SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2010/039/09:14:06 981 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 77 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 07 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 07803
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 82)
---------------------------------------
Vector Time (GMT): 2010/044/12:25:48
000
Vector Time (MET): 005/03:11:41
019
Weight (LBS) : 210843
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1933243
93 A = 6714526
17 meter
Y = -3702490
91 meter E =
0010695
Z = 5261859
81 I = 51
82035
XDOT = 6484
773310 Wp = 334
85713
YDOT = -4121
835231 meter/sec RA = 144
57540 deg
ZDOT = -508
655416 TA = 120
01615
MA = 119
90999
Ha = 188
169 n
mi
Hp = 181
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6342663
80 X = -1917237
52
Y = -12147279
88 feet Y = -3724031
01 meter
Z = 17263319
59 Z = 5252507
31
XDOT = 21275
502987 XDOT = 6532
876357
YDOT = -13523
081466 feet/sec YDOT = -4049
012667 meter/sec
ZDOT = -1668
816983 ZDOT = -477
036498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 706029
52 X = 215197
80
Y = -13732185
57 feet Y = -4185570
16 meter
Z = 17226044
17 Z = 5250498
26
XDOT = 24207
047654 XDOT = 7378
308125
YDOT = -729
162149 feet/sec YDOT = -222
248623 meter/sec
ZDOT = -1543
471512 ZDOT = -470
450117
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 36394U 10004A 10044
56470161
00020000 00000-0 20000-3 0 9008
2 36394 51
6470 145
3259 0011239 320
8697 39
1653 15
75983743 830
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10044
56470161 = yrday
fracday
Element set: 900
Inclination: 51
6470 deg
RA of node: 145
3259 deg
Eccentricity:
0011239
Arg of perigee: 320
8697 deg
Mean anomaly: 39
1653 deg
Mean motion: 15
75983743 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 83
Checksum: 295
Coasting Arc #2 (Orbit 98)
---------------------------------------
Vector Time (GMT): 2010/045/12:30:29
358
Vector Time (MET): 006/03:16:22
377
Weight (LBS) : 210828
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5763046
86 A = 6723408
88 meter
Y = 2154964
50 meter E =
0013931
Z = 2687337
38 I = 51
87417
XDOT = 316
806319 Wp = 30
50632
YDOT = -5664
351810 meter/sec RA = 139
45097 deg
ZDOT = 5221
653566 TA =
07806
MA =
07784
Ha = 188
415 n
mi
Hp = 181
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18907634
04 X = -5799781
85
Y = 7070093
49 feet Y = 2090280
47 meter
Z = 8816723
69 Z = 2659252
02
XDOT = 1039
390810 XDOT = 354
789638
YDOT = -18583
831399 feet/sec YDOT = -5660
594680 meter/sec
ZDOT = 17131
409336 ZDOT = 5223
284964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20023798
00 X = -6103253
63
Y = -2912803
34 feet Y = -887822
46 meter
Z = 8705317
56 Z = 2653380
79
XDOT = 9543
007032 XDOT = 2908
708543
YDOT = -14384
620560 feet/sec YDOT = -4384
432347 meter/sec
ZDOT = 17137
655168 ZDOT = 5223
557295
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 36394U 10004A 10045
57926368
00020000 00000-0 20000-3 0 9016
2 36394 51
6468 140
1016 0011203 325
3330 34
7103 15
76006092 998
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10045
57926368 = yrday
fracday
Element set: 901
Inclination: 51
6468 deg
RA of node: 140
1016 deg
Eccentricity:
0011203
Arg of perigee: 325
3330 deg
Mean anomaly: 34
7103 deg
Mean motion: 15
76006092 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 99
Checksum: 261
Coasting Arc #3 (Orbit 113)
---------------------------------------
Vector Time (GMT): 2010/046/12:35:35
940
Vector Time (MET): 007/03:21:28
959
Weight (LBS) : 210828
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2399500
65 A = 6723373
36 meter
Y = 5611964
88 meter E =
0012080
Z = -2802178
78 I = 51
89468
XDOT = -5739
602033 Wp = 351
90747
YDOT = 109
974943 meter/sec RA = 134
25403 deg
ZDOT = 5144
101387 TA = 336
07014
MA = 336
12624
Ha = 188
715 n
mi
Hp = 181
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7872377
45 X = -2448495
93
Y = 18411958
27 feet Y = 5584844
39 meter
Z = -9193499
94 Z = -2813954
49
XDOT = -18830
715331 XDOT = -5765
393960
YDOT = 360
810179 feet/sec YDOT = 45
614575 meter/sec
ZDOT = 16876
973056 ZDOT = 5116
156454
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15203399
18 X = -4633996
07
Y = 12998985
10 feet Y = 3962090
66 meter
Z = -9240022
45 Z = -2816358
84
XDOT = -16159
392094 XDOT = -4925
382710
YDOT = -7002
998946 feet/sec YDOT = -2134
514079 meter/sec
ZDOT = 16766
034989 ZDOT = 5110
287465
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 36394U 10004A 10046
53041041
00020000 00000-0 20000-3 0 9020
2 36394 51
6462 135
2044 0011364 328
8728 31
1762 15
75877808 1145
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10046
53041041 = yrday
fracday
Element set: 902
Inclination: 51
6462 deg
RA of node: 135
2044 deg
Eccentricity:
0011364
Arg of perigee: 328
8728 deg
Mean anomaly: 31
1762 deg
Mean motion: 15
75877808 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 114
Checksum: 272
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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