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
085/01:11:25
158 0
0 0
0 0
0
013/18:43:11
211 0
0 0
0 185
7
000/00:00:00
000 0
0 0
0 180
9
085/01:39:16
793 0
6 1
5 1
5
013/19:11:02
846 -1
1 -0
0 186
4
000/00:00:05
691 -0
8 -0
0 181
0
085/17:53:21
674 -2
5 4
0 4
0
014/11:25:07
727 -0
7 0
0 188
3
000/00:00:15
453 3
1 -0
0 181
7
Coasting Arc #1 (Orbit 209)
---------------------------------------
Vector Time (GMT): 2008/084/10:19:06
000
Vector Time (MET): 013/03:50:52
052
Weight (LBS) : 218128
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3932041
77 A = 6713991
19 meter
Y = -1833403
19 meter E =
0004476
Z = 5122473
51 I = 51
94568
XDOT = 1502
185733 Wp = 37
03691
YDOT = -7409
364034 meter/sec RA = 92
55774 deg
ZDOT = -1494
657509 TA = 67
24585
MA = 67
19855
Ha = 186
163 n
mi
Hp = 180
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12900399
51 X = -3936178
94
Y = -6015102
32 feet Y = -1877298
17 meter
Z = 16806015
45 Z = 5103361
79
XDOT = 4928
430883 XDOT = 1592
003979
YDOT = -24308
937118 feet/sec YDOT = -7392
102186 meter/sec
ZDOT = -4903
731985 ZDOT = -1487
140554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9480059
45 X = -2889522
12
Y = -10732910
99 feet Y = -3271391
27 meter
Z = 16732513
65 Z = 5100070
16
XDOT = 13529
713779 XDOT = 4123
856760
YDOT = -19573
046834 feet/sec YDOT = -5965
864675 meter/sec
ZDOT = -4875
744247 ZDOT = -1486
126846
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 08084
47498794
00020000 00000-0 70000-3 0 9002
2 32699 51
6387 93
0951 0001388 308
1540 51
9499 15
76409581 2105
Satellite: SHUTTLE
Catalog Number: 32699
Epoch time: 08084
47498794 = yrday
fracday
Element set: 900
Inclination: 51
6387 deg
RA of node: 93
0951 deg
Eccentricity:
0001388
Arg of perigee: 308
1540 deg
Mean anomaly: 51
9499 deg
Mean motion: 15
76409581 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 210
Checksum: 327
Coasting Arc #2 (Orbit 219)
---------------------------------------
Vector Time (GMT): 2008/085/01:11:25
158
Vector Time (MET): 013/18:43:11
211
Weight (LBS) : 218054
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1561738
46 A = 6723443
15 meter
Y = 6192923
57 meter E =
0012545
Z = 2079335
66 I = 51
97561
XDOT = -4395
567685 Wp = 60
86418
YDOT = -2988
810062 meter/sec RA = 89
40485 deg
ZDOT = 5581
132348 TA = 322
27622
MA = 322
36412
Ha = 185
675 n
mi
Hp = 180
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5123813
86 X = -1640820
37
Y = 20317990
70 feet Y = 6175057
20 meter
Z = 6821967
40 Z = 2071555
74
XDOT = -14421
153823 XDOT = -4389
007403
YDOT = -9805
807291 feet/sec YDOT = -3037
817265 meter/sec
ZDOT = 18310
801666 ZDOT = 5559
794909
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2091253
73 X = -637414
14
Y = -20858993
83 feet Y = -6357821
32 meter
Z = 6792826
21 Z = 2070453
43
XDOT = 15480
244257 XDOT = 4718
378450
YDOT = 4404
725064 feet/sec YDOT = 1342
560199 meter/sec
ZDOT = 18228
635053 ZDOT = 5556
087964
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 08085
10891649
00020000 00000-0 70000-3 0 9010
2 32699 51
6363 89
8233 0002524 297
2780 62
8128 15
76428146 2201
Satellite: SHUTTLE
Catalog Number: 32699
Epoch time: 08085
10891649 = yrday
fracday
Element set: 901
Inclination: 51
6363 deg
RA of node: 89
8233 deg
Eccentricity:
0002524
Arg of perigee: 297
2780 deg
Mean anomaly: 62
8128 deg
Mean motion: 15
76428146 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 220
Checksum: 311
Coasting Arc #3 (Orbit 219)
---------------------------------------
Vector Time (GMT): 2008/085/01:39:19
639
Vector Time (MET): 013/19:11:05
691
Weight (LBS) : 218010
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3068819
44 A = 6719773
11 meter
Y = -4570377
00 meter E =
0010131
Z = 3846583
48 I = 51
96022
XDOT = 3183
911810 Wp = 78
82090
YDOT = -5650
293774 meter/sec RA = 89
26058 deg
ZDOT = -4162
251559 TA = 54
52329
MA = 54
42879
Ha = 186
434 n
mi
Hp = 181
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10068305
24 X = -3036285
16
Y = -14994675
20 feet Y = -4604436
04 meter
Z = 12620024
54 Z = 3831754
73
XDOT = 10445
904890 XDOT = 3266
937799
YDOT = -18537
709232 feet/sec YDOT = -5614
305917 meter/sec
ZDOT = -13655
680968 ZDOT = -4146
581565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15838607
80 X = 4827607
66
Y = 8763253
17 feet Y = 2671039
57 meter
Z = 12562641
88 Z = 3829093
24
XDOT = -329
697119 XDOT = -100
491682
YDOT = 20139
292741 feet/sec YDOT = 6138
456427 meter/sec
ZDOT = -13596
219496 ZDOT = -4144
127702
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 08085
10892610
00020000 00000-0 70000-3 0 9020
2 32699 51
6362 89
8231 0001367 281
9591 78
1420 15
76120703 2205
Satellite: SHUTTLE
Catalog Number: 32699
Epoch time: 08085
10892610 = yrday
fracday
Element set: 902
Inclination: 51
6362 deg
RA of node: 89
8231 deg
Eccentricity:
0001367
Arg of perigee: 281
9591 deg
Mean anomaly: 78
1420 deg
Mean motion: 15
76120703 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 220
Checksum: 285
Coasting Arc #4 (Orbit 230)
---------------------------------------
Vector Time (GMT): 2008/085/17:53:29
401
Vector Time (MET): 014/11:25:15
453
Weight (LBS) : 217909
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -545956
19 A = 6727512
73 meter
Y = 6567419
91 meter E =
0015923
Z = 1306763
11 I = 51
98203
XDOT = -4725
911643 Wp = 45
90889
YDOT = -1570
045017 meter/sec RA = 85
83398 deg
ZDOT = 5883
114661 TA = 328
38476
MA = 328
48032
Ha = 188
329 n
mi
Hp = 181
742
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1791194
86 X = -625538
65
Y = 21546653
26 feet Y = 6560884
46 meter
Z = 4287280
54 Z = 1303916
70
XDOT = -15504
959458 XDOT = -4736
623512
YDOT = -5151
066329 feet/sec YDOT = -1622
834511 meter/sec
ZDOT = 19301
557287 ZDOT = 5860
130219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21579578
96 X = 6577455
67
Y = 1369547
59 feet Y = 417438
11 meter
Z = 4277093
79 Z = 1303658
19
XDOT = -4727
251599 XDOT = -1440
866287
YDOT = 14143
832569 feet/sec YDOT = 4311
040167 meter/sec
ZDOT = 19213
233528 ZDOT = 5856
193579
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 08085
80639326
00020000 00000-0 70000-3 0 9031
2 32699 51
6398 86
2351 0003997 351
7916 8
3181 15
75393679 2310
Satellite: SHUTTLE
Catalog Number: 32699
Epoch time: 08085
80639326 = yrday
fracday
Element set: 903
Inclination: 51
6398 deg
RA of node: 86
2351 deg
Eccentricity:
0003997
Arg of perigee: 351
7916 deg
Mean anomaly: 8
3181 deg
Mean motion: 15
75393679 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 231
Checksum: 331
Coasting Arc #5 (Orbit 245)
---------------------------------------
Vector Time (GMT): 2008/086/17:53:47
215
Vector Time (MET): 015/11:25:33
268
Weight (LBS) : 217909
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4211243
02 A = 6717603
00 meter
Y = 1720105
35 meter E =
0011835
Z = -4952868
55 I = 51
94635
XDOT = -492
741869 Wp = 87
30250
YDOT = 7372
776113 meter/sec RA = 80
67990 deg
ZDOT = 2146
485843 TA = 203
41869
MA = 203
47264
Ha = 188
367 n
mi
Hp = 181
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13816414
12 X = 4215799
71
Y = 5643390
25 feet Y = 1767118
18 meter
Z = -16249568
74 Z = -4932399
34
XDOT = -1616
607183 XDOT = -585
393122
YDOT = 24188
898007 feet/sec YDOT = 7366
761570 meter/sec
ZDOT = 7042
276389 ZDOT = 2143
866249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5094275
07 X = 1552735
04
Y = -14118810
84 feet Y = -4303413
55 meter
Z = -16170874
40 Z = -4928882
52
XDOT = 23205
648637 XDOT = 7073
081705
YDOT = 336
280877 feet/sec YDOT = 102
498411 meter/sec
ZDOT = 7033
036422 ZDOT = 2143
669502
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
75788819
00020000 00000-0 70000-3 0 9049
2 32699 51
6407 81
3385 0003995 354
8430 5
2692 15
75411235 2465
Satellite: SHUTTLE
Catalog Number: 32699
Epoch time: 08086
75788819 = yrday
fracday
Element set: 904
Inclination: 51
6407 deg
RA of node: 81
3385 deg
Eccentricity:
0003995
Arg of perigee: 354
8430 deg
Mean anomaly: 5
2692 deg
Mean motion: 15
75411235 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 246
Checksum: 324
Coasting Arc #6 (Orbit 261)
---------------------------------------
Vector Time (GMT): 2008/087/17:59:00
228
Vector Time (MET): 016/11:30:46
281
Weight (LBS) : 217909
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1772820
76 A = 6721637
46 meter
Y = -5220168
16 meter E =
0008328
Z = -3855209
55 I = 51
95501
XDOT = 4544
274141 Wp = 46
21558
YDOT = 4612
801459 meter/sec RA = 75
58050 deg
ZDOT = -4156
208914 TA = 180
47743
MA = 180
47823
Ha = 188
341 n
mi
Hp = 181
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5816341
07 X = 1849660
57
Y = -17126535
96 feet Y = -5199959
18 meter
Z = -12648325
29 Z = -3846410
02
XDOT = 14909
035897 XDOT = 4512
661339
YDOT = 15133
863053 feet/sec YDOT = 4663
328514 meter/sec
ZDOT = -13635
856017 ZDOT = -4134
209975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17538713
18 X = -5345799
78
Y = -4514422
68 feet Y = -1375996
03 meter
Z = -12615138
45 Z = -3845094
20
XDOT = 13571
437601 XDOT = 4136
574181
YDOT = -14857
754575 feet/sec YDOT = -4528
643595 meter/sec
ZDOT = -13550
980712 ZDOT = -4130
338921
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
77280240
00020000 00000-0 70000-3 0 9058
2 32699 51
6414 76
1155 0004023 357
9222 2
1925 15
75449088 2626
Satellite: SHUTTLE
Catalog Number: 32699
Epoch time: 08087
77280240 = yrday
fracday
Element set: 905
Inclination: 51
6414 deg
RA of node: 76
1155 deg
Eccentricity:
0004023
Arg of perigee: 357
9222 deg
Mean anomaly: 2
1925 deg
Mean motion: 15
75449088 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 262
Checksum: 294
Coasting Arc #7 (Orbit 277)
---------------------------------------
Vector Time (GMT): 2008/088/17:59:18
908
Vector Time (MET): 017/11:31:04
961
Weight (LBS) : 217909
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4134222
34 A = 6723762
31 meter
Y = -4258416
65 meter E =
0013568
Z = 3151796
27 I = 51
95340
XDOT = 2048
435464 Wp = 77
05289
YDOT = -5607
493730 meter/sec RA = 70
40427 deg
ZDOT = -4868
977894 TA = 66
39444
MA = 66
25203
Ha = 188
465 n
mi
Hp = 181
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13563721
59 X = -4101714
57
Y = -13971183
23 feet Y = -4304363
58 meter
Z = 10340538
94 Z = 3131791
54
XDOT = 6720
588793 XDOT = 2134
501040
YDOT = -18397
289141 feet/sec YDOT = -5584
158105 meter/sec
ZDOT = -15974
336921 ZDOT = -4858
817045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12574705
27 X = -3832770
17
Y = 14920980
04 feet Y = 4547914
72 meter
Z = 10263351
88 Z = 3128269
65
XDOT = -17886
230718 XDOT = -5451
723123
YDOT = -4065
768200 feet/sec YDOT = -1239
246147 meter/sec
ZDOT = -15935
961883 ZDOT = -4857
281182
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
78769785
00020000 00000-0 70000-3 0 9067
2 32699 51
6411 70
8923 0004015 3
3834 356
7357 15
75467742 2780
Satellite: SHUTTLE
Catalog Number: 32699
Epoch time: 08088
78769785 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 70
8923 deg
Eccentricity:
0004015
Arg of perigee: 3
3834 deg
Mean anomaly: 356
7357 deg
Mean motion: 15
75467742 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 278
Checksum: 337
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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