007/309/15:45:25
000
Vector Time (MET): 013/00:07:06
040
Weight (LBS) : 212431
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3430525
98 A = 6718330
43 meter
Y = -3414886
53 meter E =
0008115
Z = 4652911
62 I = 51
95083
XDOT = 2682
785953 Wp = 78
71440
YDOT = -6626
757718 meter/sec RA = 93
66301 deg
ZDOT = -2879
806327 TA = 39
64038
MA = 39
58108
Ha = 188
162 n
mi
Hp = 181
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11255006
50 X = -3414741
66
Y = -11203695
96 feet Y = -3453107
59 meter
Z = 15265458
08 Z = 4636284
33
XDOT = 8801
791185 XDOT = 2770
576754
YDOT = -21741
331095 feet/sec YDOT = -6596
308403 meter/sec
ZDOT = -9448
183486 ZDOT = -2866
559383
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9039594
29 X = 2755268
34
Y = -13131026
57 feet Y = -4002336
90 meter
Z = 15201778
22 Z = 4633502
00
XDOT = 22000
342468 XDOT = 6705
704384
YDOT = 4242
734363 feet/sec YDOT = 1293
185434 meter/sec
ZDOT = -9398
539624 ZDOT = -2864
674877
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 32272U 07050A 07309
69914689
00014500 00000-0 95600-4 0 9005
2 32272 51
6399 94
2223 0002132 161
7650 198
3591 15
75573192 2077
Satellite: SHUTTLE
Catalog Number: 32272
Epoch time: 07309
69914689 = yrday
fracday
Element set: 900
Inclination: 51
6399 deg
RA of node: 94
2223 deg
Eccentricity:
0002132
Arg of perigee: 161
7650 deg
Mean anomaly: 198
3591 deg
Mean motion: 15
75573192 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 207
Checksum: 303
Coasting Arc #2 (Orbit 222)
---------------------------------------
Vector Time (GMT): 2007/310/15:50:40
130
Vector Time (MET): 014/00:12:21
170
Weight (LBS) : 211785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3282229
93 A = 6719582
33 meter
Y = 3959201
63 meter E =
0011001
Z = 4319711
12 I = 51
95565
XDOT = -2893
400481 Wp = 118
14729
YDOT = -6227
062352 meter/sec RA = 88
56550 deg
ZDOT = 3497
111032 TA = 296
60759
MA = 296
72026
Ha = 188
035 n
mi
Hp = 181
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10768470
91 X = -3347183
20
Y = 12989506
65 feet Y = 3922185
76 meter
Z = 14172280
59 Z = 4303607
62
XDOT = -9492
783730 XDOT = -2840
638196
YDOT = -20429
994593 feet/sec YDOT = -6259
078836 meter/sec
ZDOT = 11473
461392 ZDOT = 3483
183058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15017254
91 X = -4577259
30
Y = -7803196
23 feet Y = -2378414
21 meter
Z = 14111448
17 Z = 4301169
40
XDOT = 17329
798046 XDOT = 5282
122445
YDOT = -12629
354736 feet/sec YDOT = -3849
427324 meter/sec
ZDOT = 11419
734439 ZDOT = 3480
735057
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 32272U 07050A 07310
71396872
00014500 00000-0 95600-4 0 9019
2 32272 51
6398 88
9984 0002148 167
7335 192
3882 15
75591896 2239
Satellite: SHUTTLE
Catalog Number: 32272
Epoch time: 07310
71396872 = yrday
fracday
Element set: 901
Inclination: 51
6398 deg
RA of node: 88
9984 deg
Eccentricity:
0002148
Arg of perigee: 167
7335 deg
Mean anomaly: 192
3882 deg
Mean motion: 15
75591896 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 223
Checksum: 329
Coasting Arc #3 (Orbit 224)
---------------------------------------
Vector Time (GMT): 2007/310/19:55:15
388
Vector Time (MET): 014/04:16:56
428
Weight (LBS) : 209712
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3760486
42 A = 6665934
25 meter
Y = 3096503
67 meter E =
0090898
Z = -4638493
44 I = 51
95104
XDOT = -2005
454856 Wp = 116
14790
YDOT = 6796
649511 meter/sec RA = 87
65036 deg
ZDOT = 2916
216194 TA = 182
72576
MA = 182
77564
Ha = 188
098 n
mi
Hp = 124
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12337553
87 X = 3748163
03
Y = 10159132
79 feet Y = 3138428
85 meter
Z = -15218154
34 Z = -4620254
62
XDOT = -6579
576300 XDOT = -2095
369985
YDOT = 22298
718868 feet/sec YDOT = 6773
752232 meter/sec
ZDOT = 9567
638432 ZDOT = 2906
254629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9077966
62 X = 2766964
23
Y = 13233762
70 feet Y = 4033650
87 meter
Z = -15148382
19 Z = -4617226
89
XDOT = -11651
979633 XDOT = -3551
523392
YDOT = 18883
973039 feet/sec YDOT = 5755
834982 meter/sec
ZDOT = 9530
507176 ZDOT = 2904
898587
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 32272U 07050A 07310
84083107
00014500 00000-0 95600-4 0 9028
2 32272 51
6396 88
3459 0080264 117
0308 243
9088 15
94220046 2251
Satellite: SHUTTLE
Catalog Number: 32272
Epoch time: 07310
84083107 = yrday
fracday
Element set: 902
Inclination: 51
6396 deg
RA of node: 88
3459 deg
Eccentricity:
0080264
Arg of perigee: 117
0308 deg
Mean anomaly: 243
9088 deg
Mean motion: 15
94220046 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 225
Checksum: 280
Coasting Arc #4 (Orbit 240)
---------------------------------------
Vector Time (GMT): 2007/311/19:59:21
374
Vector Time (MET): 015/04:21:02
414
Weight (LBS) : 209712
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4034170
09 A = 6665597
66 meter
Y = 2713360
85 meter E =
0090516
Z = -4647710
30 I = 51
94802
XDOT = -1350
992829 Wp = 119
51788
YDOT = 6966
542654 meter/sec RA = 82
36643 deg
ZDOT = 2892
932095 TA = 179
13605
MA = 179
12030
Ha = 187
771 n
mi
Hp = 124
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13235466
19 X = 4026149
76
Y = 8902102
53 feet Y = 2758366
41 meter
Z = -15248393
37 Z = -4628131
30
XDOT = -4432
391170 XDOT = -1442
740591
YDOT = 22856
111069 feet/sec YDOT = 6950
943634 meter/sec
ZDOT = 9491
247031 ZDOT = 2886
145607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10717375
60 X = 3266656
08
Y = 11909625
71 feet Y = 3630053
92 meter
Z = -15173568
16 Z = -4624903
57
XDOT = -9109
986614 XDOT = -2776
723920
YDOT = 20264
928057 feet/sec YDOT = 6176
750072 meter/sec
ZDOT = 9466
207696 ZDOT = 2885
300106
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 32272U 07050A 07311
84371472
00014500 00000-0 95600-4 0 9035
2 32272 51
6393 83
0383 0079933 120
9097 239
9967 15
94329828 2412
Satellite: SHUTTLE
Catalog Number: 32272
Epoch time: 07311
84371472 = yrday
fracday
Element set: 903
Inclination: 51
6393 deg
RA of node: 83
0383 deg
Eccentricity:
0079933
Arg of perigee: 120
9097 deg
Mean anomaly: 239
9967 deg
Mean motion: 15
94329828 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 241
Checksum: 318
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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