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
259 11
3 -0
1 17
6
010/21:03:13
304 6
7 -0
0 193
9
000/00:00:12
608 11
7 -17
6 181
7
Coasting Arc #1 (Orbit 150)
---------------------------------------
Vector Time (GMT): 2010/144/05:06:55
000
Vector Time (MET): 009/10:46:46
045
Weight (LBS) : 221081
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3739169
20 A = 6722925
08 meter
Y = -3210263
48 meter E =
0016348
Z = -4586272
80 I = 51
59510
XDOT = 6357
177738 Wp = 26
96158
YDOT = -3142
358338 meter/sec RA = 353
10948 deg
ZDOT = -2973
239778 TA = 213
42123
MA = 213
52452
Ha = 192
297 n
mi
Hp = 183
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12267615
50 X = -3680713
90
Y = -10532360
49 feet Y = -3251749
89 meter
Z = -15046826
78 Z = -4604296
24
XDOT = 20856
882344 XDOT = 6406
287369
YDOT = -10309
574601 feet/sec YDOT = -3070
993772 meter/sec
ZDOT = -9754
723682 ZDOT = -2942
237058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1905214
81 X = -580709
47
Y = -15988436
72 feet Y = -4873275
51 meter
Z = -15118599
51 Z = -4608149
13
XDOT = 21235
882470 XDOT = 6472
696977
YDOT = 6608
172546 feet/sec YDOT = 2014
170992 meter/sec
ZDOT = -9631
239121 ZDOT = -2935
601684
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 10144
23415742
00020000 00000-0 20000-3 0 9001
2 36572 51
6454 353
4871 0011187 347
7804 12
3086 15
74016213 1519
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10144
23415742 = yrday
fracday
Element set: 900
Inclination: 51
6454 deg
RA of node: 353
4871 deg
Eccentricity:
0011187
Arg of perigee: 347
7804 deg
Mean anomaly: 12
3086 deg
Mean motion: 15
74016213 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 151
Checksum: 261
Coasting Arc #2 (Orbit 166)
---------------------------------------
Vector Time (GMT): 2010/145/05:07:29
776
Vector Time (MET): 010/10:47:20
821
Weight (LBS) : 221081
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5479639
18 A = 6729692
90 meter
Y = 3100864
13 meter E =
0013693
Z = 2378578
25 I = 51
58816
XDOT = -4295
064985 Wp = 58
17708
YDOT = -3441
964680 meter/sec RA = 347
92575 deg
ZDOT = -5377
869431 TA = 95
01376
MA = 94
85743
Ha = 192
466 n
mi
Hp = 182
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17977818
82 X = -5525461
26
Y = 10173438
73 feet Y = 3039331
09 meter
Z = 7803734
40 Z = 2351846
67
XDOT = -14091
420555 XDOT = -4230
131886
YDOT = -11292
535040 feet/sec YDOT = -3489
631043 meter/sec
ZDOT = -17643
928578 ZDOT = -5398
577879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20261101
26 X = -6175583
66
Y = -4223629
88 feet Y = -1287362
39 meter
Z = 7697260
71 Z = 2346125
06
XDOT = -3387
760093 XDOT = -1032
589276
YDOT = -16233
772562 feet/sec YDOT = -4948
053877 meter/sec
ZDOT = -17726
388959 ZDOT = -5403
003355
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
24997835
00020000 00000-0 20000-3 0 9012
2 36572 51
6456 348
2709 0011274 351
5455 8
5517 15
74033977 1674
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10145
24997835 = yrday
fracday
Element set: 901
Inclination: 51
6456 deg
RA of node: 348
2709 deg
Eccentricity:
0011274
Arg of perigee: 351
5455 deg
Mean anomaly: 8
5517 deg
Mean motion: 15
74033977 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 167
Checksum: 307
Coasting Arc #3 (Orbit 173)
---------------------------------------
Vector Time (GMT): 2010/145/15:23:28
563
Vector Time (MET): 010/21:03:19
608
Weight (LBS) : 220697
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4262066
21 A = 6723050
91 meter
Y = 2599573
09 meter E =
0013333
Z = 4493725
11 I = 51
55255
XDOT = -5764
116617 Wp = 12
07650
YDOT = 4036
590451 meter/sec RA = 345
76578 deg
ZDOT = 3142
990439 TA = 46
59888
MA = 46
48795
Ha = 193
910 n
mi
Hp = 181
696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13983156
86 X = 4210850
42
Y = 8528783
10 feet Y = 2646947
18 meter
Z = 14743192
62 Z = 4514306
52
XDOT = -18911
143757 XDOT = -5824
094464
YDOT = 13243
406991 feet/sec YDOT = 3971
796955 meter/sec
ZDOT = 10311
648421 ZDOT = 3114
842590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2365866
47 X = 721116
10
Y = -16132209
43 feet Y = -4917097
43 meter
Z = 14825148
91 Z = 4518705
39
XDOT = 18469
695762 XDOT = 5629
563268
YDOT = 12048
387081 feet/sec YDOT = 3672
348382 meter/sec
ZDOT = 10199
529579 ZDOT = 3108
816616
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
69440136
00020000 00000-0 20000-3 0 9029
2 36572 51
6443 345
9838 0017293 342
9630 17
0950 15
74078594 1741
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10145
69440136 = yrday
fracday
Element set: 902
Inclination: 51
6443 deg
RA of node: 345
9838 deg
Eccentricity:
0017293
Arg of perigee: 342
9630 deg
Mean anomaly: 17
0950 deg
Mean motion: 15
74078594 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 174
Checksum: 301
Coasting Arc #4 (Orbit 188)
---------------------------------------
Vector Time (GMT): 2010/146/15:24:03
568
Vector Time (MET): 011/21:03:54
613
Weight (LBS) : 220697
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4880170
62 A = 6729240
37 meter
Y = -3856550
09 meter E =
0020258
Z = -2536322
42 I = 51
54501
XDOT = 4897
378121 Wp = 359
98214
YDOT = 2729
737006 meter/sec RA = 340
57710 deg
ZDOT = 5292
364101 TA = 331
19102
MA = 331
30274
Ha = 194
240 n
mi
Hp = 181
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16011058
48 X = 4935253
77
Y = -12652723
41 feet Y = -3801668
78 meter
Z = -8321267
79 Z = -2512480
85
XDOT = 16067
513521 XDOT = 4840
779906
YDOT = 8955
830072 feet/sec YDOT = 2784
185215 meter/sec
ZDOT = 17363
399282 ZDOT = 5316
018901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18145749
25 X = -5530824
37
Y = -9420654
50 feet Y = -2871415
49 meter
Z = -8226296
47 Z = -2507375
17
XDOT = 896
621390 XDOT = 273
290200
YDOT = -16913
682960 feet/sec YDOT = -5155
290566 meter/sec
ZDOT = 17457
592792 ZDOT = 5321
074283
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
64670948
00020000 00000-0 20000-3 0 9032
2 36572 51
6453 341
0938 0017293 347
0084 13
0632 15
74068320 1894
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10146
64670948 = yrday
fracday
Element set: 903
Inclination: 51
6453 deg
RA of node: 341
0938 deg
Eccentricity:
0017293
Arg of perigee: 347
0084 deg
Mean anomaly: 13
0632 deg
Mean motion: 15
74068320 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 189
Checksum: 287
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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