Date:
December 20th 2006
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
353/23:01:41
280 -2
3 0
0 3
0
009/21:14:06
307 0
4 -0
0 193
0
000/00:00:12
614 -1
9 3
0 176
2
353/23:29:55
982 6
3 -10
0 10
0
009/21:42:21
009 1
8 -0
0 192
9
000/00:00:42
017 7
5 0
0 170
9
354/00:15:12
676 -11
9 -18
5 18
5
009/22:27:37
703 -3
0 0
0 183
0
000/00:00:13
820 -13
9 -0
0 169
7
355/18:52:39
164 0
6 2
0 2
0
011/17:05:04
191 1
2 -0
0 184
3
000/00:00:08
382 1
4 0
0 169
1
Coasting Arc #1 (Orbit 145)
---------------------------------------
Vector Time (GMT): 2006/353/04:58:48
000
Vector Time (MET): 009/03:11:13
027
Weight (LBS) : 237270
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1813158
18 A = 6714972
42 meter
Y = 4003925
52 meter E =
0025989
Z = 5082008
33 I = 51
38575
XDOT = -5966
123305 Wp =
84333
YDOT = 4632
213025 meter/sec RA = 313
07641 deg
ZDOT = -1495
235201 TA = 103
69177
MA = 103
40229
Ha = 193
385 n
mi
Hp = 176
095
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5948681
68 X = 1743545
29
Y = 13136238
59 feet Y = 4023819
00 meter
Z = 16673255
66 Z = 5090648
42
XDOT = -19573
895359 XDOT = -6010
234665
YDOT = 15197
549294 feet/sec YDOT = 4565
223448 meter/sec
ZDOT = -4905
627299 ZDOT = -1524
325177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1417733
24 X = -432125
09
Y = -14312368
04 feet Y = -4362409
78 meter
Z = 16706022
44 Z = 5091995
64
XDOT = 22296
333477 XDOT = 6795
922444
YDOT = -8159
354654 feet/sec YDOT = -2486
971298 meter/sec
ZDOT = -5013
907487 ZDOT = -1528
239002
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
25250840
00014500 00000-0 95600-4 0 9003
2 29647 51
6359 313
4150 0023437 351
8276 8
2504 15
76079149 1466
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06353
25250840 = yrday
fracday
Element set: 900
Inclination: 51
6359 deg
RA of node: 313
4150 deg
Eccentricity:
0023437
Arg of perigee: 351
8276 deg
Mean anomaly: 8
2504 deg
Mean motion: 15
76079149 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 146
Checksum: 296
Coasting Arc #2 (Orbit 157)
---------------------------------------
Vector Time (GMT): 2006/353/23:01:47
587
Vector Time (MET): 009/21:14:12
614
Weight (LBS) : 237187
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5102975
20 A = 6718127
03 meter
Y = -863886
11 meter E =
0020638
Z = 4264822
34 I = 51
37978
XDOT = -1797
439227 Wp = 22
43255
YDOT = 6633
673836 meter/sec RA = 309
22196 deg
ZDOT = 3507
672811 TA = 32
05074
MA = 31
92540
Ha = 193
035 n
mi
Hp = 176
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16742044
62 X = 5091541
77
Y = -2834272
02 feet Y = -806863
85 meter
Z = 13992199
28 Z = 4289584
81
XDOT = -5897
110326 XDOT = -1888
553564
YDOT = 21764
021773 feet/sec YDOT = 6613
055496 meter/sec
ZDOT = 11508
112896 ZDOT = 3498
720814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2126891
46 X = 648276
52
Y = -16769248
12 feet Y = -5111266
83 meter
Z = 14084723
89 Z = 4293023
84
XDOT = 17872
363086 XDOT = 5447
496268
YDOT = 11868
815903 feet/sec YDOT = 3617
615087 meter/sec
ZDOT = 11475
376461 ZDOT = 3497
694745
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
01338634
00014500 00000-0 95600-4 0 9017
2 29647 51
6330 309
4906 0022171 356
8959 3
2064 15
76102120 1581
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06354
01338634 = yrday
fracday
Element set: 901
Inclination: 51
6330 deg
RA of node: 309
4906 deg
Eccentricity:
0022171
Arg of perigee: 356
8959 deg
Mean anomaly: 3
2064 deg
Mean motion: 15
76102120 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 158
Checksum: 285
Coasting Arc #3 (Orbit 157)
---------------------------------------
Vector Time (GMT): 2006/353/23:30:16
990
Vector Time (MET): 009/21:42:42
017
Weight (LBS) : 236913
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3389733
16 A = 6720304
48 meter
Y = 5693147
78 meter E =
0024054
Z = 1200346
27 I = 51
40444
XDOT = -4734
106798 Wp = 20
61655
YDOT = -1573
729042 meter/sec RA = 309
08367 deg
ZDOT = -5847
056289 TA = 146
19950
MA = 146
04593
Ha = 192
925 n
mi
Hp = 170
919
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11121171
80 X = -3458999
14
Y = 18678306
35 feet Y = 5654839
09 meter
Z = 3938143
95 Z = 1183711
75
XDOT = -15531
846449 XDOT = -4687
745921
YDOT = -5163
153024 feet/sec YDOT = -1626
429079 meter/sec
ZDOT = -19183
255541 ZDOT = -5869
942431
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16524142
52 X = 5036558
64
Y = 14141906
58 feet Y = 4310453
12 meter
Z = 3876565
56 Z = 1181577
18
XDOT = -6666
797512 XDOT = -2032
039882
YDOT = 13124
662694 feet/sec YDOT = 4000
397189 meter/sec
ZDOT = -19269
036804 ZDOT = -5873
202418
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
01334219
00014500 00000-0 95600-4 0 9023
2 29647 51
6330 309
4905 0030049 353
9954 6
0846 15
77960783 1583
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06354
01334219 = yrday
fracday
Element set: 902
Inclination: 51
6330 deg
RA of node: 309
4905 deg
Eccentricity:
0030049
Arg of perigee: 353
9954 deg
Mean anomaly: 6
0846 deg
Mean motion: 15
77960783 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 158
Checksum: 313
Coasting Arc #4 (Orbit 157)
---------------------------------------
Vector Time (GMT): 2006/354/00:15:19
586
Vector Time (MET): 009/22:27:44
613
Weight (LBS) : 236482
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3173239
95 A = 6710315
13 meter
Y = -5725342
17 meter E =
0023463
Z = -1413303
19 I = 51
40517
XDOT = 4914
666053 Wp = 14
88672
YDOT = 1299
565487 meter/sec RA = 308
92013 deg
ZDOT = 5813
696757 TA = 329
44768
MA = 329
58414
Ha = 183
030 n
mi
Hp = 169
696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10410892
23 X = 3243916
69
Y = -18783931
01 feet Y = -5689447
46 meter
Z = -4636821
50 Z = -1397716
98
XDOT = 16124
232457 XDOT = 4871
520767
YDOT = 4263
666297 feet/sec YDOT = 1354
303436 meter/sec
ZDOT = 19073
808258 ZDOT = 5837
467813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19059762
32 X = -5809415
56
Y = -9923685
69 feet Y = -3024739
40 meter
Z = -4579167
76 Z = -1395730
33
XDOT = 3104
379233 XDOT = 946
214790
YDOT = -14738
083677 feet/sec YDOT = -4492
167905 meter/sec
ZDOT = 19162
868813 ZDOT = 5840
842414
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
01334485
00014500 00000-0 95600-4 0 9039
2 29647 51
6351 309
4911 0015742 3
2467 356
8799 15
81410949 1582
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06354
01334485 = yrday
fracday
Element set: 903
Inclination: 51
6351 deg
RA of node: 309
4911 deg
Eccentricity:
0015742
Arg of perigee: 3
2467 deg
Mean anomaly: 356
8799 deg
Mean motion: 15
81410949 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 158
Checksum: 318
Coasting Arc #5 (Orbit 173)
---------------------------------------
Vector Time (GMT): 2006/355/00:17:24
872
Vector Time (MET): 010/22:29:49
899
Weight (LBS) : 236482
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2034884
10 A = 6700307
63 meter
Y = -4060296
58 meter E =
0018882
Z = -4934758
28 I = 51
35486
XDOT = 5374
206049 Wp = 49
55868
YDOT = -5136
667334 meter/sec RA = 303
69928 deg
ZDOT = 2027
479536 TA = 240
03446
MA = 240
22203
Ha = 183
040 n
mi
Hp = 169
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6676128
93 X = -1965339
67
Y = -13321183
01 feet Y = -4082670
86 meter
Z = -16190151
83 Z = -4944475
66
XDOT = 17631
909608 XDOT = 5421
419086
YDOT = -16852
583117 feet/sec YDOT = -5076
282324 meter/sec
ZDOT = 6651
835747 ZDOT = 2053
701068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12950321
59 X = -3947258
02
Y = 7288381
71 feet Y = 2221498
75 meter
Z = -16226961
92 Z = -4945977
99
XDOT = -17236
800634 XDOT = -5253
776833
YDOT = -15725
242272 feet/sec YDOT = -4793
053844 meter/sec
ZDOT = 6749
343002 ZDOT = 2057
199747
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
02440132
00014500 00000-0 95600-4 0 9049
2 29647 51
6352 304
2419 0015701 7
1863 352
9527 15
81457609 1745
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06355
02440132 = yrday
fracday
Element set: 904
Inclination: 51
6352 deg
RA of node: 304
2419 deg
Eccentricity:
0015701
Arg of perigee: 7
1863 deg
Mean anomaly: 352
9527 deg
Mean motion: 15
81457609 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 174
Checksum: 291
Coasting Arc #6 (Orbit 186)
---------------------------------------
Vector Time (GMT): 2006/355/18:52:43
355
Vector Time (MET): 011/17:05:08
382
Weight (LBS) : 236427
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4444219
49 A = 6710267
91 meter
Y = -4593492
36 meter E =
0027888
Z = 1982997
92 I = 51
37268
XDOT = 2421
829895 Wp = 35
54869
YDOT = 4761
259249 meter/sec RA = 299
69952 deg
ZDOT = 5584
815180 TA = 346
74192
MA = 346
81506
Ha = 184
346 n
mi
Hp = 169
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14580772
60 X = 4485641
53
Y = -15070513
01 feet Y = -4543543
50 meter
Z = 6505898
69 Z = 2004687
55
XDOT = 7945
636138 XDOT = 2341
257562
YDOT = 15620
929296 feet/sec YDOT = 4787
900509 meter/sec
ZDOT = 18322
884450 ZDOT = 5596
385621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10890468
31 X = 3319414
74
Y = -17890262
67 feet Y = -5452952
06 meter
Z = 6586517
39 Z = 2007570
50
XDOT = 9770
338543 XDOT = 2977
999188
YDOT = 12729
343820 feet/sec YDOT = 3879
903996 meter/sec
ZDOT = 18366
711967 ZDOT = 5598
173808
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
84588501
00014500 00000-0 95600-4 0 9053
2 29647 51
6343 299
9783 0017740 10
3144 349
8384 15
81107007 1876
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06355
84588501 = yrday
fracday
Element set: 905
Inclination: 51
6343 deg
RA of node: 299
9783 deg
Eccentricity:
0017740
Arg of perigee: 10
3144 deg
Mean anomaly: 349
8384 deg
Mean motion: 15
81107007 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 187
Checksum: 326
Coasting Arc #7 (Orbit 201)
---------------------------------------
Vector Time (GMT): 2006/356/18:54:32
848
Vector Time (MET): 012/17:06:57
875
Weight (LBS) : 236427
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 100918
48 A = 6708099
96 meter
Y = -5997228
65 meter E =
0020603
Z = -2987772
87 I = 51
35129
XDOT = 5424
668634 Wp = 24
49234
YDOT = -2361
519685 meter/sec RA = 294
43844 deg
ZDOT = 4954
036936 TA = 300
69456
MA = 300
89742
Ha = 184
522 n
mi
Hp = 168
908
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 331097
36 X = 182513
51
Y = -19675947
02 feet Y = -5995642
73 meter
Z = -9802404
44 Z = -2987085
52
XDOT = 17797
469272 XDOT = 5426
616982
YDOT = -7747
767996 feet/sec YDOT = -2300
823826 meter/sec
ZDOT = 16253
402022 ZDOT = 4980
394044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4417873
21 X = -1346567
75
Y = -19177377
16 feet Y = -5845264
56 meter
Z = -9800522
99 Z = -2987199
41
XDOT = 13888
740621 XDOT = 4233
288141
YDOT = -11504
663092 feet/sec YDOT = -3506
621311 meter/sec
ZDOT = 16351
741722 ZDOT = 4984
010877
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
79395269
00014500 00000-0 95600-4 0 9066
2 29647 51
6334 295
0569 0017729 14
1520 346
0140 15
81106262 2021
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06356
79395269 = yrday
fracday
Element set: 906
Inclination: 51
6334 deg
RA of node: 295
0569 deg
Eccentricity:
0017729
Arg of perigee: 14
1520 deg
Mean anomaly: 346
0140 deg
Mean motion: 15
81106262 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 202
Checksum: 304
Coasting Arc #8 (Orbit 217)
---------------------------------------
Vector Time (GMT): 2006/357/18:56:11
227
Vector Time (MET): 013/17:08:36
254
Weight (LBS) : 236427
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4048865
47 A = 6699822
70 meter
Y = -1124886
78 meter E =
0026913
Z = -5236417
73 I = 51
31195
XDOT = 2358
293894 Wp = 49
97163
YDOT = -7322
933193 meter/sec RA = 289
24691 deg
ZDOT = -234
073963 TA = 217
70099
MA = 217
88989
Ha = 184
560 n
mi
Hp = 168
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13283679
35 X = -4010543
42
Y = -3690573
42 feet Y = -1169966
33 meter
Z = -17179848
20 Z = -5255993
98
XDOT = 7737
184691 XDOT = 2441
174324
YDOT = -24025
371368 feet/sec YDOT = -7296
087287 meter/sec
ZDOT = -767
959197 ZDOT = -222
417346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13694841
30 X = -4174187
63
Y = -33840
23 feet Y = -10314
50 meter
Z = -17253226
66 Z = -5258783
48
XDOT = 1040
474509 XDOT = 317
136630
YDOT = -24221
558956 feet/sec YDOT = -7382
731170 meter/sec
ZDOT = -725
198203 ZDOT = -221
040412
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
80520344
00014500 00000-0 95600-4 0 9074
2 29647 51
6323 289
8076 0017694 18
4172 341
7632 15
81149636 2181
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06357
80520344 = yrday
fracday
Element set: 907
Inclination: 51
6323 deg
RA of node: 289
8076 deg
Eccentricity:
0017694
Arg of perigee: 18
4172 deg
Mean anomaly: 341
7632 deg
Mean motion: 15
81149636 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 218
Checksum: 322
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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