Date:
June 13th 2008
SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2008/152/21:02:11 970 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 69 ET - UTC (sec) : 65 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
164/20:20:25
149 -3
8 7
0 7
0
011/23:18:13
179 2
3 -0
0 190
0
000/00:00:26
358 5
4 -0
1 181
9
Coasting Arc #1 (Orbit 174)
---------------------------------------
Vector Time (GMT): 2008/163/20:48:17
000
Vector Time (MET): 010/23:46:05
030
Weight (LBS) : 212520
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3247726
12 A = 6723020
94 meter
Y = -5451285
02 meter E =
0000838
Z = -2219731
83 I = 51
87739
XDOT = 5311
221373 Wp = 207
48560
YDOT = -925
280781 meter/sec RA = 43
28159 deg
ZDOT = -5498
511580 TA = 357
33181
MA = 357
33226
Ha = 185
657 n
mi
Hp = 181
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10655269
42 X = -3175744
51
Y = -17884793
37 feet Y = -5487200
21 meter
Z = -7282584
74 Z = -2235335
18
XDOT = 17425
266971 XDOT = 5347
884150
YDOT = -3035
698102 feet/sec YDOT = -865
681995 meter/sec
ZDOT = -18039
736156 ZDOT = -5472
620615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18458433
81 X = 5626130
62
Y = 9581319
24 feet Y = 2920386
11 meter
Z = -7343104
51 Z = -2238178
25
XDOT = -12581
688773 XDOT = -3834
898738
YDOT = 10489
140891 feet/sec YDOT = 3197
090144 meter/sec
ZDOT = -17940
135263 ZDOT = -5468
153228
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 32960U 08027A 08163
89414986
00020000 00000-0 70000-3 0 9008
2 32960 51
6407 43
6821 0005786 309
1769 50
8881 15
76457321 1754
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08163
89414986 = yrday
fracday
Element set: 900
Inclination: 51
6407 deg
RA of node: 43
6821 deg
Eccentricity:
0005786
Arg of perigee: 309
1769 deg
Mean anomaly: 50
8881 deg
Mean motion: 15
76457321 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 175
Checksum: 312
Coasting Arc #2 (Orbit 190)
---------------------------------------
Vector Time (GMT): 2008/164/20:20:38
328
Vector Time (MET): 011/23:18:26
358
Weight (LBS) : 212347
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4444866
13 A = 6728086
35 meter
Y = 4850339
12 meter E =
0018865
Z = 1348812
10 I = 51
86056
XDOT = -4398
594292 Wp = 29
29114
YDOT = 2395
417465 meter/sec RA = 38
23376 deg
ZDOT = 5863
059187 TA = 345
50367
MA = 345
55771
Ha = 189
975 n
mi
Hp = 181
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14582894
12 X = 4383746
18
Y = 15913186
09 feet Y = 4899702
24 meter
Z = 4425236
56 Z = 1370257
62
XDOT = -14431
083634 XDOT = -4453
535210
YDOT = 7858
981186 feet/sec YDOT = 2345
921894 meter/sec
ZDOT = 19235
758489 ZDOT = 5841
557516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20051196
94 X = -6111604
83
Y = -7943469
88 feet Y = -2421169
62 meter
Z = 4508192
40 Z = 1374097
04
XDOT = 9059
406442 XDOT = 2761
307083
YDOT = -11964
921306 feet/sec YDOT = -3646
908014 meter/sec
ZDOT = 19153
174941 ZDOT = 5837
887722
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 32960U 08027A 08164
90845115
00020000 00000-0 70000-3 0 9014
2 32960 51
6411 38
4543 0009863 343
4741 16
6100 15
75163482 1916
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08164
90845115 = yrday
fracday
Element set: 901
Inclination: 51
6411 deg
RA of node: 38
4543 deg
Eccentricity:
0009863
Arg of perigee: 343
4741 deg
Mean anomaly: 16
6100 deg
Mean motion: 15
75163482 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 191
Checksum: 270
Coasting Arc #3 (Orbit 205)
---------------------------------------
Vector Time (GMT): 2008/165/20:25:56
676
Vector Time (MET): 012/23:23:44
706
Weight (LBS) : 212347
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5357964
87 A = 6721807
41 meter
Y = -310120
14 meter E =
0008611
Z = -4045597
98 I = 51
81576
XDOT = 3268
929198 Wp = 31
29569
YDOT = 5783
010130 meter/sec RA = 33
04671 deg
ZDOT = 3896
934605 TA = 278
72595
MA = 278
82348
Ha = 190
171 n
mi
Hp = 181
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17578624
92 X = 5380687
45
Y = -1017454
53 feet Y = -250076
65 meter
Z = -13272959
26 Z = -4019513
58
XDOT = 10724
833328 XDOT = 3185
088920
YDOT = 18973
130348 feet/sec YDOT = 5819
095808 meter/sec
ZDOT = 12785
218521 ZDOT = 3912
612444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15069310
99 X = -4593125
99
Y = 9252791
79 feet Y = 2820250
94 meter
Z = -13172563
37 Z = -4014997
31
XDOT = -17689
115801 XDOT = -5391
642496
YDOT = -10572
127841 feet/sec YDOT = -3222
384566 meter/sec
ZDOT = 12846
037956 ZDOT = 3915
472369
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 32960U 08027A 08165
86009121
00020000 00000-0 70000-3 0 9020
2 32960 51
6413 33
5599 0009903 346
3586 13
7309 15
75176088 2061
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08165
86009121 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 33
5599 deg
Eccentricity:
0009903
Arg of perigee: 346
3586 deg
Mean anomaly: 13
7309 deg
Mean motion: 15
75176088 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 206
Checksum: 291
Coasting Arc #4 (Orbit 221)
---------------------------------------
Vector Time (GMT): 2008/166/20:26:17
081
Vector Time (MET): 013/23:24:05
111
Weight (LBS) : 212347
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2733962
69 A = 6722490
01 meter
Y = -4836376
19 meter E =
0012174
Z = -3798213
68 I = 51
79308
XDOT = 6433
299456 Wp = 20
76843
YDOT = -330
212460 meter/sec RA = 27
96460 deg
ZDOT = -4203
177421 TA = 205
14083
MA = 205
20015
Ha = 190
191 n
mi
Hp = 181
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8969693
86 X = -2661227
14
Y = -15867375
95 feet Y = -4866541
59 meter
Z = -12461330
96 Z = -3811319
56
XDOT = 21106
625511 XDOT = 6456
932298
YDOT = -1083
374211 feet/sec YDOT = -258
138768 meter/sec
ZDOT = -13789
952169 ZDOT = -4171
866760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15529145
32 X = 4733283
49
Y = 9476555
95 feet Y = 2888454
25 meter
Z = -12512167
27 Z = -3813708
58
XDOT = -17248
923585 XDOT = -5257
471909
YDOT = 10187
062166 feet/sec YDOT = 3105
016548 meter/sec
ZDOT = -13669
436093 ZDOT = -4166
444121
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 32960U 08027A 08166
87516288
00020000 00000-0 70000-3 0 9030
2 32960 51
6412 28
3382 0009880 350
3749 9
7224 15
75188539 2225
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08166
87516288 = yrday
fracday
Element set: 903
Inclination: 51
6412 deg
RA of node: 28
3382 deg
Eccentricity:
0009880
Arg of perigee: 350
3749 deg
Mean anomaly: 9
7224 deg
Mean motion: 15
75188539 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 222
Checksum: 305
Coasting Arc #5 (Orbit 237)
---------------------------------------
Vector Time (GMT): 2008/167/20:26:35
255
Vector Time (MET): 014/23:24:23
285
Weight (LBS) : 212347
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5870220
16 A = 6724188
08 meter
Y = 323269
01 meter E =
0015169
Z = 3263619
92 I = 51
77209
XDOT = -2945
789739 Wp = 51
54639
YDOT = -5295
080598 meter/sec RA = 22
77810 deg
ZDOT = -4749
991563 TA = 90
29458
MA = 90
12076
Ha = 190
370 n
mi
Hp = 181
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19259252
50 X = -5889252
95
Y = 1060593
86 feet Y = 257517
81 meter
Z = 10707414
44 Z = 3235055
93
XDOT = -9664
664497 XDOT = -2863
285547
YDOT = -17372
311672 feet/sec YDOT = -5327
559903 meter/sec
ZDOT = -15583
961822 ZDOT = -4764
102952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16129939
71 X = 4916405
63
Y = -10686958
19 feet Y = -3257384
86 meter
Z = 10597469
48 Z = 3230108
70
XDOT = 16268
095281 XDOT = 4958
515442
YDOT = 8966
764961 feet/sec YDOT = 2733
069960 meter/sec
ZDOT = -15638
699901 ZDOT = -4766
675730
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 32960U 08027A 08167
89021959
00020000 00000-0 70000-3 0 9040
2 32960 51
6410 23
1164 0009997 354
9540 5
1521 15
75220745 2385
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08167
89021959 = yrday
fracday
Element set: 904
Inclination: 51
6410 deg
RA of node: 23
1164 deg
Eccentricity:
0009997
Arg of perigee: 354
9540 deg
Mean anomaly: 5
1521 deg
Mean motion: 15
75220745 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 238
Checksum: 285
Coasting Arc #6 (Orbit 253)
---------------------------------------
Vector Time (GMT): 2008/168/20:26:53
229
Vector Time (MET): 015/23:24:41
259
Weight (LBS) : 212347
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2365918
72 A = 6719898
79 meter
Y = 4437085
19 meter E =
0010317
Z = 4447407
22 I = 51
73096
XDOT = -6976
209567 Wp = 49
93108
YDOT = 465
154643 meter/sec RA = 17
68842 deg
ZDOT = 3248
698222 TA = 7
61622
MA = 7
60056
Ha = 190
337 n
mi
Hp = 180
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7762200
54 X = 2294521
84
Y = 14557366
11 feet Y = 4463142
14 meter
Z = 14591231
02 Z = 4458728
42
XDOT = -22887
826662 XDOT = -6996
674216
YDOT = 1526
097911 feet/sec YDOT = 387
027587 meter/sec
ZDOT = 10658
458735 ZDOT = 3214
757916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14145519
86 X = -4311554
45
Y = -8413626
99 feet Y = -2564473
51 meter
Z = 14635157
56 Z = 4460796
02
XDOT = 18168
366630 XDOT = 5537
718149
YDOT = -12242
135824 feet/sec YDOT = -3731
402999 meter/sec
ZDOT = 10527
821460 ZDOT = 3208
879981
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 32960U 08027A 08168
90525880
00020000 00000-0 70000-3 0 9056
2 32960 51
6410 17
8937 0010016 357
9271 2
1850 15
75271002 2543
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08168
90525880 = yrday
fracday
Element set: 905
Inclination: 51
6410 deg
RA of node: 17
8937 deg
Eccentricity:
0010016
Arg of perigee: 357
9271 deg
Mean anomaly: 2
1850 deg
Mean motion: 15
75271002 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 254
Checksum: 269
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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