Date: September 9th 2006

SHUTTLE TRAJECTORY DATA

Lift off time (UTC) : 2006/252/15:14:56 000 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 0

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


252/15:53:30 893 136 9 221 7 221 8
000/00:38:34 893 22 3 -0 1 154 1
000/00:02:27 786 -173 0 -6 0 123 7

252/18:10:01 000 -46 7 83 4 83 4
000/02:55:05 000 -21 7 0 0 171 2
000/00:00:56 341 65 6 -0 0 153 7

253/07:05:49 269 21 8 48 8 49 2
000/15:50:53 269 27 2 -1 6 181 5
000/00:04:01 496 -34 7 -5 9 171 2

253/18:27:01 504 -2 5 6 0 6 0
001/03:12:05 504 -3 3 0 0 181 5
000/00:00:26 467 4 3 0 0 174 4

254/06:36:41 135 -5 1 12 5 12 5
001/15:21:45 135 -7 5 0 0 182 5
000/00:00:18 533 8 6 -0 0 180 8

254/08:08:15 448 -3 7 8 9 8 9
001/16:53:19 448 -5 3 -0 1 187 5
000/00:00:14 016 6 2 -0 3 181 3

254/09:25:08 911 -1 7 2 5 2 9
001/18:10:12 911 -0 7 0 1 188 9
000/00:00:12 942 2 3 1 5 181 4

Coasting Arc #1 (begining on orbit 1)
---------------------------------------

Vector Time (GMT): 2006/252/15:25:25
000
Vector Time (MET): 000/00:10:29
000
Weight (LBS)     : 257857
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4420985
54                 A    =         6518741
46  meter
 Y    =        1795751
38  meter          E    =           
0127675
 Z    =        4392309
05                 I    =           51
91530
 XDOT =        145
900014                 Wp   =          352
20423
 YDOT =      -7170
724269  meter/sec      RA   =          111
72760  deg
 ZDOT =       3214
401463                 TA   =           67
16100
                                          MA   =           65
81768
                                          Ha   =            123
974  n
mi
                                          Hp   =             31
470

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14504545
74                 X    =        -4462074
39
 Y    =        5891572
78  feet           Y    =         1746084
07  meter
 Z    =       14410462
76                 Z    =         4370731
93
 XDOT =        478
674586                 XDOT =         210
458185
 YDOT =     -23525
998257  feet/sec       YDOT =       -7168
731529  meter/sec
 ZDOT =      10545
936557                 ZDOT =        3215
267598

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7586354
79                 X    =         2312320
94
 Y    =      -13778299
08  feet           Y    =        -4199625
56  meter
 Z    =       14330373
67                 Z    =         4367897
89
 XDOT =      13527
432649                 XDOT =        4123
161472
 YDOT =      17952
784679  feet/sec       YDOT =        5472
008770  meter/sec
 ZDOT =      10548
131849                 ZDOT =        3215
070587


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 99115U          06252
69318985  
00014500  00000-0  95600-4 0  9005
2 99115  51
6321 112
2274 0057068 348
9940  11
0025 16
70601030    22


Satellite: SHUTTLE
Catalog Number: 99115
Epoch time:      06252
69318985   =   yrday
fracday
Element set:     900
Inclination:       51
6321  deg
RA of node:       112
2274  deg
Eccentricity:     
0057068     
Arg of perigee:   348
9940  deg
Mean anomaly:      11
0025  deg
Mean motion:   16
70601030  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:               2
Checksum:              270


Coasting Arc #2 (begining on orbit 1)
---------------------------------------

Vector Time (GMT): 2006/252/15:54:44
786
Vector Time (MET): 000/00:39:48
786
Weight (LBS)     : 252279
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2354894
88                 A    =         6641376
47  meter
 Y    =       -6172682
71  meter          E    =           
0051219
 Z    =         103987
85                 I    =           51
94715
 XDOT =       4520
393192                 Wp   =          174
73396
 YDOT =       1618
214498  meter/sec      RA   =          111
58793  deg
 ZDOT =      -6130
382535                 TA   =            4
12083
                                          MA   =            4
07882
                                          Ha   =            154
082  n
mi
                                          Hp   =            123
743

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7726033
06                 X    =         2423238
49
 Y    =      -20251583
70  feet           Y    =        -6145966
84  meter
 Z    =         341167
49                 Z    =          115594
42
 XDOT =      14830
686327                 XDOT =        4531
742479
 YDOT =       5309
102684  feet/sec       YDOT =        1668
827034  meter/sec
 ZDOT =     -20112
803591                 ZDOT =       -6108
394980

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9379252
60                 X    =         2858796
19
 Y    =       19540142
59  feet           Y    =         5955835
46  meter
 Z    =         383500
60                 Z    =          116890
98
 XDOT =     -12709
032812                 XDOT =       -3873
713201
 YDOT =       6503
832466  feet/sec       YDOT =        1982
368136  meter/sec
 ZDOT =     -20030
695774                 ZDOT =       -6105
356072


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 99115U          06252
69436307  
00014500  00000-0  95600-4 0  9015
2 99115  51
6324 112
2375 0042349 185
9994 174
0684 16
06469124    27


Satellite: SHUTTLE
Catalog Number: 99115
Epoch time:      06252
69436307   =   yrday
fracday
Element set:     901
Inclination:       51
6324  deg
RA of node:       112
2375  deg
Eccentricity:     
0042349     
Arg of perigee:   185
9994  deg
Mean anomaly:     174
0684  deg
Mean motion:   16
06469124  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:               2
Checksum:              305


Coasting Arc #3 (begining on orbit 3)
---------------------------------------

Vector Time (GMT): 2006/252/18:10:29
171
Vector Time (MET): 000/02:55:33
171
Weight (LBS)     : 250215
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2675001
91                 A    =         6684993
74  meter
 Y    =        6090396
74  meter          E    =           
0032877
 Z    =         389175
01                 I    =           51
95082
 XDOT =      -4234
205767                 Wp   =           14
05379
 YDOT =      -2253
191754  meter/sec      RA   =          111
08736  deg
 ZDOT =       6083
456420                 TA   =          350
19959
                                          MA   =          350
26356
                                          Ha   =            171
221  n
mi
                                          Hp   =            153
705

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8776252
97                 X    =        -2744797
29
 Y    =       19981616
59  feet           Y    =         6060093
17  meter
 Z    =        1276820
90                 Z    =          376009
84
 XDOT =     -13891
751203                 XDOT =       -4238
247978
 YDOT =      -7392
361396  feet/sec       YDOT =       -2300
563140  meter/sec
 ZDOT =      19958
846521                 ZDOT =        6062
876947

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18267494
95                 X    =        -5567932
46
 Y    =      -11945998
67  feet           Y    =        -3641140
40  meter
 Z    =        1228671
51                 Z    =          374499
07
 XDOT =       8720
940136                 XDOT =        2658
142553
 YDOT =     -11264
983754  feet/sec       YDOT =       -3433
567048  meter/sec
 ZDOT =      19881
890925                 ZDOT =        6060
000354


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 99115U          06252
81939306  
00014500  00000-0  95600-4 0  9027
2 99115  51
6356 111
5717 0023371 355
4991   4
5967 15
90714097    46


Satellite: SHUTTLE
Catalog Number: 99115
Epoch time:      06252
81939306   =   yrday
fracday
Element set:     902
Inclination:       51
6356  deg
RA of node:       111
5717  deg
Eccentricity:     
0023371     
Arg of perigee:   355
4991  deg
Mean anomaly:       4
5967  deg
Mean motion:   15
90714097  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:               4
Checksum:              306


Coasting Arc #4 (begining on orbit 11)
---------------------------------------

Vector Time (GMT): 2006/253/07:07:50
017
Vector Time (MET): 000/15:52:54
017
Weight (LBS)     : 248950
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4058581
62                 A    =         6706536
33  meter
 Y    =       -4237421
51  meter          E    =           
0017275
 Z    =       -3224140
55                 I    =           51
93765
 XDOT =       2094
325894                 Wp   =          222
49799
 YDOT =       5667
361325  meter/sec      RA   =          108
28024  deg
 ZDOT =      -4809
828144                 TA   =          355
21076
                                          MA   =          355
22727
                                          Ha   =            181
540  n
mi
                                          Hp   =            171
157

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13315556
51                 X    =         4121325
78
 Y    =      -13902301
54  feet           Y    =        -4191685
58  meter
 Z    =      -10577888
94                 Z    =        -3204271
19
 XDOT =       6871
147945                 XDOT =        2054
162423
 YDOT =      18593
705136  feet/sec       YDOT =        5690
556371  meter/sec
 ZDOT =     -15780
276062                 ZDOT =       -4799
751769

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15102145
97                 X    =        -4603134
09
 Y    =      -12002096
34  feet           Y    =        -3658238
96  meter
 Z    =      -10504505
61                 Z    =        -3201773
31
 XDOT =      16979
120142                 XDOT =        5175
235819
 YDOT =      -7580
315637  feet/sec       YDOT =       -2310
480206  meter/sec
 ZDOT =     -15741
944396                 ZDOT =       -4798
144652


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 99115U          06253
32209355  
00014500  00000-0  95600-4 0  9039
2 99115  51
6324 108
9289 0020225 233
3453 126
5855 15
81453931   124


Satellite: SHUTTLE
Catalog Number: 99115
Epoch time:      06253
32209355   =   yrday
fracday
Element set:     903
Inclination:       51
6324  deg
RA of node:       108
9289  deg
Eccentricity:     
0020225     
Arg of perigee:   233
3453  deg
Mean anomaly:     126
5855  deg
Mean motion:   15
81453931  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:              12
Checksum:              286


Coasting Arc #5 (begining on orbit 19)
---------------------------------------

Vector Time (GMT): 2006/253/18:27:14
738
Vector Time (MET): 001/03:12:18
738
Weight (LBS)     : 248778
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3375769
74                 A    =         6711881
45  meter
 Y    =        5332966
59  meter          E    =           
0003832
 Z    =        2290697
17                 I    =           51
94986
 XDOT =      -3206
370828                 Wp   =          198
99413
 YDOT =      -4378
435156  meter/sec      RA   =          105
83073  deg
 ZDOT =       5467
232003                 TA   =          186
67889
                                          MA   =          186
68400
                                          Ha   =            181
454  n
mi
                                          Hp   =            174
389

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11075360
03                 X    =        -3446280
68
 Y    =       17496609
55  feet           Y    =         5294822
73  meter
 Z    =        7515410
66                 Z    =         2274126
03
 XDOT =     -10519
589332                 XDOT =       -3183
731269
 YDOT =     -14364
944736  feet/sec       YDOT =       -4414
163707  meter/sec
 ZDOT =      17937
112872                 ZDOT =        5451
710562

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16620857
33                 X    =        -5066037
31
 Y    =      -12387673
35  feet           Y    =        -3775762
84  meter
 Z    =        7454461
33                 Z    =         2272119
81
 XDOT =      14212
094176                 XDOT =        4331
846305
 YDOT =      -8307
964922  feet/sec       YDOT =       -2532
267708  meter/sec
 ZDOT =      17878
691364                 ZDOT =        5449
425128


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 99115U          06253
82765735  
00014500  00000-0  95600-4 0  9044
2 99115  51
6331 106
2993 0016625 241
8410 118
1077 15
80358346   206


Satellite: SHUTTLE
Catalog Number: 99115
Epoch time:      06253
82765735   =   yrday
fracday
Element set:     904
Inclination:       51
6331  deg
RA of node:       106
2993  deg
Eccentricity:     
0016625     
Arg of perigee:   241
8410  deg
Mean anomaly:     118
1077  deg
Mean motion:   15
80358346  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:              20
Checksum:              293


Coasting Arc #6 (begining on orbit 27)
---------------------------------------

Vector Time (GMT): 2006/254/06:36:50
402
Vector Time (MET): 001/15:21:54
402
Weight (LBS)     : 248472
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3350038
10                 A    =         6717778
05  meter
 Y    =        5177934
90  meter          E    =           
0005895
 Z    =        2653643
57                 I    =           51
94966
 XDOT =      -3114
892272                 Wp   =           35
53021
 YDOT =      -4706
062617  meter/sec      RA   =          103
22101  deg
 ZDOT =       5249
313749                 TA   =          354
59718
                                          MA   =          354
60354
                                          Ha   =            182
458  n
mi
                                          Hp   =            180
762

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10990938
66                 X    =        -3420580
52
 Y    =       16987975
40  feet           Y    =         5140078
60  meter
 Z    =        8706179
68                 Z    =         2637197
41
 XDOT =     -10219
462836                 XDOT =       -3087
537348
 YDOT =     -15439
837983  feet/sec       YDOT =       -4740
741922  meter/sec
 ZDOT =      17222
157968                 ZDOT =        5234
248103

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16719251
14                 X    =         5096027
75
 Y    =       11441532
25  feet           Y    =         3487379
03  meter
 Z    =        8645668
66                 Z    =         2635199
81
 XDOT =     -14847
760574                 XDOT =       -4525
597423
 YDOT =       8723
155842  feet/sec       YDOT =        2658
817901  meter/sec
 ZDOT =      17165
389743                 ZDOT =        5232
010794


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 99115U          06254
33363069  
00014500  00000-0  95600-4 0  9056
2 99115  51
6319 103
6810 0010187 280
8234  79
1784 15
78001970   289


Satellite: SHUTTLE
Catalog Number: 99115
Epoch time:      06254
33363069   =   yrday
fracday
Element set:     905
Inclination:       51
6319  deg
RA of node:       103
6810  deg
Eccentricity:     
0010187     
Arg of perigee:   280
8234  deg
Mean anomaly:      79
1784  deg
Mean motion:   15
78001970  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:              28
Checksum:              298


Coasting Arc #7 (begining on orbit 28)
---------------------------------------

Vector Time (GMT): 2006/254/08:08:22
456
Vector Time (MET): 001/16:53:26
456
Weight (LBS)     : 248254
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3383857
33                 A    =         6722279
49  meter
 Y    =        5099468
15  meter          E    =           
0012653
 Z    =        2760391
54                 I    =           51
95042
 XDOT =      -3052
185536                 Wp   =           33
43299
 YDOT =      -4828
747863  meter/sec      RA   =          102
89492  deg
 ZDOT =       5178
123982                 TA   =          358
04118
                                          MA   =          358
04613
                                          Ha   =            187
480  n
mi
                                          Hp   =            181
327

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11101894
13                 X    =        -3454038
38
 Y    =       16730538
54  feet           Y    =         5061235
68  meter
 Z    =        9056402
68                 Z    =         2743781
98
 XDOT =     -10013
732074                 XDOT =       -3023
117561
 YDOT =     -15842
348631  feet/sec       YDOT =       -4862
716380  meter/sec
 ZDOT =      16988
595741                 ZDOT =        5163
367124

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19659064
08                 X    =         5992082
73
 Y    =        4217546
09  feet           Y    =         1285508
05  meter
 Z    =        8995271
38                 Z    =         2741758
72
 XDOT =     -10707
880755                 XDOT =       -3263
762054
 YDOT =      13791
496722  feet/sec       YDOT =        4203
648201  meter/sec
 ZDOT =      16932
960380                 ZDOT =        5161
166324


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 99115U          06254
39702786  
00014500  00000-0  95600-4 0  9066
2 99115  51
6331 103
3546 0010305 321
6398  38
4033 15
76328145   293


Satellite: SHUTTLE
Catalog Number: 99115
Epoch time:      06254
39702786   =   yrday
fracday
Element set:     906
Inclination:       51
6331  deg
RA of node:       103
3546  deg
Eccentricity:     
0010305     
Arg of perigee:   321
6398  deg
Mean anomaly:      38
4033  deg
Mean motion:   15
76328145  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:              29
Checksum:              292


Coasting Arc #8 (begining on orbit 28)
---------------------------------------

Vector Time (GMT): 2006/254/09:25:15
382
Vector Time (MET): 001/18:10:19
382
Weight (LBS)     : 248169
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         412133
14                 A    =         6724595
06  meter
 Y    =        6306623
62  meter          E    =           
0014678
 Z    =       -2269035
57                 I    =           51
95523
 XDOT =      -4909
446942                 Wp   =          349
33637
 YDOT =       2291
367400  meter/sec      RA   =          102
57796  deg
 ZDOT =       5485
484752                 TA   =          345
25525
                                          MA   =          345
29801
                                          Ha   =            188
873  n
mi
                                          Hp   =            181
359

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1352142
83                 X    =          352603
63
 Y    =       20691022
38  feet           Y    =         6310899
40  meter
 Z    =       -7444342
41                 Z    =        -2267178
22
 XDOT =     -16107
109391                 XDOT =       -4961
352156
 YDOT =       7517
609580  feet/sec       YDOT =        2236
177218  meter/sec
 ZDOT =      17996
997217                 ZDOT =        5461
508311

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14739992
99                 X    =         4492749
86
 Y    =      -14587511
28  feet           Y    =        -4446273
44  meter
 Z    =       -7436534
99                 Z    =        -2266655
87
 XDOT =      15222
699509                 XDOT =        4639
878810
 YDOT =       6266
774792  feet/sec       YDOT =        1910
112957  meter/sec
 ZDOT =      17908
035173                 ZDOT =        5458
369121


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 99115U          06254
39702620  
00014500  00000-0  95600-4 0  9074
2 99115  51
6341 103
3549 0012227 325
9976  34
0403 15
75877614   293


Satellite: SHUTTLE
Catalog Number: 99115
Epoch time:      06254
39702620   =   yrday
fracday
Element set:     907
Inclination:       51
6341  deg
RA of node:       103
3549  deg
Eccentricity:     
0012227     
Arg of perigee:   325
9976  deg
Mean anomaly:      34
0403  deg
Mean motion:   15
75877614  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:              29
Checksum:              300


Coasting Arc #9 (begining on orbit 44)
---------------------------------------

Vector Time (GMT): 2006/255/09:30:16
736
Vector Time (MET): 002/18:15:20
736
Weight (LBS)     : 248169
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4087985
79                 A    =         6714618
60  meter
 Y    =         691412
34  meter          E    =           
0013616
 Z    =       -5289039
98                 I    =           51
92692
 XDOT =      -1111
762613                 Wp   =           40
51908
 YDOT =       7616
013049  meter/sec      RA   =           97
45008  deg
 ZDOT =        146
638264                 TA   =          230
80694
                                          MA   =          230
92794
                                          Ha   =            189
036  n
mi
                                          Hp   =            181
125

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13412026
88                 X    =         4105643
90
 Y    =        2268413
20  feet           Y    =          737225
15  meter
 Z    =      -17352493
39                 Z    =        -5269137
51
 XDOT =      -3647
515135                 XDOT =       -1197
555638
 YDOT =      24986
919452  feet/sec       YDOT =        7603
101013  meter/sec
 ZDOT =        481
096668                 ZDOT =         141
028819

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7571814
69                 X    =        -2307889
12
 Y    =      -11413409
46  feet           Y    =        -3478807
20  meter
 Z    =      -17278278
18                 Z    =        -5266419
19
 XDOT =      19907
548799                 XDOT =        6067
820874
 YDOT =     -13853
712334  feet/sec       YDOT =       -4222
611519  meter/sec
 ZDOT =        461
270545                 ZDOT =         140
595262


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 99115U          06255
41164195  
00014500  00000-0  95600-4 0  9088
2 99115  51
6341  98
1287 0012323 329
7310  30
3141 15
75926605   455


Satellite: SHUTTLE
Catalog Number: 99115
Epoch time:      06255
41164195   =   yrday
fracday
Element set:     908
Inclination:       51
6341  deg
RA of node:        98
1287  deg
Eccentricity:     
0012323     
Arg of perigee:   329
7310  deg
Mean anomaly:      30
3141  deg
Mean motion:   15
75926605  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:              45
Checksum:              286


Coasting Arc #10 (begining on orbit 60)
---------------------------------------

Vector Time (GMT): 2006/256/09:35:00
396
Vector Time (MET): 003/18:20:04
396
Weight (LBS)     : 248169
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2134879
37                 A    =         6724198
87  meter
 Y    =       -5903469
30  meter          E    =           
0007348
 Z    =       -2420139
36                 I    =           51
96165
 XDOT =       4070
786707                 Wp   =          347
16167
 YDOT =       3685
986247  meter/sec      RA   =           92
32693  deg
 ZDOT =      -5390
183563                 TA   =          220
01404
                                          MA   =          220
06820
                                          Ha   =            189
125  n
mi
                                          Hp   =            180
946

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7004197
42                 X    =         2212490
77
 Y    =      -19368337
59  feet           Y    =        -5879161
93  meter
 Z    =       -7940089
75                 Z    =        -2409579
59
 XDOT =      13355
599431                 XDOT =        4055
451623
 YDOT =      12093
130732  feet/sec       YDOT =        3731
422338  meter/sec
 ZDOT =     -17684
329274                 ZDOT =       -5370
444799

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18638424
75                 X    =        -5680991
86
 Y    =        8798323
45  feet           Y    =         2681728
99  meter
 Z    =       -7901578
02                 Z    =        -2408400
98
 XDOT =       -403
485869                 XDOT =        -122
982493
 YDOT =     -16700
109432  feet/sec       YDOT =       -5090
193355  meter/sec
 ZDOT =     -17610
305348                 ZDOT =       -5367
621070


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 99115U          06256
42623490  
00014500  00000-0  95600-4 0  9099
2 99115  51
6342  92
9028 0012335 332
7277  27
3238 15
75916913   612


Satellite: SHUTTLE
Catalog Number: 99115
Epoch time:      06256
42623490   =   yrday
fracday
Element set:     909
Inclination:       51
6342  deg
RA of node:        92
9028  deg
Eccentricity:     
0012335     
Arg of perigee:   332
7277  deg
Mean anomaly:      27
3238  deg
Mean motion:   15
75916913  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:              61
Checksum:              304


Coasting Arc #11 (begining on orbit 76)
---------------------------------------

Vector Time (GMT): 2006/257/09:39:33
466
Vector Time (MET): 004/18:24:37
466
Weight (LBS)     : 248169
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2784225
81                 A    =         6721988
47  meter
 Y    =       -5204984
54  meter          E    =           
0013527
 Z    =        3221043
48                 I    =           51
95510
 XDOT =       3522
666868                 Wp   =           36
43047
 YDOT =      -4872
044326  meter/sec      RA   =           87
13540  deg
 ZDOT =      -4807
050560                 TA   =          106
10762
                                          MA   =          105
95865
                                          Ha   =            189
261  n
mi
                                          Hp   =            180
469

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9134599
11                 X    =        -2741463
29
 Y    =      -17076720
92  feet           Y    =        -5235880
25  meter
 Z    =       10567727
95                 Z    =         3207621
48
 XDOT =      11557
305997                 XDOT =        3600
236739
 YDOT =     -15984
397395  feet/sec       YDOT =       -4832
218125  meter/sec
 ZDOT =     -15771
163255                 ZDOT =       -4789
749083

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4794756
38                 X    =        -1461441
74
 Y    =       18791879
73  feet           Y    =         5727764
94  meter
 Z    =       10517021
43                 Z    =         3205588
13
 XDOT =     -18020
712109                 XDOT =       -5492
713051
 YDOT =       4231
317441  feet/sec       YDOT =        1289
705556  meter/sec
 ZDOT =     -15707
390178                 ZDOT =       -4787
612526


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 99115U          06257
44080270  
00014500  00000-0  95600-4 0  9107
2 99115  51
6344  87
6761 0012561 337
3405  22
7203 15
76011043   773


Satellite: SHUTTLE
Catalog Number: 99115
Epoch time:      06257
44080270   =   yrday
fracday
Element set:     910
Inclination:       51
6344  deg
RA of node:        87
6761  deg
Eccentricity:     
0012561     
Arg of perigee:   337
3405  deg
Mean anomaly:      22
7203  deg
Mean motion:   15
76011043  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:              77
Checksum:              273

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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