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 67)
---------------------------------------
Vector Time (GMT): 2010/043/13:36:59
999
Vector Time (MET): 004/04:22:53
018
Weight (LBS) : 210961
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1241310
51 A = 6714798
40 meter
Y = -4040429
54 meter E =
0011069
Z = 5222972
90 I = 51
79646
XDOT = 6913
007599 Wp = 333
66391
YDOT = -3274
288560 meter/sec RA = 149
45527 deg
ZDOT = -880
967441 TA = 124
76020
MA = 124
65595
Ha = 188
030 n
mi
Hp = 182
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4072541
05 X = -1221385
85
Y = -13256002
44 feet Y = -4054206
28 meter
Z = 17135737
85 Z = 5216991
15
XDOT = 22680
471126 XDOT = 6953
405118
YDOT = -10742
416537 feet/sec YDOT = -3196
717884 meter/sec
ZDOT = -2890
313126 ZDOT = -847
287031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -835998
48 X = -254812
34
Y = -13871806
43 feet Y = -4228126
60 meter
Z = 17111832
04 Z = 5215686
40
XDOT = 23612
414975 XDOT = 7197
064084
YDOT = -4860
207631 feet/sec YDOT = -1481
391286 meter/sec
ZDOT = -2756
760024 ZDOT = -840
260455
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 10043
61352300
00020000 00000-0 20000-3 0 9007
2 36394 51
6467 150
2244 0011341 316
6377 43
3894 15
75945350 686
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10043
61352300 = yrday
fracday
Element set: 900
Inclination: 51
6467 deg
RA of node: 150
2244 deg
Eccentricity:
0011341
Arg of perigee: 316
6377 deg
Mean anomaly: 43
3894 deg
Mean motion: 15
75945350 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 68
Checksum: 270
Coasting Arc #2 (Orbit 83)
---------------------------------------
Vector Time (GMT): 2010/044/13:42:18
663
Vector Time (MET): 005/04:28:11
682
Weight (LBS) : 210961
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5824847
84 A = 6722405
62 meter
Y = 1146785
10 meter E =
0011504
Z = 3137396
98 I = 51
84728
XDOT = 1487
141435 Wp = 31
38218
YDOT = -5782
705591 meter/sec RA = 144
33242 deg
ZDOT = 4876
383772 TA = 5
07196
MA = 5
06032
Ha = 188
321 n
mi
Hp = 181
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19110393
18 X = -5852485
07
Y = 3762418
30 feet Y = 1081460
47 meter
Z = 10293297
19 Z = 3109033
61
XDOT = 4879
072949 XDOT = 1528
039087
YDOT = -18972
131204 feet/sec YDOT = -5765
838210 meter/sec
ZDOT = 15998
634421 ZDOT = 4883
707461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19535214
71 X = -5954333
44
Y = -206224
20 feet Y = -62857
14 meter
Z = 10180753
60 Z = 3103093
70
XDOT = 8520
618711 XDOT = 2597
084583
YDOT = -16181
324900 feet/sec YDOT = -4932
067830 meter/sec
ZDOT = 16027
471485 ZDOT = 4885
173309
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
62811252
00020000 00000-0 20000-3 0 9016
2 36394 51
6464 145
0002 0011297 321
1574 38
8778 15
75960766 843
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10044
62811252 = yrday
fracday
Element set: 901
Inclination: 51
6464 deg
RA of node: 145
0002 deg
Eccentricity:
0011297
Arg of perigee: 321
1574 deg
Mean anomaly: 38
8778 deg
Mean motion: 15
75960766 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 84
Checksum: 286
Coasting Arc #3 (Orbit 98)
---------------------------------------
Vector Time (GMT): 2010/045/13:47:14
548
Vector Time (MET): 006/04:33:07
567
Weight (LBS) : 210961
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3301052
49 A = 6724034
91 meter
Y = 5336977
33 meter E =
0013420
Z = -2390846
87 I = 51
87634
XDOT = -5413
907808 Wp = 349
71043
YDOT = -929
176344 meter/sec RA = 139
13462 deg
ZDOT = 5409
148631 TA = 343
38110
MA = 343
42504
Ha = 188
423 n
mi
Hp = 181
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10830224
69 X = -3348902
35
Y = 17509768
16 feet Y = 5299776
49 meter
Z = -7843985
79 Z = -2406999
28
XDOT = -17762
164725 XDOT = -5429
385510
YDOT = -3048
478818 feet/sec YDOT = -989
835118 meter/sec
ZDOT = 17746
550627 ZDOT = 5382
811048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13522574
48 X = -4121680
70
Y = 15492549
81 feet Y = 4722129
18 meter
Z = -7907891
04 Z = -2410325
19
XDOT = -15989
596607 XDOT = -4873
629046
YDOT = -4965
189846 feet/sec YDOT = -1513
389865 meter/sec
ZDOT = 17641
956948 ZDOT = 5377
268478
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
57926733
00020000 00000-0 20000-3 0 9023
2 36394 51
6457 140
1027 0011455 325
3463 34
6953 15
75971444 997
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10045
57926733 = yrday
fracday
Element set: 902
Inclination: 51
6457 deg
RA of node: 140
1027 deg
Eccentricity:
0011455
Arg of perigee: 325
3463 deg
Mean anomaly: 34
6953 deg
Mean motion: 15
75971444 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 99
Checksum: 297
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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