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
085/17:53:21
646 -2
5 4
0 4
0
014/11:25:07
699 -0
8 0
0 188
3
000/00:00:15
398 3
1 -0
0 181
6
Coasting Arc #1 (Orbit 222)
---------------------------------------
Vector Time (GMT): 2008/085/06:03:30
000
Vector Time (MET): 013/23:35:16
052
Weight (LBS) : 217567
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4137622
60 A = 6713863
56 meter
Y = -461866
87 meter E =
0001722
Z = 5266217
52 I = 51
94512
XDOT = 188
634677 Wp = 43
51438
YDOT = -7685
818235 meter/sec RA = 88
34428 deg
ZDOT = -524
543381 TA = 51
45252
MA = 51
43709
Ha = 186
333 n
mi
Hp = 180
855
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13574877
31 X = -4157745
53
Y = -1515311
26 feet Y = -508144
92 meter
Z = 17277616
54 Z = 5246068
01
XDOT = 618
880173 XDOT = 276
922011
YDOT = -25215
939092 feet/sec YDOT = -7683
221027 meter/sec
ZDOT = -1720
942851 ZDOT = -523
411494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 749410
69 X = 228420
38
Y = -13736008
42 feet Y = -4186735
37 meter
Z = 17200289
30 Z = 5242648
18
XDOT = 24210
043678 XDOT = 7379
221313
YDOT = -835
218467 feet/sec YDOT = -254
574589 meter/sec
ZDOT = -1717
462400 ZDOT = -523
482540
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
29912344
00020000 00000-0 70000-3 0 9005
2 32699 51
6401 88
8465 0001369 278
5609 81
5400 15
76228597 2230
Satellite: SHUTTLE
Catalog Number: 32699
Epoch time: 08085
29912344 = yrday
fracday
Element set: 900
Inclination: 51
6401 deg
RA of node: 88
8465 deg
Eccentricity:
0001369
Arg of perigee: 278
5609 deg
Mean anomaly: 81
5400 deg
Mean motion: 15
76228597 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 223
Checksum: 315
Coasting Arc #2 (Orbit 230)
---------------------------------------
Vector Time (GMT): 2008/085/17:53:29
345
Vector Time (MET): 014/11:25:15
398
Weight (LBS) : 217128
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -555335
94 A = 6727373
10 meter
Y = 6564224
90 meter E =
0015999
Z = 1318291
72 I = 51
98147
XDOT = -4724
521755 Wp = 46
85670
YDOT = -1587
266323 meter/sec RA = 85
83476 deg
ZDOT = 5879
656591 TA = 327
56610
MA = 327
66433
Ha = 188
294 n
mi
Hp = 181
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1821968
32 X = -634938
06
Y = 21536170
93 feet Y = 6557584
68 meter
Z = 4325104
08 Z = 1315399
71
XDOT = -15500
399459 XDOT = -4735
024785
YDOT = -5207
566675 feet/sec YDOT = -1640
039144 meter/sec
ZDOT = 19290
211912 ZDOT = 5856
679410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21569733
92 X = 6574454
90
Y = 1400832
51 feet Y = 426973
75 meter
Z = 4314742
04 Z = 1315133
37
XDOT = -4781
617615 XDOT = -1457
437049
YDOT = 14141
075792 feet/sec YDOT = 4310
199901 meter/sec
ZDOT = 19201
914090 ZDOT = 5852
743415
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
80636811
00020000 00000-0 70000-3 0 9015
2 32699 51
6393 86
2359 0003858 354
6726 5
4396 15
75438215 2312
Satellite: SHUTTLE
Catalog Number: 32699
Epoch time: 08085
80636811 = yrday
fracday
Element set: 901
Inclination: 51
6393 deg
RA of node: 86
2359 deg
Eccentricity:
0003858
Arg of perigee: 354
6726 deg
Mean anomaly: 5
4396 deg
Mean motion: 15
75438215 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 231
Checksum: 317
Coasting Arc #3 (Orbit 245)
---------------------------------------
Vector Time (GMT): 2008/086/17:53:39
984
Vector Time (MET): 015/11:25:26
037
Weight (LBS) : 217128
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4212597
32 A = 6717440
08 meter
Y = 1700194
09 meter E =
0012079
Z = -4958631
26 I = 51
94575
XDOT = -477
906716 Wp = 87
91587
YDOT = 7378
731855 meter/sec RA = 80
68073 deg
ZDOT = 2128
838061 TA = 202
62784
MA = 202
68114
Ha = 188
320 n
mi
Hp = 181
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13820857
35 X = 4217404
06
Y = 5578064
59 feet Y = 1747223
42 meter
Z = -16268475
26 Z = -4938154
86
XDOT = -1567
935421 XDOT = -570
539788
YDOT = 24208
437846 feet/sec YDOT = 7372
882939 meter/sec
ZDOT = 6984
376842 ZDOT = 2126
290581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5036266
62 X = 1535054
06
Y = -14118145
22 feet Y = -4303210
66 meter
Z = -16189755
53 Z = -4934637
48
XDOT = 23222
952379 XDOT = 7078
355885
YDOT = 303
572067 feet/sec YDOT = 92
528766 meter/sec
ZDOT = 6975
414106 ZDOT = 2126
106220
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
75783594
00020000 00000-0 70000-3 0 9022
2 32699 51
6402 81
3391 0003851 357
7095 2
4050 15
75459937 2465
Satellite: SHUTTLE
Catalog Number: 32699
Epoch time: 08086
75783594 = yrday
fracday
Element set: 902
Inclination: 51
6402 deg
RA of node: 81
3391 deg
Eccentricity:
0003851
Arg of perigee: 357
7095 deg
Mean anomaly: 2
4050 deg
Mean motion: 15
75459937 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 246
Checksum: 317
Coasting Arc #4 (Orbit 261)
---------------------------------------
Vector Time (GMT): 2008/087/17:58:51
184
Vector Time (MET): 016/11:30:37
237
Weight (LBS) : 217128
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1764703
45 A = 6721523
42 meter
Y = -5228338
08 meter E =
0008336
Z = -3847663
18 I = 51
95458
XDOT = 4548
510494 Wp = 47
86821
YDOT = 4600
452010 meter/sec RA = 75
58089 deg
ZDOT = -4165
364718 TA = 178
70730
MA = 178
70515
Ha = 188
290 n
mi
Hp = 181
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5789709
47 X = 1841598
35
Y = -17153340
14 feet Y = -5208219
36 meter
Z = -12623566
87 Z = -3838902
95
XDOT = 14922
934692 XDOT = 4517
079642
YDOT = 15093
346489 feet/sec YDOT = 4651
027348 meter/sec
ZDOT = -13665
894745 ZDOT = -4143
344756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17560353
02 X = -5352395
60
Y = -4497195
70 feet Y = -1370745
25 meter
Z = -12590531
65 Z = -3837594
05
XDOT = 13541
837084 XDOT = 4127
551943
YDOT = -14857
852260 feet/sec YDOT = -4528
673369 meter/sec
ZDOT = -13580
940139 ZDOT = -4139
470554
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
77271861
00020000 00000-0 70000-3 0 9035
2 32699 51
6409 76
1158 0003875
7332 359
3837 15
75497882 2626
Satellite: SHUTTLE
Catalog Number: 32699
Epoch time: 08087
77271861 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 76
1158 deg
Eccentricity:
0003875
Arg of perigee:
7332 deg
Mean anomaly: 359
3837 deg
Mean motion: 15
75497882 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 262
Checksum: 331
Coasting Arc #5 (Orbit 277)
---------------------------------------
Vector Time (GMT): 2008/088/18:03:56
966
Vector Time (MET): 017/11:35:43
018
Weight (LBS) : 217128
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3331685
44 A = 6726846
23 meter
Y = -5614106
67 meter E =
0013207
Z = 1604275
77 I = 51
96371
XDOT = 3473
437602 Wp = 101
57680
YDOT = -3723
474646 meter/sec RA = 70
39693 deg
ZDOT = -5779
512876 TA = 60
78580
MA = 60
65378
Ha = 188
382 n
mi
Hp = 181
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10930726
52 X = -3276593
64
Y = -18418985
15 feet Y = -5650973
25 meter
Z = 5263371
95 Z = 1588224
74
XDOT = 11395
792657 XDOT = 3542
800275
YDOT = -12216
124168 feet/sec YDOT = -3684
332487 meter/sec
ZDOT = -18961
656418 ZDOT = -5762
470099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16999929
00 X = -5181578
36
Y = 13053457
70 feet Y = 3978693
91 meter
Z = 5201205
30 Z = 1585327
37
XDOT = -12534
000201 XDOT = -3820
363261
YDOT = -8744
772604 feet/sec YDOT = -2665
406690 meter/sec
ZDOT = -18896
683070 ZDOT = -5759
709000
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
78758268
00020000 00000-0 70000-3 0 9049
2 32699 51
6408 70
8922 0003764 6
0979 354
0230 15
75496801 2784
Satellite: SHUTTLE
Catalog Number: 32699
Epoch time: 08088
78758268 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 70
8922 deg
Eccentricity:
0003764
Arg of perigee: 6
0979 deg
Mean anomaly: 354
0230 deg
Mean motion: 15
75496801 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 278
Checksum: 333
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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