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 06121
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
353/22:38:38
130 0
3 -0
0 1
5
009/20:51:03
157 -1
3 0
0 193
3
000/00:00:06
314 -0
7 -1
5 176
2
353/23:06:56
004 4
8 -10
0 10
0
009/21:19:21
031 -8
5 0
0 189
4
000/00:00:42
062 -2
1 0
0 174
3
353/23:52:12
667 -8
4 -18
2 18
2
009/22:04:37
694 15
6 -0
0 186
5
000/00:00:13
651 4
1 0
0 166
3
355/18:52:39
169 0
6 2
0 2
0
011/17:05:04
196 1
2 -0
0 187
9
000/00:00:08
392 1
4 0
0 165
8
Coasting Arc #1 (Orbit 129)
---------------------------------------
Vector Time (GMT): 2006/352/04:36:48
000
Vector Time (MET): 008/02:49:13
027
Weight (LBS) : 237484
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1850925
59 A = 6714670
34 meter
Y = 3874428
70 meter E =
0025074
Z = 5167870
94 I = 51
40571
XDOT = -6221
940405 Wp = 355
44037
YDOT = 4411
622294 meter/sec RA = 318
32522 deg
ZDOT = -1054
721938 TA = 104
79239
MA = 104
51445
Ha = 193
235 n
mi
Hp = 176
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6072590
53 X = 1782341
32
Y = 12711380
25 feet Y = 3894750
52 meter
Z = 16954957
16 Z = 5176696
94
XDOT = -20413
190304 XDOT = -6265
705013
YDOT = 14473
826423 feet/sec YDOT = 4341
772721 meter/sec
ZDOT = -3460
373811 ZDOT = -1085
054078
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -77942
70 X = -23756
94
Y = -14046857
06 feet Y = -4281482
03 meter
Z = 16988403
33 Z = 5178065
34
XDOT = 23565
414840 XDOT = 7182
738443
YDOT = -4548
531121 feet/sec YDOT = -1386
392286 meter/sec
ZDOT = -3573
316311 ZDOT = -1089
146811
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 06352
23797990
00014500 00000-0 95600-4 0 9002
2 29647 51
6364 318
6403 0023433 347
7778 12
2815 15
76049418 1306
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06352
23797990 = yrday
fracday
Element set: 900
Inclination: 51
6364 deg
RA of node: 318
6403 deg
Eccentricity:
0023433
Arg of perigee: 347
7778 deg
Mean anomaly: 12
2815 deg
Mean motion: 15
76049418 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 130
Checksum: 315
Coasting Arc #2 (Orbit 145)
---------------------------------------
Vector Time (GMT): 2006/353/04:41:20
487
Vector Time (MET): 009/02:53:45
514
Weight (LBS) : 237484
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5505966
20 A = 6722150
00 meter
Y = -2313620
68 meter E =
0026160
Z = 3047893
35 I = 51
41041
XDOT = -211
298897 Wp = 21
55764
YDOT = 5952
734950 meter/sec RA = 313
17584 deg
ZDOT = 4911
083147 TA = 14
00247
MA = 13
93008
Ha = 193
281 n
mi
Hp = 176
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18064193
57 X = 5516632
01
Y = -7590619
03 feet Y = -2251966
26 meter
Z = 9999650
09 Z = 3074667
07
XDOT = -693
237850 XDOT = -301
731449
YDOT = 19529
970310 feet/sec YDOT = 5949
864367 meter/sec
ZDOT = 16112
477516 ZDOT = 4909
838128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19542869
62 X = -5956666
66
Y = 36953
12 feet Y = 11263
31 meter
Z = 10099528
20 Z = 3078336
20
XDOT = 8275
891095 XDOT = 2522
491606
YDOT = -16283
185477 feet/sec YDOT = -4963
114933 meter/sec
ZDOT = 16108
491622 ZDOT = 4909
868246
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 06353
25250071
00014500 00000-0 95600-4 0 9010
2 29647 51
6361 313
4142 0023355 351
9857 8
0930 15
76068708 1465
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06353
25250071 = yrday
fracday
Element set: 901
Inclination: 51
6361 deg
RA of node: 313
4142 deg
Eccentricity:
0023355
Arg of perigee: 351
9857 deg
Mean anomaly: 8
0930 deg
Mean motion: 15
76068708 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 146
Checksum: 292
Coasting Arc #3 (Orbit 156)
---------------------------------------
Vector Time (GMT): 2006/353/22:38:41
287
Vector Time (MET): 009/20:51:06
314
Weight (LBS) : 237442
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1448890
71 A = 6721915
07 meter
Y = -5745652
22 meter E =
0023825
Z = -3148179
14 I = 51
39307
XDOT = 5908
914205 Wp = 4
61279
YDOT = -1140
307534 meter/sec RA = 309
25520 deg
ZDOT = 4826
527505 TA = 318
48827
MA = 318
66898
Ha = 193
298 n
mi
Hp = 176
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4753578
46 X = 1528350
66
Y = -18850565
04 feet Y = -5728998
36 meter
Z = -10328671
72 Z = -3140948
53
XDOT = 19386
201461 XDOT = 5897
784374
YDOT = -3741
166450 feet/sec YDOT = -1074
267633 meter/sec
ZDOT = 15835
063992 ZDOT = 4855
205932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15539294
92 X = -4736377
09
Y = -11705350
70 feet Y = -3567790
89 meter
Z = -10302273
94 Z = -3140133
10
XDOT = 3133
281928 XDOT = 955
024332
YDOT = -18115
792492 feet/sec YDOT = -5521
693552 meter/sec
ZDOT = 15942
204592 ZDOT = 4859
183959
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 06353
94996715
00014500 00000-0 95600-4 0 9029
2 29647 51
6335 309
8174 0022938 353
9218 6
1664 15
76090725 1578
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06353
94996715 = yrday
fracday
Element set: 902
Inclination: 51
6335 deg
RA of node: 309
8174 deg
Eccentricity:
0022938
Arg of perigee: 353
9218 deg
Mean anomaly: 6
1664 deg
Mean motion: 15
76090725 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 157
Checksum: 334
Coasting Arc #4 (Orbit 157)
---------------------------------------
Vector Time (GMT): 2006/353/23:07:17
035
Vector Time (MET): 009/21:19:42
062
Weight (LBS) : 237168
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4160013
31 A = 6709444
58 meter
Y = 1338671
76 meter E =
0019311
Z = 5092858
68 I = 51
36842
XDOT = -3837
245946 Wp = 340
12885
YDOT = 6526
185210 meter/sec RA = 309
18867 deg
ZDOT = 1438
462318 TA = 96
15644
MA = 95
93639
Ha = 189
400 n
mi
Hp = 174
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13648337
63 X = 4119988
40
Y = 4391967
71 feet Y = 1384984
99 meter
Z = 16708853
93 Z = 5112971
20
XDOT = -12589
389588 XDOT = -3916
954235
YDOT = 21411
368798 feet/sec YDOT = 6482
811732 meter/sec
ZDOT = 4719
364560 ZDOT = 1419
628561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7855695
39 X = 2394415
96
Y = -11888222
53 feet Y = -3623530
23 meter
Z = 16784234
12 Z = 5115834
56
XDOT = 16392
945550 XDOT = 4996
569804
YDOT = 17307
036057 feet/sec YDOT = 5275
184590 meter/sec
ZDOT = 4649
654087 ZDOT = 1417
214566
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 06354
01329714
00014500 00000-0 95600-4 0 9038
2 29647 51
6332 309
4894 0023148 334
2277 25
7733 15
77973578 1583
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06354
01329714 = yrday
fracday
Element set: 903
Inclination: 51
6332 deg
RA of node: 309
4894 deg
Eccentricity:
0023148
Arg of perigee: 334
2277 deg
Mean anomaly: 25
7733 deg
Mean motion: 15
77973578 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 158
Checksum: 328
Coasting Arc #5 (Orbit 157)
---------------------------------------
Vector Time (GMT): 2006/353/23:52:19
493
Vector Time (MET): 009/22:04:44
520
Weight (LBS) : 236743
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4317526
74 A = 6700052
85 meter
Y = -1061942
93 meter E =
0032643
Z = -5033707
67 I = 51
37019
XDOT = 3607
493498 Wp = 31
22681
YDOT = -6584
999339 meter/sec RA = 309
03044 deg
ZDOT = -1682
367696 TA = 222
39358
MA = 222
64623
Ha = 186
510 n
mi
Hp = 166
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14165113
98 X = -4280873
12
Y = -3484064
72 feet Y = -1110037
14 meter
Z = -16514788
94 Z = -5054593
52
XDOT = 11835
608589 XDOT = 3689
061657
YDOT = -21604
328541 feet/sec YDOT = -6544
185654 meter/sec
ZDOT = -5519
579054 ZDOT = -1664
645582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4508617
29 X = -1374226
55
Y = 13779372
83 feet Y = 4199952
84 meter
Z = -16593030
74 Z = -5057555
77
XDOT = -19669
232170 XDOT = -5995
181966
YDOT = -13092
552467 feet/sec YDOT = -3990
609992 meter/sec
ZDOT = -5454
033089 ZDOT = -1662
389286
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 06354
01328444
00014500 00000-0 95600-4 0 9048
2 29647 51
6346 309
4908 0025132 8
6380 351
5214 15
81393088 1587
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06354
01328444 = yrday
fracday
Element set: 904
Inclination: 51
6346 deg
RA of node: 309
4908 deg
Eccentricity:
0025132
Arg of perigee: 8
6380 deg
Mean anomaly: 351
5214 deg
Mean motion: 15
81393088 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 158
Checksum: 302
Coasting Arc #6 (Orbit 173)
---------------------------------------
Vector Time (GMT): 2006/354/23:53:46
359
Vector Time (MET): 010/22:06:11
386
Weight (LBS) : 236743
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4580681
92 A = 6710080
44 meter
Y = 4688067
78 meter E =
0020745
Z = -1498837
19 I = 51
38733
XDOT = -2603
799832 Wp = 29
88199
YDOT = -4380
837866 meter/sec RA = 303
81312 deg
ZDOT = -5761
284885 TA = 166
69422
MA = 166
63943
Ha = 186
630 n
mi
Hp = 166
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15028483
99 X = -4625503
72
Y = 15380799
80 feet Y = 4636573
20 meter
Z = -4917444
85 Z = -1521198
07
XDOT = -8542
650367 XDOT = -2526
612208
YDOT = -14372
827645 feet/sec YDOT = -4409
533692 meter/sec
ZDOT = -18901
853298 ZDOT = -5773
747559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14611778
82 X = 4453670
18
Y = 15751060
50 feet Y = 4800923
24 meter
Z = -5000561
00 Z = -1524170
99
XDOT = -13627
939876 XDOT = -4153
796074
YDOT = 6643
317047 feet/sec YDOT = 2024
883036 meter/sec
ZDOT = -18948
969026 ZDOT = -5775
645759
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 06355
02436505
00014500 00000-0 95600-4 0 9059
2 29647 51
6344 304
2393 0025148 12
5192 347
6594 15
81430323 1747
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06355
02436505 = yrday
fracday
Element set: 905
Inclination: 51
6344 deg
RA of node: 304
2393 deg
Eccentricity:
0025148
Arg of perigee: 12
5192 deg
Mean anomaly: 347
6594 deg
Mean motion: 15
81430323 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 174
Checksum: 293
Coasting Arc #7 (Orbit 186)
---------------------------------------
Vector Time (GMT): 2006/355/18:52:43
365
Vector Time (MET): 011/17:05:08
392
Weight (LBS) : 236689
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4445445
67 A = 6710353
33 meter
Y = -4578439
51 meter E =
0037245
Z = 1993794
87 I = 51
37283
XDOT = 2410
599508 Wp = 32
66102
YDOT = 4779
714435 meter/sec RA = 299
69863 deg
ZDOT = 5584
020749 TA = 349
77975
MA = 349
85527
Ha = 187
859 n
mi
Hp = 165
842
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14584795
51 X = 4486646
79
Y = -15021126
99 feet Y = -4528478
16 meter
Z = 6541321
76 Z = 2015489
93
XDOT = 7908
791036 XDOT = 2329
825419
YDOT = 15681
477805 feet/sec YDOT = 4806
228932 meter/sec
ZDOT = 18320
278047 ZDOT = 5595
536146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10905006
78 X = 3323846
07
Y = -17842921
47 feet Y = -5438522
46 meter
Z = 6621962
46 Z = 2018374
16
XDOT = 9751
125891 XDOT = 2972
143172
YDOT = 12795
421336 feet/sec YDOT = 3900
044423 meter/sec
ZDOT = 18363
901746 ZDOT = 5597
317252
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 06355
84586762
00014500 00000-0 95600-4 0 9061
2 29647 51
6345 299
9774 0027081 15
2323 344
9653 15
81070762 1872
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06355
84586762 = yrday
fracday
Element set: 906
Inclination: 51
6345 deg
RA of node: 299
9774 deg
Eccentricity:
0027081
Arg of perigee: 15
2323 deg
Mean anomaly: 344
9653 deg
Mean motion: 15
81070762 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 187
Checksum: 340
Coasting Arc #8 (Orbit 201)
---------------------------------------
Vector Time (GMT): 2006/356/18:54:28
028
Vector Time (MET): 012/17:06:53
055
Weight (LBS) : 236689
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 69294
49 A = 6708119
34 meter
Y = -5980845
78 meter E =
0030015
Z = -3015237
16 I = 51
35125
XDOT = 5427
520634 Wp = 25
70348
YDOT = -2402
909313 meter/sec RA = 294
43796 deg
ZDOT = 4935
910961 TA = 299
09981
MA = 299
40001
Ha = 188
033 n
mi
Hp = 165
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 227344
14 X = 150842
03
Y = -19622197
45 feet Y = -5979613
90 meter
Z = -9892510
38 Z = -3014703
55
XDOT = 17806
826226 XDOT = 5430
019830
YDOT = -7883
560738 feet/sec YDOT = -2342
178464 meter/sec
ZDOT = 16193
933598 ZDOT = 4962
283254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4498213
11 X = -1371055
36
Y = -19101682
56 feet Y = -5822192
85 meter
Z = -9891202
24 Z = -3014838
44
XDOT = 13874
788800 XDOT = 4229
035626
YDOT = -11627
501815 feet/sec YDOT = -3544
062553 meter/sec
ZDOT = 16292
325348 ZDOT = 4965
900766
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 06356
79395623
00014500 00000-0 95600-4 0 9071
2 29647 51
6336 295
0563 0027060 18
9856 341
2313 15
81071698 2023
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06356
79395623 = yrday
fracday
Element set: 907
Inclination: 51
6336 deg
RA of node: 295
0563 deg
Eccentricity:
0027060
Arg of perigee: 18
9856 deg
Mean anomaly: 341
2313 deg
Mean motion: 15
81071698 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 202
Checksum: 321
Coasting Arc #9 (Orbit 217)
---------------------------------------
Vector Time (GMT): 2006/357/18:56:29
004
Vector Time (MET): 013/17:08:54
031
Weight (LBS) : 236689
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4014692
04 A = 6699904
77 meter
Y = -1236101
92 meter E =
0035915
Z = -5241949
04 I = 51
31212
XDOT = 2440
681264 Wp = 45
51914
YDOT = -7294
567539 meter/sec RA = 289
24445 deg
ZDOT = -124
856785 TA = 223
14835
MA = 223
43036
Ha = 188
063 n
mi
Hp = 165
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13171561
81 X = -3975101
54
Y = -4055452
50 feet Y = -1280792
08 meter
Z = -17197995
55 Z = -5261356
22
XDOT = 8007
484461 XDOT = 2522
707700
YDOT = -23932
308198 feet/sec YDOT = -7266
804758 meter/sec
ZDOT = -409
635123 ZDOT = -112
802005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13684687
38 X = -4171092
71
Y = -397695
79 feet Y = -121217
68 meter
Z = -17270754
35 Z = -5264125
93
XDOT = 1264
687859 XDOT = 385
476859
YDOT = -24205
982478 feet/sec YDOT = -7377
983459 meter/sec
ZDOT = -365
381041 ZDOT = -111
368141
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 06357
80522843
00014500 00000-0 95600-4 0 9081
2 29647 51
6325 289
8070 0027014 23
1271 337
1105 15
81117567 2189
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06357
80522843 = yrday
fracday
Element set: 908
Inclination: 51
6325 deg
RA of node: 289
8070 deg
Eccentricity:
0027014
Arg of perigee: 23
1271 deg
Mean anomaly: 337
1105 deg
Mean motion: 15
81117567 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 218
Checksum: 297
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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