SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2008/071/06:28:13 948 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 10 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : -0 34056
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 237)
---------------------------------------
Vector Time (GMT): 2008/086/04:57:03
000
Vector Time (MET): 014/22:28:49
052
Weight (LBS) : 216838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4131625
39 A = 6717727
61 meter
Y = -1793341
51 meter E =
0008794
Z = 4982135
10 I = 51
94788
XDOT = 750
009619 Wp = 33
99758
YDOT = -7394
260879 meter/sec RA = 83
44198 deg
ZDOT = -2030
777975 TA = 75
60694
MA = 75
50935
Ha = 188
665 n
mi
Hp = 181
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13555201
42 X = -4135513
05
Y = -5883666
36 feet Y = -1839462
20 meter
Z = 16345587
61 Z = 4962054
31
XDOT = 2460
661481 XDOT = 842
319450
YDOT = -24259
386087 feet/sec YDOT = -7385
377723 meter/sec
ZDOT = -6662
657397 ZDOT = -2026
909322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8692032
66 X = 2649331
55
Y = -12055197
54 feet Y = -3674424
21 meter
Z = 16268375
16 Z = 4958600
75
XDOT = 22268
387606 XDOT = 6787
404542
YDOT = 7044
324701 feet/sec YDOT = 2147
110169 meter/sec
ZDOT = -6648
636005 ZDOT = -2026
504254
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 32699U 08009A 08086
25043436
00020000 00000-0 70000-3 0 9009
2 32699 51
6406 83
9477 0003944 359
5836
5324 15
75318213 2383
Satellite: SHUTTLE
Catalog Number: 32699
Epoch time: 08086
25043436 = yrday
fracday
Element set: 900
Inclination: 51
6406 deg
RA of node: 83
9477 deg
Eccentricity:
0003944
Arg of perigee: 359
5836 deg
Mean anomaly:
5324 deg
Mean motion: 15
75318213 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 238
Checksum: 302
Coasting Arc #2 (Orbit 253)
---------------------------------------
Vector Time (GMT): 2008/087/04:57:03
316
Vector Time (MET): 015/22:28:49
369
Weight (LBS) : 216807
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -437212
15 A = 6726328
60 meter
Y = 6337601
30 meter E =
0015969
Z = 2183259
51 I = 51
97277
XDOT = -4878
028364 Wp = 57
83663
YDOT = -2248
342674 meter/sec RA = 78
35518 deg
ZDOT = 5528
810279 TA = 326
53203
MA = 326
63284
Ha = 188
641 n
mi
Hp = 181
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1434423
07 X = -518496
37
Y = 20792655
18 feet Y = 6332269
75 meter
Z = 7162924
89 Z = 2180937
44
XDOT = -16004
030066 XDOT = -4879
439784
YDOT = -7376
452341 feet/sec YDOT = -2302
777744 meter/sec
ZDOT = 18139
141334 ZDOT = 5505
109504
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20082705
11 X = -6121208
52
Y = -5585219
66 feet Y = -1702374
95 meter
Z = 7154708
14 Z = 2180755
04
XDOT = 10028
287777 XDOT = 3056
622114
YDOT = -12851
211406 feet/sec YDOT = -3917
049237 meter/sec
ZDOT = 18047
994680 ZDOT = 5501
028778
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 32699U 08009A 08087
26542157
00020000 00000-0 70000-3 0 9016
2 32699 51
6409 78
7253 0003906 3
7211 356
3981 15
75340724 2544
Satellite: SHUTTLE
Catalog Number: 32699
Epoch time: 08087
26542157 = yrday
fracday
Element set: 901
Inclination: 51
6409 deg
RA of node: 78
7253 deg
Eccentricity:
0003906
Arg of perigee: 3
7211 deg
Mean anomaly: 356
3981 deg
Mean motion: 15
75340724 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 254
Checksum: 300
Coasting Arc #3 (Orbit 268)
---------------------------------------
Vector Time (GMT): 2008/088/05:01:55
267
Vector Time (MET): 016/22:33:41
319
Weight (LBS) : 216807
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4084741
46 A = 6723045
24 meter
Y = 4029263
69 meter E =
0006528
Z = -3505431
57 I = 51
95474
XDOT = -1931
211425 Wp = 57
15076
YDOT = 5905
323323 meter/sec RA = 73
17029 deg
ZDOT = 4546
949780 TA = 261
39534
MA = 261
46931
Ha = 188
678 n
mi
Hp = 181
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13401382
75 X = 4056512
01
Y = 13219369
05 feet Y = 4074682
35 meter
Z = -11500759
73 Z = -3485656
78
XDOT = -6335
995488 XDOT = -2019
044340
YDOT = 19374
420350 feet/sec YDOT = 5883
285777 meter/sec
ZDOT = 14917
814240 ZDOT = 4537
354057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15217690
57 X = -4638352
09
Y = 11158827
43 feet Y = 3401210
60 meter
Z = -11424478
82 Z = -3482181
15
XDOT = -17271
964276 XDOT = -5264
494711
YDOT = -8350
704905 feet/sec YDOT = -2545
294855 meter/sec
ZDOT = 14881
643240 ZDOT = 4535
924859
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 32699U 08009A 08088
21695509
00020000 00000-0 70000-3 0 9023
2 32699 51
6409 73
8301 0003935 5
6079 354
5128 15
75353823 2692
Satellite: SHUTTLE
Catalog Number: 32699
Epoch time: 08088
21695509 = yrday
fracday
Element set: 902
Inclination: 51
6409 deg
RA of node: 73
8301 deg
Eccentricity:
0003935
Arg of perigee: 5
6079 deg
Mean anomaly: 354
5128 deg
Mean motion: 15
75353823 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 269
Checksum: 315
Coasting Arc #4 (Orbit 284)
---------------------------------------
Vector Time (GMT): 2008/089/05:06:55
361
Vector Time (MET): 017/22:38:41
413
Weight (LBS) : 216807
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2974002
72 A = 6717177
34 meter
Y = -3261906
53 meter E =
0015457
Z = -5076726
47 I = 51
92490
XDOT = 4005
568696 Wp = 63
32656
YDOT = 6336
426780 meter/sec RA = 68
06827 deg
ZDOT = -1722
008191 TA = 190
13469
MA = 190
16589
Ha = 188
671 n
mi
Hp = 181
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9757226
78 X = 3034838
46
Y = -10701793
08 feet Y = -3228384
44 meter
Z = -16655926
75 Z = -5062130
73
XDOT = 13141
629581 XDOT = 3942
939751
YDOT = 20788
801773 feet/sec YDOT = 6380
770309 meter/sec
ZDOT = -5649
633174 ZDOT = -1702
701829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9413807
60 X = 2869328
56
Y = 11088842
43 feet Y = 3379879
17 meter
Z = -16600287
50 Z = -5059767
63
XDOT = -21437
887887 XDOT = -6534
268228
YDOT = 9840
109673 feet/sec YDOT = 2999
265428 meter/sec
ZDOT = -5574
903907 ZDOT = -1699
230711
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 32699U 08009A 08089
23190472
00020000 00000-0 70000-3 0 9036
2 32699 51
6405 68
6075 0003933 9
2766 350
8470 15
75367301 2852
Satellite: SHUTTLE
Catalog Number: 32699
Epoch time: 08089
23190472 = yrday
fracday
Element set: 903
Inclination: 51
6405 deg
RA of node: 68
6075 deg
Eccentricity:
0003933
Arg of perigee: 9
2766 deg
Mean anomaly: 350
8470 deg
Mean motion: 15
75367301 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 285
Checksum: 308
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 may contain past, current and future orbital data 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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