Date: September 17th 2006

SHUTTLE TRAJECTORY DATA

Lift off time (UTC) : 2006/252/15:14:54 972 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 12 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 16339

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


260/14:04:57 861 0 4 0 4 1 6
007/22:50:02 889 -1 1 -0 0 189 6
000/00:00:05 778 -1 0 -1 5 180 4

260/14:32:56 832 -0 3 1 0 1 0
007/23:18:01 861 0 7 0 0 190 2
000/00:00:03 721 0 7 -0 0 180 6

260/16:14:54 972 -0 0 0 0 0 0
008/01:00:00 001 0 0 0 0 190 2
000/00:00:00 043 0 0 0 0 180 5

261/17:19:54 969 -0 9 -1 5 1 5
009/02:04:59 997 0 3 0 0 190 2
000/00:00:05 639 1 2 -0 0 179 6

Coasting Arc #1 (Orbit 91)
---------------------------------------

Vector Time (GMT): 2006/258/08:18:45
000
Vector Time (MET): 005/17:03:50
028
Weight (LBS)     : 209988
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4197950
51                 A    =         6715352
86  meter
 Y    =        -592083
34  meter          E    =           
0013134
 Z    =        5210123
28                 I    =           51
92811
 XDOT =       -216
230430                 Wp   =          358
68449
 YDOT =      -7630
334359  meter/sec      RA   =           82
31821  deg
 ZDOT =      -1028
542373                 TA   =          101
15541
                                          MA   =          101
00772
                                          Ha   =            189
623  n
mi
                                          Hp   =            180
630

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13772803
50                 X    =        -4216319
90
 Y    =       -1942530
66  feet           Y    =         -639180
25  meter
 Z    =       17093580
30                 Z    =         5189685
04
 XDOT =       -709
417421                 XDOT =        -125
803518
 YDOT =     -25033
905378  feet/sec       YDOT =       -7632
248750  meter/sec
 ZDOT =      -3374
482851                 ZDOT =       -1029
373563

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4822415
03                 X    =         1469872
10
 Y    =       13145626
63  feet           Y    =         4006787
00  meter
 Z    =       17017368
85                 Z    =         5186894
03
 XDOT =     -20794
643863                 XDOT =       -6338
207449
 YDOT =      12056
743422  feet/sec       YDOT =        3674
895395  meter/sec
 ZDOT =      -3378
621153                 ZDOT =       -1029
803728


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 29391U 06036A   06258
39221257  
00014500  00000-0  95600-4 0  9007
2 29391  51
6343  82
7833 0011622 343
3367  16
7414 15
75791565   925


Satellite: SHUTTLE
Catalog Number: 29391
Epoch time:      06258
39221257   =   yrday
fracday
Element set:     900
Inclination:       51
6343  deg
RA of node:        82
7833  deg
Eccentricity:     
0011622     
Arg of perigee:   343
3367  deg
Mean anomaly:      16
7414  deg
Mean motion:   15
75791565  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:              92
Checksum:              300


Coasting Arc #2 (Orbit 107)
---------------------------------------

Vector Time (GMT): 2006/259/08:23:19
445
Vector Time (MET): 006/17:08:24
474
Weight (LBS)     : 209988
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1046150
78                 A    =         6723304
46  meter
 Y    =        5922981
99  meter          E    =           
0016867
 Z    =        2979063
20                 I    =           51
94924
 XDOT =      -4791
740682                 Wp   =           38
97828
 YDOT =      -3370
622899  meter/sec      RA   =           77
20649  deg
 ZDOT =       5016
394713                 TA   =          355
32914
                                          MA   =          355
34486
                                          Ha   =            189
849  n
mi
                                          Hp   =            180
341

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3432253
21                 X    =        -1126846
71
 Y    =       19432355
60  feet           Y    =         5910819
09  meter
 Z    =        9773829
39                 Z    =         2973785
27
 XDOT =     -15720
933995                 XDOT =       -4778
021567
 YDOT =     -11058
474078  feet/sec       YDOT =       -3424
187307  meter/sec
 ZDOT =      16457
987904                 ZDOT =        4993
149767

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18542140
63                 X    =         5651644
46
 Y    =       -6778939
82  feet           Y    =        -2066220
86  meter
 Z    =        9754975
29                 Z    =         2973316
47
 XDOT =      -2080
880007                 XDOT =        -634
252226
 YDOT =      17877
504663  feet/sec       YDOT =        5449
063421  meter/sec
 ZDOT =      16370
937363                 ZDOT =        4989
861708


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 29391U 06036A   06259
40690584  
00014500  00000-0  95600-4 0  9014
2 29391  51
6340  77
5574 0011781 347
6079  12
4794 15
75763564  1089


Satellite: SHUTTLE
Catalog Number: 29391
Epoch time:      06259
40690584   =   yrday
fracday
Element set:     901
Inclination:       51
6340  deg
RA of node:        77
5574  deg
Eccentricity:     
0011781     
Arg of perigee:   347
6079  deg
Mean anomaly:      12
4794  deg
Mean motion:   15
75763564  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             108
Checksum:              321


Coasting Arc #3 (Orbit 122)
---------------------------------------

Vector Time (GMT): 2006/260/08:23:21
283
Vector Time (MET): 007/17:08:26
312
Weight (LBS)     : 209988
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4334872
89                 A    =         6720140
67  meter
 Y    =        3222397
23  meter          E    =           
0010554
 Z    =       -3995112
53                 I    =           51
93101
 XDOT =      -1170
642572                 Wp   =           26
17016
 YDOT =       6491
719669  meter/sec      RA   =           72
02790  deg
 ZDOT =       3979
140784                 TA   =          284
77438
                                          MA   =          284
89130
                                          Ha   =            189
924  n
mi
                                          Hp   =            180
145

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14222023
92                 X    =         4317885
82
 Y    =       10572169
39  feet           Y    =         3270828
85  meter
 Z    =      -13107324
56                 Z    =        -3974095
08
 XDOT =      -3840
690852                 XDOT =       -1262
553830
 YDOT =      21298
292878  feet/sec       YDOT =        6478
100397  meter/sec
 ZDOT =      13054
923832                 ZDOT =        3973
230769

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1624240
31                 X    =          495068
45
 Y    =      -17704700
65  feet           Y    =        -5396392
76  meter
 Z    =      -13028588
01                 Z    =        -3971113
63
 XDOT =      18947
282568                 XDOT =        5775
131727
 YDOT =      -7821
007343  feet/sec       YDOT =       -2383
843038  meter/sec
 ZDOT =      13033
791119                 ZDOT =        3972
699533


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 29391U 06036A   06260
35816321  
00014500  00000-0  95600-4 0  9020
2 29391  51
6336  72
6583 0011798 350
2054   9
8879 15
75811954  1239


Satellite: SHUTTLE
Catalog Number: 29391
Epoch time:      06260
35816321   =   yrday
fracday
Element set:     902
Inclination:       51
6336  deg
RA of node:        72
6583  deg
Eccentricity:     
0011798     
Arg of perigee:   350
2054  deg
Mean anomaly:       9
8879  deg
Mean motion:   15
75811954  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             123
Checksum:              307


Coasting Arc #4 (Orbit 126)
---------------------------------------

Vector Time (GMT): 2006/260/14:05:00
749
Vector Time (MET): 007/22:50:05
778
Weight (LBS)     : 209950
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         668457
21                 A    =         6722617
06  meter
 Y    =       -5850835
83  meter          E    =           
0010494
 Z    =       -3256359
08                 I    =           51
93438
 XDOT =       5084
620929                 Wp   =           18
36554
 YDOT =       3242
178734  meter/sec      RA   =           70
85681  deg
 ZDOT =      -4776
008706                 TA   =          199
56032
                                          MA   =          199
60060
                                          Ha   =            189
636  n
mi
                                          Hp   =            180
370

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2193101
07                 X    =          749720
65
 Y    =      -19195655
61  feet           Y    =        -5842897
89  meter
 Z    =      -10683592
78                 Z    =        -3252914
48
 XDOT =      16681
827194                 XDOT =        5071
150011
 YDOT =      10637
069337  feet/sec       YDOT =        3299
023061  meter/sec
 ZDOT =     -15669
319902                 ZDOT =       -4751
340495

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6674622
49                 X    =         2034424
94
 Y    =       18138062
72  feet           Y    =         5528481
52  meter
 Z    =      -10671557
36                 Z    =        -3252690
68
 XDOT =     -18443
458912                 XDOT =       -5621
566276
 YDOT =      -2388
538169  feet/sec       YDOT =        -728
026434  meter/sec
 ZDOT =     -15576
979227                 ZDOT =       -4747
863268


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 29391U 06036A   06260
61183391  
00014500  00000-0  95600-4 0  9034
2 29391  51
6313  71
3468 0010548 353
0848   7
0169 15
75743495  1276


Satellite: SHUTTLE
Catalog Number: 29391
Epoch time:      06260
61183391   =   yrday
fracday
Element set:     903
Inclination:       51
6313  deg
RA of node:        71
3468  deg
Eccentricity:     
0010548     
Arg of perigee:   353
0848  deg
Mean anomaly:       7
0169  deg
Mean motion:   15
75743495  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             127
Checksum:              298


Coasting Arc #5 (Orbit 126)
---------------------------------------

Vector Time (GMT): 2006/260/14:32:58
693
Vector Time (MET): 007/23:18:03
721
Weight (LBS)     : 209926
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3951147
79                 A    =         6724418
34  meter
 Y    =        4656621
45  meter          E    =           
0013713
 Z    =       -2798132
12                 I    =           51
93922
 XDOT =      -2462
747446                 Wp   =            9
79909
 YDOT =       5175
527861  meter/sec      RA   =           70
70912  deg
 ZDOT =       5152
370050                 TA   =          318
26045
                                          MA   =          318
36499
                                          Ha   =            190
183  n
mi
                                          Hp   =            180
593

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12963083
30                 X    =         3912319
84
 Y    =       15277629
43  feet           Y    =         4700635
18  meter
 Z    =       -9180223
50                 Z    =        -2779031
84
 XDOT =      -8079
880072                 XDOT =       -2545
528258
 YDOT =      16980
078285  feet/sec       YDOT =        5147
495263  meter/sec
 ZDOT =      16904
101213                 ZDOT =        5140
205167

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19322913
04                 X    =        -5889623
89
 Y    =       -5420837
18  feet           Y    =        -1652271
17  meter
 Z    =       -9108432
86                 Z    =        -2776250
34
 XDOT =      -3083
674948                 XDOT =        -939
904124
 YDOT =     -17242
665506  feet/sec       YDOT =       -5255
564446  meter/sec
 ZDOT =      16859
487181                 ZDOT =        5138
771693


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 29391U 06036A   06260
61183382  
00014500  00000-0  95600-4 0  9045
2 29391  51
6323  71
3471 0011256 351
2115   8
8851 15
75544311  1278


Satellite: SHUTTLE
Catalog Number: 29391
Epoch time:      06260
61183382   =   yrday
fracday
Element set:     904
Inclination:       51
6323  deg
RA of node:        71
3471  deg
Eccentricity:     
0011256     
Arg of perigee:   351
2115  deg
Mean anomaly:       8
8851  deg
Mean motion:   15
75544311  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             127
Checksum:              271


Coasting Arc #6 (Orbit 128)
---------------------------------------

Vector Time (GMT): 2006/260/16:14:54
994
Vector Time (MET): 008/01:00:00
022
Weight (LBS)     : 209925
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1549378
42                 A    =         6727429
09  meter
 Y    =        6468657
16  meter          E    =           
0021317
 Z    =         910603
13                 I    =           51
95021
 XDOT =      -4858
192767                 Wp   =           26
25408
 YDOT =        316
678024  meter/sec      RA   =           70
37922  deg
 ZDOT =       5982
532287                 TA   =          343
66396
                                          MA   =          343
73257
                                          Ha   =            190
164  n
mi
                                          Hp   =            180
538

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5083262
54                 X    =         1472429
08
 Y    =       21222628
49  feet           Y    =         6485570
91  meter
 Z    =        2987543
07                 Z    =          917943
16
 XDOT =     -15938
952649                 XDOT =       -4890
437751
 YDOT =       1038
969894  feet/sec       YDOT =         262
112541  meter/sec
 ZDOT =      19627
730599                 ZDOT =        5958
853087

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20852996
14                 X    =        -6355993
22
 Y    =       -6420484
46  feet           Y    =        -1956963
66  meter
 Z    =        3015769
02                 Z    =          919206
40
 XDOT =       6791
437599                 XDOT =        2070
030180
 YDOT =     -12827
927218  feet/sec       YDOT =       -3909
952216  meter/sec
 ZDOT =      19539
558906                 ZDOT =        5955
657554


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 29391U 06036A   06260
73868772  
00014500  00000-0  95600-4 0  9052
2 29391  51
6338  70
6950 0011347 351
6549   8
4424 15
75544366  1298


Satellite: SHUTTLE
Catalog Number: 29391
Epoch time:      06260
73868772   =   yrday
fracday
Element set:     905
Inclination:       51
6338  deg
RA of node:        70
6950  deg
Eccentricity:     
0011347     
Arg of perigee:   351
6549  deg
Mean anomaly:       8
4424  deg
Mean motion:   15
75544366  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             129
Checksum:              318


Coasting Arc #7 (Orbit 143)
---------------------------------------

Vector Time (GMT): 2006/261/16:15:01
115
Vector Time (MET): 009/01:00:06
143
Weight (LBS)     : 209925
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4398418
22                 A    =         6716487
77  meter
 Y    =          18044
59  meter          E    =           
0014845
 Z    =       -5084300
96                 I    =           51
90298
 XDOT =       1900
690567                 Wp   =           55
66587
 YDOT =       7265
927321  meter/sec      RA   =           65
22951  deg
 ZDOT =       1681
720599                 TA   =          230
38901
                                          MA   =          230
52015
                                          Ha   =            190
265  n
mi
                                          Hp   =            180
334

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14430505
96                 X    =         4422587
13
 Y    =          59201
42  feet           Y    =           67417
82  meter
 Z    =      -16680777
43                 Z    =        -5062874
94
 XDOT =       6235
861440                 XDOT =        1811
044468
 YDOT =      23838
344229  feet/sec       YDOT =        7286
702773  meter/sec
 ZDOT =       5517
456035                 ZDOT =        1690
736311

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7209305
30                 X    =        -2197396
26
 Y    =       12606571
89  feet           Y    =         3842483
11  meter
 Z    =      -16600951
93                 Z    =        -5059970
15
 XDOT =     -22880
880895                 XDOT =       -6974
092497
 YDOT =      -5824
243208  feet/sec       YDOT =       -1775
229330  meter/sec
 ZDOT =       5552
035331                 ZDOT =        1692
260369


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 29391U 06036A   06261
69008739  
00014500  00000-0  95600-4 0  9068
2 29391  51
6337  65
7979 0011371 355
2006   4
9047 15
75597850  1443


Satellite: SHUTTLE
Catalog Number: 29391
Epoch time:      06261
69008739   =   yrday
fracday
Element set:     906
Inclination:       51
6337  deg
RA of node:        65
7979  deg
Eccentricity:     
0011371     
Arg of perigee:   355
2006  deg
Mean anomaly:       4
9047  deg
Mean motion:   15
75597850  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             144
Checksum:              319


Coasting Arc #8 (Orbit 144)
---------------------------------------

Vector Time (GMT): 2006/261/17:19:57
789
Vector Time (MET): 009/02:05:02
817
Weight (LBS)     : 209888
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2691677
85                 A    =         6726885
09  meter
 Y    =       -6164448
27  meter          E    =           
0008192
 Z    =        -209381
52                 I    =           51
93919
 XDOT =       4422
608272                 Wp   =           61
03060
 YDOT =      -1731
377871  meter/sec      RA   =           65
01512  deg
 ZDOT =      -6053
714819                 TA   =          121
23406
                                          MA   =          121
15376
                                          Ha   =            190
232  n
mi
                                          Hp   =            179
566

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8830964
08                 X    =        -2621455
16
 Y    =      -20224567
82  feet           Y    =        -6194187
12  meter
 Z    =        -686947
25                 Z    =         -222286
99
 XDOT =      14509
869658                 XDOT =        4471
067701
 YDOT =      -5680
373593  feet/sec       YDOT =       -1681
597898  meter/sec
 ZDOT =     -19861
269090                 ZDOT =       -6032
112274

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21709256
57                 X    =         6616981
40
 Y    =       -3956974
15  feet           Y    =        -1206085
72  meter
 Z    =        -735867
76                 Z    =         -224292
49
 XDOT =       1889
947457                 XDOT =         576
055985
 YDOT =      13948
780817  feet/sec       YDOT =        4251
588393  meter/sec
 ZDOT =     -19781
024491                 ZDOT =       -6029
256265


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 29391U 06036A   06261
75350823  
00014500  00000-0  95600-4 0  9070
2 29391  51
6329  65
4723 0012570 355
8969   4
2090 15
75850000  1455


Satellite: SHUTTLE
Catalog Number: 29391
Epoch time:      06261
75350823   =   yrday
fracday
Element set:     907
Inclination:       51
6329  deg
RA of node:        65
4723  deg
Eccentricity:     
0012570     
Arg of perigee:   355
8969  deg
Mean anomaly:       4
2090  deg
Mean motion:   15
75850000  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             145
Checksum:              293


Coasting Arc #9 (Orbit 160)
---------------------------------------

Vector Time (GMT): 2006/262/17:20:02
355
Vector Time (MET): 010/02:05:07
383
Weight (LBS)     : 209888
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4094276
33                 A    =         6715021
98  meter
 Y    =        1087389
47  meter          E    =           
0014948
 Z    =        5209910
17                 I    =           51
88718
 XDOT =      -3137
897831                 Wp   =           10
67649
 YDOT =      -6965
800817  meter/sec      RA   =           59
87260  deg
 ZDOT =       -997
246691                 TA   =           88
87766
                                          MA   =           88
70641
                                          Ha   =            190
396  n
mi
                                          Hp   =            179
254

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13432665
11                 X    =        -4131452
40
 Y    =        3567550
74  feet           Y    =         1041348
25  meter
 Z    =       17092881
12                 Z    =         5189929
99
 XDOT =     -10294
940392                 XDOT =       -3054
844257
 YDOT =     -22853
677220  feet/sec       YDOT =       -7000
463066  meter/sec
 ZDOT =      -3271
806730                 ZDOT =       -1012
288602

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -617452
82                 X    =         -188199
62
 Y    =      -13975577
15  feet           Y    =        -4259755
92  meter
 Z    =       17018592
50                 Z    =         5187266
99
 XDOT =      23494
146826                 XDOT =        7161
015953
 YDOT =      -5151
143649  feet/sec       YDOT =       -1570
068584  meter/sec
 ZDOT =      -3328
797505                 ZDOT =       -1014
617480


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 29391U 06036A   06262
76813931  
00014500  00000-0  95600-4 0  9087
2 29391  51
6337  60
2455 0012699 359
1094   1
0046 15
75903841  1613


Satellite: SHUTTLE
Catalog Number: 29391
Epoch time:      06262
76813931   =   yrday
fracday
Element set:     908
Inclination:       51
6337  deg
RA of node:        60
2455  deg
Eccentricity:     
0012699     
Arg of perigee:   359
1094  deg
Mean anomaly:       1
0046  deg
Mean motion:   15
75903841  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             161
Checksum:              298


Coasting Arc #10 (Orbit 176)
---------------------------------------

Vector Time (GMT): 2006/263/17:25:19
666
Vector Time (MET): 011/02:10:24
694
Weight (LBS)     : 209888
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1040028
34                 A    =         6722304
78  meter
 Y    =        5809422
21  meter          E    =           
0019127
 Z    =        3191757
41                 I    =           51
89600
 XDOT =      -5788
933829                 Wp   =           45
21456
 YDOT =      -1622
368032  meter/sec      RA   =           54
75570  deg
 ZDOT =       4834
919409                 TA   =          351
98068
                                          MA   =          352
01121
                                          Ha   =            190
475  n
mi
                                          Hp   =            178
966

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3412166
47                 X    =          959415
01
 Y    =       19059784
16  feet           Y    =         5820613
68  meter
 Z    =       10471645
04                 Z    =         3196613
82
 XDOT =     -18992
565057                 XDOT =       -5793
829018
 YDOT =      -5322
729763  feet/sec       YDOT =       -1687
199291  meter/sec
 ZDOT =      15862
596487                 ZDOT =        4806
785045

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19352573
04                 X    =        -5898664
26
 Y    =          16393
95  feet           Y    =            4996
87  meter
 Z    =       10490531
44                 Z    =         3197513
98
 XDOT =       8535
487992                 XDOT =        2601
616740
 YDOT =     -16464
361022  feet/sec       YDOT =       -5018
337240  meter/sec
 ZDOT =      15757
559782                 ZDOT =        4802
904222


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 29391U 06036A   06263
78276254  
00014500  00000-0  95600-4 0  9092
2 29391  51
6333  55
0198 0012737   3
4929 356
6322 15
75901506  1773


Satellite: SHUTTLE
Catalog Number: 29391
Epoch time:      06263
78276254   =   yrday
fracday
Element set:     909
Inclination:       51
6333  deg
RA of node:        55
0198  deg
Eccentricity:     
0012737     
Arg of perigee:     3
4929  deg
Mean anomaly:     356
6322  deg
Mean motion:   15
75901506  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             177
Checksum:              313


Coasting Arc #11 (Orbit 191)
---------------------------------------

Vector Time (GMT): 2006/264/17:30:16
382
Vector Time (MET): 012/02:15:21
410
Weight (LBS)     : 209888
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5304497
21                 A    =         6724404
42  meter
 Y    =        3383931
34  meter          E    =           
0017858
 Z    =       -2348100
34                 I    =           51
88498
 XDOT =      -1029
633924                 Wp   =           18
06542
 YDOT =       5367
458446  meter/sec      RA   =           49
55957  deg
 ZDOT =       5436
770995                 TA   =          315
55002
                                          MA   =          315
69319
                                          Ha   =            190
709  n
mi
                                          Hp   =            178
723

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17403206
06                 X    =         5277629
01
 Y    =       11102136
95  feet           Y    =         3443161
87  meter
 Z    =       -7703741
28                 Z    =        -2322396
49
 XDOT =      -3378
064055                 XDOT =       -1116
051741
 YDOT =      17609
771806  feet/sec       YDOT =        5355
448791  meter/sec
 ZDOT =      17837
175180                 ZDOT =        5431
558874

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13341664
45                 X    =        -4066539
32
 Y    =       15798805
69  feet           Y    =         4815475
98  meter
 Z    =       -7607521
54                 Z    =        -2318772
57
 XDOT =     -15832
150001                 XDOT =       -4825
639320
 YDOT =      -4833
828262  feet/sec       YDOT =       -1473
350854  meter/sec
 ZDOT =      17818
490285                 ZDOT =        5431
075839


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 29391U 06036A   06264
73395290  
00014500  00000-0  95600-4 0  9102
2 29391  51
6328  50
1207 0012942   6
8371 353
2967 15
75906899  1925


Satellite: SHUTTLE
Catalog Number: 29391
Epoch time:      06264
73395290   =   yrday
fracday
Element set:     910
Inclination:       51
6328  deg
RA of node:        50
1207  deg
Eccentricity:     
0012942     
Arg of perigee:     6
8371  deg
Mean anomaly:     353
2967  deg
Mean motion:   15
75906899  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             192
Checksum:              315


Coasting Arc #12 (Orbit 207)
---------------------------------------

Vector Time (GMT): 2006/265/17:35:15
511
Vector Time (MET): 013/02:20:20
539
Weight (LBS)     : 209888
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2950107
57                 A    =         6714602
31  meter
 Y    =       -2928402
44  meter          E    =           
0021558
 Z    =       -5288039
10                 I    =           51
83283
 XDOT =       5460
107201                 Wp   =           53
93400
 YDOT =       5416
820294  meter/sec      RA   =           44
42672  deg
 ZDOT =         58
965059                 TA   =          216
55101
                                          MA   =          216
69832
                                          Ha   =            190
752  n
mi
                                          Hp   =            178
511

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9678830
60                 X    =         3008357
09
 Y    =       -9607619
54  feet           Y    =        -2895051
77  meter
 Z    =      -17349209
65                 Z    =        -5273565
76
 XDOT =      17913
737536                 XDOT =        5398
778057
 YDOT =      17771
720125  feet/sec       YDOT =        5477
600022  meter/sec
 ZDOT =        193
454919                 ZDOT =          85
341178

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8631513
46                 X    =         2630885
30
 Y    =       10645997
45  feet           Y    =         3244900
02  meter
 Z    =      -17295690
33                 Z    =        -5271726
41
 XDOT =     -18622
582526                 XDOT =       -5676
163154
 YDOT =      15506
582357  feet/sec       YDOT =        4726
406302  meter/sec
 ZDOT =        292
451417                 ZDOT =          89
139192


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 29391U 06036A   06265
74853442  
00014500  00000-0  95600-4 0  9113
2 29391  51
6329  44
8941 0013003  10
8190 349
3252 15
75933610  2086


Satellite: SHUTTLE
Catalog Number: 29391
Epoch time:      06265
74853442   =   yrday
fracday
Element set:     911
Inclination:       51
6329  deg
RA of node:        44
8941  deg
Eccentricity:     
0013003     
Arg of perigee:    10
8190  deg
Mean anomaly:     349
3252  deg
Mean motion:   15
75933610  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             208
Checksum:              287

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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