SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2010/134/18:20:08 955 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 80 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 80 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
145/15:23:22
242 11
4 -0
1 17
6
010/21:03:13
287 6
6 -0
0 194
0
000/00:00:12
574 11
6 -17
6 181
9
Coasting Arc #1 (Orbit 164)
---------------------------------------
Vector Time (GMT): 2010/145/01:58:36
000
Vector Time (MET): 010/07:38:27
045
Weight (LBS) : 220514
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3538637
26 A = 6725164
58 meter
Y = 4013380
82 meter E =
0015595
Z = 4076887
02 I = 51
57439
XDOT = -6442
461626 Wp = 30
11727
YDOT = -1786
561459 meter/sec RA = 348
59334 deg
ZDOT = -3813
611174 TA = 99
20289
MA = 99
02646
Ha = 192
466 n
mi
Hp = 183
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11609702
31 X = -3603057
76
Y = 13167259
91 feet Y = 3973449
07 meter
Z = 13375613
59 Z = 4059539
92
XDOT = -21136
685124 XDOT = -6403
478973
YDOT = -5861
422108 feet/sec YDOT = -1858
386559 meter/sec
ZDOT = -12511
847685 ZDOT = -3844
814726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13454883
78 X = -4101048
57
Y = -11356575
88 feet Y = -3461484
33 meter
Z = 13306511
45 Z = 4055824
69
XDOT = 4506
902540 XDOT = 1373
703894
YDOT = -20220
931789 feet/sec YDOT = -6163
340009 meter/sec
ZDOT = -12636
113014 ZDOT = -3851
487247
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 36572U 10019A 10145
12301315
00020000 00000-0 20000-3 0 9000
2 36572 51
6440 348
9210 0011304 347
3969 12
6910 15
73955012 1651
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10145
12301315 = yrday
fracday
Element set: 900
Inclination: 51
6440 deg
RA of node: 348
9210 deg
Eccentricity:
0011304
Arg of perigee: 347
3969 deg
Mean anomaly: 12
6910 deg
Mean motion: 15
73955012 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 165
Checksum: 252
Coasting Arc #2 (Orbit 173)
---------------------------------------
Vector Time (GMT): 2010/145/15:23:28
529
Vector Time (MET): 010/21:03:19
574
Weight (LBS) : 219942
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4284247
40 A = 6723350
68 meter
Y = 2584512
06 meter E =
0013265
Z = 4482276
08 I = 51
55234
XDOT = -5742
180619 Wp = 9
07042
YDOT = 4049
389236 meter/sec RA = 345
76447 deg
ZDOT = 3165
196910 TA = 49
35717
MA = 49
24191
Ha = 194
030 n
mi
Hp = 181
883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14055929
81 X = 4233254
00
Y = 8479370
28 feet Y = 2632135
44 meter
Z = 14705630
17 Z = 4502965
78
XDOT = -18839
175258 XDOT = -5802
411091
YDOT = 13285
397757 feet/sec YDOT = 3984
839627 meter/sec
ZDOT = 10384
504298 ZDOT = 3137
155016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2291735
14 X = 698520
87
Y = -16179830
67 feet Y = -4931612
39 meter
Z = 14788017
83 Z = 4507387
83
XDOT = 18476
611363 XDOT = 5631
671144
YDOT = 11971
546591 feet/sec YDOT = 3648
927401 meter/sec
ZDOT = 10272
807379 ZDOT = 3131
151689
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 36572U 10019A 10145
69444688
00020000 00000-0 20000-3 0 9014
2 36572 51
6440 345
9822 0017583 340
6204 19
4289 15
73989642 1740
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10145
69444688 = yrday
fracday
Element set: 901
Inclination: 51
6440 deg
RA of node: 345
9822 deg
Eccentricity:
0017583
Arg of perigee: 340
6204 deg
Mean anomaly: 19
4289 deg
Mean motion: 15
73989642 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 174
Checksum: 315
Coasting Arc #3 (Orbit 188)
---------------------------------------
Vector Time (GMT): 2010/146/15:24:07
947
Vector Time (MET): 011/21:03:58
992
Weight (LBS) : 219942
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4859413
54 A = 6729444
61 meter
Y = -3868065
22 meter E =
0020285
Z = -2558488
24 I = 51
54449
XDOT = 4924
838215 Wp = 357
82024
YDOT = 2708
111398 meter/sec RA = 340
57592 deg
ZDOT = 5278
178461 TA = 333
07664
MA = 333
18174
Ha = 194
365 n
mi
Hp = 181
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15942957
80 X = 4914734
67
Y = -12690502
71 feet Y = -3813414
70 meter
Z = -8393990
30 Z = -2534746
93
XDOT = 16157
605692 XDOT = 4868
548693
YDOT = 8884
879914 feet/sec YDOT = 2762
868410 meter/sec
ZDOT = 17316
858469 ZDOT = 5301
967411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18155278
61 X = -5533728
92
Y = -9337630
91 feet Y = -2846109
90 meter
Z = -8299418
23 Z = -2529662
68
XDOT = 794
954864 XDOT = 242
302243
YDOT = -16966
568591 feet/sec YDOT = -5171
410107 meter/sec
ZDOT = 17411
586358 ZDOT = 5307
051522
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 36572U 10019A 10146
64680877
00020000 00000-0 20000-3 0 9023
2 36572 51
6450 341
0926 0017579 344
6561 15
4067 15
73979475 1897
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10146
64680877 = yrday
fracday
Element set: 902
Inclination: 51
6450 deg
RA of node: 341
0926 deg
Eccentricity:
0017579
Arg of perigee: 344
6561 deg
Mean anomaly: 15
4067 deg
Mean motion: 15
73979475 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 189
Checksum: 321
Coasting Arc #4 (Orbit 204)
---------------------------------------
Vector Time (GMT): 2010/147/15:25:10
509
Vector Time (MET): 012/21:05:01
554
Weight (LBS) : 219942
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4150549
74 A = 6722138
59 meter
Y = -2288073
62 meter E =
0022289
Z = -4781846
83 I = 51
49224
XDOT = 5521
837894 Wp = 19
75566
YDOT = -4720
940980 meter/sec RA = 335
47069 deg
ZDOT = -2516
702975 TA = 225
42535
MA = 225
60750
Ha = 194
445 n
mi
Hp = 181
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13617289
19 X = -4101425
91
Y = -7506803
22 feet Y = -2334212
12 meter
Z = -15688473
87 Z = -4801891
56
XDOT = 18116
266056 XDOT = 5586
443784
YDOT = -15488
651510 feet/sec YDOT = -4658
830874 meter/sec
ZDOT = -8256
899524 ZDOT = -2489
721283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -927861
25 X = -282812
11
Y = 15440560
24 feet Y = 4706282
76 meter
Z = -15768292
38 Z = -4806175
52
XDOT = -20690
334280 XDOT = -6306
413889
YDOT = -9623
103333 feet/sec YDOT = -2933
121896 meter/sec
ZDOT = -8149
412873 ZDOT = -2483
941044
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 36572U 10019A 10147
66264701
00020000 00000-0 20000-3 0 9031
2 36572 51
6450 335
8768 0017669 348
4819 11
5937 15
74010473 2057
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10147
66264701 = yrday
fracday
Element set: 903
Inclination: 51
6450 deg
RA of node: 335
8768 deg
Eccentricity:
0017669
Arg of perigee: 348
4819 deg
Mean anomaly: 11
5937 deg
Mean motion: 15
74010473 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 205
Checksum: 299
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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