SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2006/344/01:47:34 973 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 12 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 06245
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
344/18:45:34
793 -47
5 56
8 56
8
000/16:57:59
820 -17
5 0
0 187
7
000/00:00:38
548 -25
6 -0
0 160
1
345/04:51:12
871 0
0 3
0 3
0
001/03:03:37
898 1
9 -0
0 189
2
000/00:00:13
137 2
4 -0
0 160
2
345/17:56:56
846 18
9 25
2 25
2
001/16:09:21
873 -12
1 0
0 191
1
000/00:00:18
538 -11
6 0
0 172
8
345/19:28:29
126 7
1 9
0 9
0
001/17:40:54
153 -4
4 -0
5 192
4
000/00:00:13
992 -3
3 0
5 176
6
345/20:45:24
710 0
9 2
5 3
9
001/18:57:49
737 -3
8 -2
6 192
5
000/00:00:17
159 -0
4 1
5 178
2
Coasting Arc #1 (Orbit 3)
---------------------------------------
Vector Time (GMT): 2006/344/05:00:06
000
Vector Time (MET): 000/03:12:31
027
Weight (LBS) : 248479
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1844920
30 A = 6665180
81 meter
Y = 3974827
91 meter E =
0062812
Z = 5032664
58 I = 51
62079
XDOT = -7409
583367 Wp = 332
86204
YDOT = 1381
686922 meter/sec RA = 359
65487 deg
ZDOT = 1688
168498 TA = 101
30243
MA = 100
59596
Ha = 180
650 n
mi
Hp = 134
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6052888
14 X = 1775870
20
Y = 13040773
97 feet Y = 3995080
34 meter
Z = 16511366
74 Z = 5041459
98
XDOT = -24309
656717 XDOT = -7432
689599
YDOT = 4533
093576 feet/sec YDOT = 1298
665641 meter/sec
ZDOT = 5538
610558 ZDOT = 1652
116881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 587554
57 X = 179086
63
Y = -14326614
24 feet Y = -4366752
02 meter
Z = 16544708
41 Z = 5042827
12
XDOT = 22710
644214 XDOT = 6922
204357
YDOT = 6933
179844 feet/sec YDOT = 2113
233217 meter/sec
ZDOT = 5403
945130 ZDOT = 1647
122476
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 29647U 06055A 06344
25819815
00014500 00000-0 95600-4 0 9006
2 29647 51
6415 359
8560 0067300 331
5339 28
2164 15
93768912 49
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06344
25819815 = yrday
fracday
Element set: 900
Inclination: 51
6415 deg
RA of node: 359
8560 deg
Eccentricity:
0067300
Arg of perigee: 331
5339 deg
Mean anomaly: 28
2164 deg
Mean motion: 15
93768912 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 4
Checksum: 312
Coasting Arc #2 (Orbit 12)
---------------------------------------
Vector Time (GMT): 2006/344/18:45:54
067
Vector Time (MET): 000/16:58:19
094
Weight (LBS) : 247096
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3777781
97 A = 6698555
80 meter
Y = 3579599
07 meter E =
0041157
Z = 4227095
56 I = 51
61551
XDOT = -6374
240620 Wp = 23
27008
YDOT = -2453
240553 meter/sec RA = 356
58908 deg
ZDOT = -3570
210423 TA = 103
18670
MA = 102
72719
Ha = 187
698 n
mi
Hp = 160
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12394297
82 X = -3838079
32
Y = 11744091
42 feet Y = 3536998
83 meter
Z = 13868423
74 Z = 4208597
08
XDOT = -20912
862928 XDOT = -6328
979494
YDOT = -8048
689478 feet/sec YDOT = -2524
296280 meter/sec
ZDOT = -11713
288788 ZDOT = -3601
066788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12450352
18 X = -3794867
34
Y = 11765791
22 feet Y = 3586213
16 meter
Z = 13799650
95 Z = 4206133
61
XDOT = -20003
745338 XDOT = -6097
141579
YDOT = -7104
264008 feet/sec YDOT = -2165
379670 meter/sec
ZDOT = -11828
961024 ZDOT = -3605
467320
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 29647U 06055A 06344
82286581
00014500 00000-0 95600-4 0 9018
2 29647 51
6412 356
8793 0035464 11
2289 348
9663 15
83134390 135
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06344
82286581 = yrday
fracday
Element set: 901
Inclination: 51
6412 deg
RA of node: 356
8793 deg
Eccentricity:
0035464
Arg of perigee: 11
2289 deg
Mean anomaly: 348
9663 deg
Mean motion: 15
83134390 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 13
Checksum: 320
Coasting Arc #3 (Orbit 19)
---------------------------------------
Vector Time (GMT): 2006/345/04:51:19
439
Vector Time (MET): 001/03:03:44
466
Weight (LBS) : 247010
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6657422
76 A = 6707876
09 meter
Y = -383441
88 meter E =
0048425
Z = 335005
96 I = 51
63027
XDOT = -38
264170 Wp = 21
06878
YDOT = 4823
408234 meter/sec RA = 354
42411 deg
ZDOT = 6058
714558 TA = 342
60042
MA = 342
76578
Ha = 189
188 n
mi
Hp = 160
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21841938
20 X = 6659589
68
Y = -1258011
42 feet Y = -308952
48 meter
Z = 1099100
92 Z = 367352
92
XDOT = -125
538617 XDOT = -121
651426
YDOT = 15824
830165 feet/sec YDOT = 4822
513058 meter/sec
ZDOT = 19877
672434 ZDOT = 6058
326664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19849474
09 X = -6050119
70
Y = -9185357
65 feet Y = -2799697
01 meter
Z = 1220025
89 Z = 371863
89
XDOT = 6998
841086 XDOT = 2133
246763
YDOT = -12397
000658 feet/sec YDOT = -3778
605800 meter/sec
ZDOT = 19876
770174 ZDOT = 6058
439549
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 29647U 06055A 06345
26474785
00014500 00000-0 95600-4 0 9023
2 29647 51
6418 354
5751 0037350 12
5007 347
7079 15
82569003 206
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06345
26474785 = yrday
fracday
Element set: 902
Inclination: 51
6418 deg
RA of node: 354
5751 deg
Eccentricity:
0037350
Arg of perigee: 12
5007 deg
Mean anomaly: 347
7079 deg
Mean motion: 15
82569003 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 20
Checksum: 306
Coasting Arc #4 (Orbit 27)
---------------------------------------
Vector Time (GMT): 2006/345/17:57:06
115
Vector Time (MET): 001/16:09:31
142
Weight (LBS) : 246397
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4348305
77 A = 6712981
75 meter
Y = -2802348
64 meter E =
0028247
Z = -4296385
98 I = 51
58729
XDOT = 5812
614250 Wp = 2
42934
YDOT = -3645
260003 meter/sec RA = 351
60991 deg
ZDOT = -3478
292216 TA = 232
19726
MA = 232
45334
Ha = 191
123 n
mi
Hp = 172
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14266095
06 X = -4295762
28
Y = -9194057
23 feet Y = -2850699
26 meter
Z = -14095754
53 Z = -4317382
73
XDOT = 19070
256726 XDOT = 5869
857279
YDOT = -11959
514445 feet/sec YDOT = -3579
913097 meter/sec
ZDOT = -11411
719868 ZDOT = -3449
915852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12142629
95 X = -3701073
61
Y = -11763495
34 feet Y = -3585513
38 meter
Z = -14174595
85 Z = -4320416
81
XDOT = 20226
533052 XDOT = 6165
047274
YDOT = -7149
258692 feet/sec YDOT = -2179
094049 meter/sec
ZDOT = -11306
015607 ZDOT = -3446
073557
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 29647U 06055A 06345
76993853
00014500 00000-0 95600-4 0 9031
2 29647 51
6416 351
9528 0026011 344
7239 15
3138 15
77899722 286
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06345
76993853 = yrday
fracday
Element set: 903
Inclination: 51
6416 deg
RA of node: 351
9528 deg
Eccentricity:
0026011
Arg of perigee: 344
7239 deg
Mean anomaly: 15
3138 deg
Mean motion: 15
77899722 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 28
Checksum: 334
Coasting Arc #5 (Orbit 28)
---------------------------------------
Vector Time (GMT): 2006/345/19:28:36
122
Vector Time (MET): 001/17:41:01
149
Weight (LBS) : 246179
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4258760
93 A = 6717498
65 meter
Y = -2843373
08 meter E =
0024932
Z = -4358216
66 I = 51
58497
XDOT = 5895
729298 Wp = 349
80695
YDOT = -3613
351056 meter/sec RA = 351
28027 deg
ZDOT = -3376
705937 TA = 246
00463
MA = 246
26584
Ha = 192
399 n
mi
Hp = 176
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13972312
75 X = -4205464
80
Y = -9328651
83 feet Y = -2890717
73 meter
Z = -14298611
10 Z = -4378776
58
XDOT = 19342
943891 XDOT = 5952
115705
YDOT = -11854
826299 feet/sec YDOT = -3547
079138 meter/sec
ZDOT = -11078
431552 ZDOT = -3347
927870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15505906
39 X = -4726200
27
Y = -6293020
96 feet Y = -1918112
79 meter
Z = -14375823
53 Z = -4381751
01
XDOT = 16113
446467 XDOT = 4911
378483
YDOT = -14438
743896 feet/sec YDOT = -4400
929139 meter/sec
ZDOT = -10971
221515 ZDOT = -3344
028318
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 29647U 06055A 06345
83328196
00014500 00000-0 95600-4 0 9042
2 29647 51
6419 351
6251 0024886 328
9913 30
9780 15
76226651 291
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06345
83328196 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 351
6251 deg
Eccentricity:
0024886
Arg of perigee: 328
9913 deg
Mean anomaly: 30
9780 deg
Mean motion: 15
76226651 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 29
Checksum: 330
Coasting Arc #6 (Orbit 29)
---------------------------------------
Vector Time (GMT): 2006/345/20:45:33
289
Vector Time (MET): 001/18:57:58
316
Weight (LBS) : 246067
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6644502
95 A = 6727314
26 meter
Y = 1095553
80 meter E =
0011522
Z = 50916
12 I = 51
60565
XDOT = -818
378837 Wp = 335
70870
YDOT = -4705
316289 meter/sec RA = 350
98052 deg
ZDOT = -6026
318256 TA = 203
73858
MA = 203
79177
Ha = 192
501 n
mi
Hp = 178
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21799550
35 X = -6656511
74
Y = 3594336
60 feet Y = 1021153
84 meter
Z = 167047
62 Z = 18608
03
XDOT = -2684
969938 XDOT = -736
406249
YDOT = -15437
389401 feet/sec YDOT = -4714
012440 meter/sec
ZDOT = -19771
385353 ZDOT = -6030
095320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16814876
86 X = -5125174
47
Y = 14332666
32 feet Y = 4368596
70 meter
Z = 46349
38 Z = 14127
29
XDOT = -9130
052546 XDOT = -2782
840016
YDOT = -10665
317538 feet/sec YDOT = -3250
788786 meter/sec
ZDOT = -19786
046912 ZDOT = -6030
787099
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 29647U 06055A 06345
89669013
00014500 00000-0 95600-4 0 9055
2 29647 51
6360 351
2986 0023400 325
1116 34
8513 15
75704883 308
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06345
89669013 = yrday
fracday
Element set: 905
Inclination: 51
6360 deg
RA of node: 351
2986 deg
Eccentricity:
0023400
Arg of perigee: 325
1116 deg
Mean anomaly: 34
8513 deg
Mean motion: 15
75704883 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 30
Checksum: 300
Coasting Arc #7 (Orbit 45)
---------------------------------------
Vector Time (GMT): 2006/346/20:50:32
857
Vector Time (MET): 002/19:02:57
884
Weight (LBS) : 246067
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1930713
34 A = 6717297
59 meter
Y = 4369742
55 meter E =
0024500
Z = 4737036
59 I = 51
54476
XDOT = -7222
035008 Wp = 346
68435
YDOT = -321
998992 meter/sec RA = 345
78759 deg
ZDOT = -2625
762106 TA = 129
27056
MA = 129
05297
Ha = 192
661 n
mi
Hp = 177
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6334361
36 X = -2002464
49
Y = 14336425
69 feet Y = 4347741
65 meter
Z = 15541458
62 Z = 4727483
28
XDOT = -23694
340577 XDOT = -7205
140244
YDOT = -1056
427139 feet/sec YDOT = -402
697929 meter/sec
ZDOT = -8614
705072 ZDOT = -2660
805909
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2509773
44 X = 764978
94
Y = 15506514
33 feet Y = 4726385
57 meter
Z = 15506231
72 Z = 4726299
43
XDOT = -19209
074317 XDOT = -5854
925852
YDOT = 11922
911018 feet/sec YDOT = 3634
103278 meter/sec
ZDOT = -8745
794888 ZDOT = -2665
718282
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 29647U 06055A 06346
91138786
00014500 00000-0 95600-4 0 9068
2 29647 51
6360 346
0726 0023641 329
0499 30
9271 15
75822009 462
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06346
91138786 = yrday
fracday
Element set: 906
Inclination: 51
6360 deg
RA of node: 346
0726 deg
Eccentricity:
0023641
Arg of perigee: 329
0499 deg
Mean anomaly: 30
9271 deg
Mean motion: 15
75822009 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 46
Checksum: 317
SPACE SHUTTLE ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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