Date: September 8th 2006

SHUTTLE TRAJECTORY DATA

Lift off time (UTC) : 2006/250/16:03:09 000 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


250/16:41:45 616 134 3 227 0 227 1
000/00:38:36 616 46 7 -0 1 157 1
000/00:02:31 231 -177 0 -7 2 123 7

250/18:58:14 001 -42 5 83 5 83 5
000/02:55:05 001 -29 2 0 0 171 4
000/00:00:56 378 65 7 -0 0 156 5

251/07:54:02 155 17 5 44 1 44 7
000/15:50:53 155 25 5 -1 8 182 2
000/00:04:58 742 -32 2 -7 0 171 6

251/19:14:49 704 -2 2 6 0 6 0
001/03:11:40 704 -3 4 0 0 182 2
000/00:00:26 463 4 4 -0 0 175 0

252/07:21:53 704 -5 2 11 6 11 6
001/15:18:44 704 -5 4 0 0 181 5
000/00:00:17 037 8 9 -0 0 181 1

252/08:53:26 615 -3 9 8 9 8 9
001/16:50:17 615 -4 1 -0 2 187 2
000/00:00:14 005 6 9 -0 2 181 8

252/10:10:20 088 -2 0 2 5 2 9
001/18:07:11 088 -0 3 0 2 188 6
000/00:00:12 953 2 2 1 5 181 9

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

Vector Time (GMT): 2006/250/16:13:38
000
Vector Time (MET): 000/00:10:29
000
Weight (LBS)     : 257857
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4667341
87                 A    =         6518751
71  meter
 Y    =         987061
56  meter          E    =           
0127683
 Z    =        4393614
08                 I    =           51
89084
 XDOT =       1403
575943                 Wp   =          352
27162
 YDOT =      -7036
603566  meter/sec      RA   =          121
80753  deg
 ZDOT =       3207
683063                 TA   =           67
15482
                                          MA   =           65
81148
                                          Ha   =            123
983  n
mi
                                          Hp   =             31
476

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15312801
41                 X    =        -4699375
58
 Y    =        3238390
94  feet           Y    =          934689
96  meter
 Z    =       14414744
36                 Z    =         4370862
52
 XDOT =       4604
907949                 XDOT =        1466
573728
 YDOT =     -23085
969704  feet/sec       YDOT =       -7020
555539  meter/sec
 ZDOT =      10523
894563                 ZDOT =        3214
655071

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7586564
36                 X    =         2312384
82
 Y    =      -13778396
70  feet           Y    =        -4199655
31  meter
 Z    =       14330169
00                 Z    =         4367835
51
 XDOT =      13526
647906                 XDOT =        4122
922282
 YDOT =      17953
004644  feet/sec       YDOT =        5472
075815  meter/sec
 ZDOT =      10548
839224                 ZDOT =        3215
286196


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          06250
72667426  
00014500  00000-0  95600-4 0  9004
2 99115  51
6326 122
3464 0057115 348
9980  10
9985 16
70585498    29


Satellite: SHUTTLE
Catalog Number: 99115
Epoch time:      06250
72667426   =   yrday
fracday
Element set:     900
Inclination:       51
6326  deg
RA of node:       122
3464  deg
Eccentricity:     
0057115     
Arg of perigee:   348
9980  deg
Mean anomaly:      10
9985  deg
Mean motion:   16
70585498  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:               2
Checksum:              316


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

Vector Time (GMT): 2006/250/16:43:01
231
Vector Time (MET): 000/00:39:52
231
Weight (LBS)     : 252146
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3416975
08                 A    =         6644159
50  meter
 Y    =       -5654839
88  meter          E    =           
0055362
 Z    =          77288
18                 I    =           51
92280
 XDOT =       4150
127675                 Wp   =          174
64433
 YDOT =       2420
023453  meter/sec      RA   =          121
66786  deg
 ZDOT =      -6130
127875                 TA   =            4
50426
                                          MA   =            4
45464
                                          Ha   =            157
069  n
mi
                                          Hp   =            123
749

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11210548
17                 X    =         3479578
88
 Y    =      -18552624
28  feet           Y    =        -5616279
33  meter
 Z    =         253570
16                 Z    =           94040
12
 XDOT =      13615
904447                 XDOT =        4152
536913
 YDOT =       7939
709490  feet/sec       YDOT =        2466
445513  meter/sec
 ZDOT =     -20111
968095                 ZDOT =       -6109
961106

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9334807
68                 X    =         2845249
38
 Y    =       19562786
45  feet           Y    =         5962737
31  meter
 Z    =         315131
08                 Z    =           96051
95
 XDOT =     -12752
317629                 XDOT =       -3886
906413
 YDOT =       6420
050411  feet/sec       YDOT =        1956
831365  meter/sec
 ZDOT =     -20036
525284                 ZDOT =       -6107
132906


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          06250
72786913  
00014500  00000-0  95600-4 0  9018
2 99115  51
6330 122
3566 0046389 184
7409 175
3337 16
05459610    21


Satellite: SHUTTLE
Catalog Number: 99115
Epoch time:      06250
72786913   =   yrday
fracday
Element set:     901
Inclination:       51
6330  deg
RA of node:       122
3566  deg
Eccentricity:     
0046389     
Arg of perigee:   184
7409  deg
Mean anomaly:     175
3337  deg
Mean motion:   16
05459610  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:               2
Checksum:              302


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

Vector Time (GMT): 2006/250/18:58:42
190
Vector Time (MET): 000/02:55:33
190
Weight (LBS)     : 250081
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3686247
42                 A    =         6687836
54  meter
 Y    =        5545600
44  meter          E    =           
0029035
 Z    =         362648
84                 I    =           51
92689
 XDOT =      -3795
997426                 Wp   =           16
16080
 YDOT =      -2926
547673  meter/sec      RA   =          121
16758  deg
 ZDOT =       6079
954905                 TA   =          347
80020
                                          MA   =          347
87036
                                          Ha   =            171
362  n
mi
                                          Hp   =            156
549

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12093987
61                 X    =        -3749746
79
 Y    =       18194227
18  feet           Y    =         5504023
77  meter
 Z    =        1189792
80                 Z    =          344586
61
 XDOT =     -12454
059796                 XDOT =       -3792
525248
 YDOT =      -9601
534359  feet/sec       YDOT =       -2968
976761  meter/sec
 ZDOT =      19947
358612                 ZDOT =        6061
522797

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18332781
21                 X    =        -5587831
71
 Y    =      -11889377
31  feet           Y    =        -3623882
21  meter
 Z    =        1123336
96                 Z    =          342393
11
 XDOT =       8589
008719                 XDOT =        2617
929858
 YDOT =     -11337
040980  feet/sec       YDOT =       -3455
530091  meter/sec
 ZDOT =      19878
301658                 ZDOT =        6058
906345


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          06250
85297804  
00014500  00000-0  95600-4 0  9029
2 99115  51
6361 121
6915 0019363 355
0229   5
0747 15
89700297    47


Satellite: SHUTTLE
Catalog Number: 99115
Epoch time:      06250
85297804   =   yrday
fracday
Element set:     902
Inclination:       51
6361  deg
RA of node:       121
6915  deg
Eccentricity:     
0019363     
Arg of perigee:   355
0229  deg
Mean anomaly:       5
0747  deg
Mean motion:   15
89700297  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:               4
Checksum:              299


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

Vector Time (GMT): 2006/251/07:56:31
526
Vector Time (MET): 000/15:53:22
526
Weight (LBS)     : 248918
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4733989
61                 A    =         6707204
06  meter
 Y    =       -3492084
62  meter          E    =           
0016666
 Z    =       -3198954
13                 I    =           51
91607
 XDOT =       1105
981351                 Wp   =          208
30895
 YDOT =       5921
165041  meter/sec      RA   =          118
36205  deg
 ZDOT =      -4831
282899                 TA   =            9
05980
                                          MA   =            9
02976
                                          Ha   =            182
155  n
mi
                                          Hp   =            171
645

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15531461
97                 X    =         4788226
57
 Y    =      -11456970
55  feet           Y    =        -3438843
54  meter
 Z    =      -10495256
34                 Z    =        -3175824
56
 XDOT =       3628
547738                 XDOT =        1063
157203
 YDOT =      19426
394490  feet/sec       YDOT =        5933
292907  meter/sec
 ZDOT =     -15850
665680                 ZDOT =       -4826
014575

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15237388
64                 X    =        -4644356
06
 Y    =      -11920587
08  feet           Y    =        -3633394
94  meter
 Z    =      -10409634
09                 Z    =        -3172856
47
 XDOT =      16834
766354                 XDOT =        5131
236785
 YDOT =      -7707
437592  feet/sec       YDOT =       -2349
226978  meter/sec
 ZDOT =     -15830
193087                 ZDOT =       -4825
042853


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          06251
35599757  
00014500  00000-0  95600-4 0  9038
2 99115  51
6325 119
0506 0018623 221
7213 138
2535 15
81246307   126


Satellite: SHUTTLE
Catalog Number: 99115
Epoch time:      06251
35599757   =   yrday
fracday
Element set:     903
Inclination:       51
6325  deg
RA of node:       119
0506  deg
Eccentricity:     
0018623     
Arg of perigee:   221
7213  deg
Mean anomaly:     138
2535  deg
Mean motion:   15
81246307  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:              12
Checksum:              287


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

Vector Time (GMT): 2006/251/19:15:02
935
Vector Time (MET): 001/03:11:53
935
Weight (LBS)     : 248746
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4090650
21                 A    =         6713154
27  meter
 Y    =        4964424
85  meter          E    =           
0004587
 Z    =        1927819
13                 I    =           51
93229
 XDOT =      -2748
922322                 Wp   =          155
90118
 YDOT =      -4461
087248  meter/sec      RA   =          115
91335  deg
 ZDOT =       5646
239650                 TA   =          225
48451
                                          MA   =          225
52200
                                          Ha   =            182
156  n
mi
                                          Hp   =            175
000

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13420768
40                 X    =        -4155224
03
 Y    =       16287483
11  feet           Y    =         4918320
04  meter
 Z    =        6324865
92                 Z    =         1907789
58
 XDOT =      -9018
774022                 XDOT =       -2726
261834
 YDOT =     -14636
113020  feet/sec       YDOT =       -4491
700054  meter/sec
 ZDOT =      18524
408302                 ZDOT =        5632
940848

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17552530
56                 X    =        -5350011
32
 Y    =      -11757412
51  feet           Y    =        -3583659
33  meter
 Z    =        6250998
42                 Z    =         1905304
32
 XDOT =      12792
437288                 XDOT =        3899
134885
 YDOT =      -9260
116302  feet/sec       YDOT =       -2822
483449  meter/sec
 ZDOT =      18474
244290                 ZDOT =        5630
949660


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          06251
86162763  
00014500  00000-0  95600-4 0  9048
2 99115  51
6330 116
4216 0014787 229
2970 130
6912 15
80145498   203


Satellite: SHUTTLE
Catalog Number: 99115
Epoch time:      06251
86162763   =   yrday
fracday
Element set:     904
Inclination:       51
6330  deg
RA of node:       116
4216  deg
Eccentricity:     
0014787     
Arg of perigee:   229
2970  deg
Mean anomaly:     130
6912  deg
Mean motion:   15
80145498  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:              20
Checksum:              294


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

Vector Time (GMT): 2006/252/07:22:02
222
Vector Time (MET): 001/15:18:53
222
Weight (LBS)     : 248460
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3559603
35                 A    =         6720148
44  meter
 Y    =        5522897
81  meter          E    =           
0007856
 Z    =        1384496
10                 I    =           51
93939
 XDOT =      -3412
734524                 Wp   =           22
25191
 YDOT =      -3668
649645  meter/sec      RA   =          113
30619  deg
 ZDOT =       5856
711752                 TA   =          352
92889
                                          MA   =          352
93996
                                          Ha   =            181
520  n
mi
                                          Hp   =            181
080

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11678488
69                 X    =        -3627822
23
 Y    =       18119743
48  feet           Y    =         5482711
04  meter
 Z    =        4542310
03                 Z    =         1367037
41
 XDOT =     -11196
635577                 XDOT =       -3399
908377
 YDOT =     -12036
252115  feet/sec       YDOT =       -3706
740550  meter/sec
 ZDOT =      19214
933569                 ZDOT =        5840
164142

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19570517
36                 X    =         5965093
69
 Y    =        9071180
02  feet           Y    =         2764895
67  meter
 Z    =        4478093
97                 Z    =         1364923
04
 XDOT =      -9687
181444                 XDOT =       -2952
652904
 YDOT =      11438
571165  feet/sec       YDOT =        3486
476491  meter/sec
 ZDOT =      19152
787230                 ZDOT =        5837
769548


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
36765995  
00014500  00000-0  95600-4 0  9051
2 99115  51
6315 113
8036 0009215 272
0186  87
9924 15
77949842   288


Satellite: SHUTTLE
Catalog Number: 99115
Epoch time:      06252
36765995   =   yrday
fracday
Element set:     905
Inclination:       51
6315  deg
RA of node:       113
8036  deg
Eccentricity:     
0009215     
Arg of perigee:   272
0186  deg
Mean anomaly:      87
9924  deg
Mean motion:   15
77949842  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:              28
Checksum:              332


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

Vector Time (GMT): 2006/252/08:53:33
617
Vector Time (MET): 001/16:50:24
617
Weight (LBS)     : 248242
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3594575
66                 A    =         6724769
35  meter
 Y    =        5470009
41  meter          E    =           
0014776
 Z    =        1499099
67                 I    =           51
94103
 XDOT =      -3342
448844                 Wp   =           20
28437
 YDOT =      -3792
846430  meter/sec      RA   =          112
98051  deg
 ZDOT =       5821
588139                 TA   =          356
18711
                                          MA   =          356
19835
                                          Ha   =            187
197  n
mi
                                          Hp   =            181
839

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11793227
23                 X    =        -3662757
26
 Y    =       17946225
11  feet           Y    =         5429431
78  meter
 Z    =        4918305
99                 Z    =         1481471
18
 XDOT =     -10966
039516                 XDOT =       -3328
068524
 YDOT =     -12443
721884  feet/sec       YDOT =       -3830
142679  meter/sec
 ZDOT =      19099
698618                 ZDOT =        5805
385753

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21469646
21                 X    =         6543948
16
 Y    =         913923
29  feet           Y    =          278563
82  meter
 Z    =        4853449
69                 Z    =         1479331
46
 XDOT =      -4916
378246                 XDOT =       -1498
512089
 YDOT =      14327
537403  feet/sec       YDOT =        4367
033401  meter/sec
 ZDOT =      19038
820065                 ZDOT =        5803
032356


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
43105877  
00014500  00000-0  95600-4 0  9067
2 99115  51
6330 113
4772 0010224 314
7678  45
2654 15
76272381   294


Satellite: SHUTTLE
Catalog Number: 99115
Epoch time:      06252
43105877   =   yrday
fracday
Element set:     906
Inclination:       51
6330  deg
RA of node:       113
4772  deg
Eccentricity:     
0010224     
Arg of perigee:   314
7678  deg
Mean anomaly:      45
2654  deg
Mean motion:   15
76272381  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:              29
Checksum:              294


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

Vector Time (GMT): 2006/252/10:10:26
565
Vector Time (MET): 001/18:07:17
565
Weight (LBS)     : 248157
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         506226
97                 A    =         6721884
48  meter
 Y    =        5753486
98  meter          E    =           
0009482
 Z    =       -3427044
48                 I    =           51
92835
 XDOT =      -5265
072541                 Wp   =          340
13014
 YDOT =       3213
110245  meter/sec      RA   =          112
66739  deg
 ZDOT =       4621
611779                 TA   =          339
46404
                                          MA   =          339
50213
                                          Ha   =            188
566  n
mi
                                          Hp   =            181
920

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1660849
63                 X    =          458501
03
 Y    =       18876269
62  feet           Y    =         5758880
77  meter
 Z    =      -11243584
24                 Z    =        -3424701
60
 XDOT =     -17273
860043                 XDOT =       -5323
061636
 YDOT =      10541
700278  feet/sec       YDOT =        3153
909418  meter/sec
 ZDOT =      15162
768303                 ZDOT =        4595
892942

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10757623
60                 X    =         3278923
67
 Y    =      -15606415
62  feet           Y    =        -4756835
48  meter
 Z    =      -11234032
62                 Z    =        -3424133
14
 XDOT =      18945
253823                 XDOT =        5774
513365
 YDOT =       2224
901082  feet/sec       YDOT =         678
149850  meter/sec
 ZDOT =      15067
461031                 ZDOT =        4592
562122


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
43105678  
00014500  00000-0  95600-4 0  9077
2 99115  51
6337 113
4779 0012262 317
8662  42
1559 15
75818755   299


Satellite: SHUTTLE
Catalog Number: 99115
Epoch time:      06252
43105678   =   yrday
fracday
Element set:     907
Inclination:       51
6337  deg
RA of node:       113
4779  deg
Eccentricity:     
0012262     
Arg of perigee:   317
8662  deg
Mean anomaly:      42
1559  deg
Mean motion:   15
75818755  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:              29
Checksum:              319


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

Vector Time (GMT): 2006/253/10:15:30
484
Vector Time (MET): 002/18:12:21
484
Weight (LBS)     : 248157
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4320074
87                 A    =         6715446
11  meter
 Y    =        -300538
89  meter          E    =           
0013755
 Z    =       -5140380
27                 I    =           51
91658
 XDOT =      -1190
693857                 Wp   =           26
30906
 YDOT =       7469
778015  meter/sec      RA   =          107
55716  deg
 ZDOT =      -1426
796073                 TA   =          230
00987
                                          MA   =          230
13071
                                          Ha   =            188
717  n
mi
                                          Hp   =            181
687

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14173473
98                 X    =         4348085
64
 Y    =        -986019
97  feet           Y    =         -252073
11  meter
 Z    =      -16864764
66                 Z    =        -5119325
17
 XDOT =      -3906
475908                 XDOT =       -1267
202289
 YDOT =      24507
145719  feet/sec       YDOT =        7456
035153  meter/sec
 ZDOT =      -4681
089479                 ZDOT =       -1432
766780

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11913008
27                 X    =        -3631084
92
 Y    =       -7910549
21  feet           Y    =        -2411135
40  meter
 Z    =      -16786403
20                 Z    =        -5116495
70
 XDOT =      17432
263888                 XDOT =        5313
354033
 YDOT =     -16199
800769  feet/sec       YDOT =       -4937
699274  meter/sec
 ZDOT =      -4702
257198                 ZDOT =       -1433
247994


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
44570642  
00014500  00000-0  95600-4 0  9087
2 99115  51
6334 108
2517 0012348 321
7414  38
2873 15
75875891   459


Satellite: SHUTTLE
Catalog Number: 99115
Epoch time:      06253
44570642   =   yrday
fracday
Element set:     908
Inclination:       51
6334  deg
RA of node:       108
2517  deg
Eccentricity:     
0012348     
Arg of perigee:   321
7414  deg
Mean anomaly:      38
2873  deg
Mean motion:   15
75875891  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:              45
Checksum:              309


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

Vector Time (GMT): 2006/254/10:20:06
181
Vector Time (MET): 003/18:16:57
181
Weight (LBS)     : 248157
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2221913
51                 A    =         6726425
43  meter
 Y    =       -6262344
34  meter          E    =           
0002602
 Z    =       -1053461
11                 I    =           51
96081
 XDOT =       4210
020582                 Wp   =          334
61307
 YDOT =       2494
330716  meter/sec      RA   =          102
40973  deg
 ZDOT =      -5940
394472                 TA   =          216
85446
                                          MA   =          216
87235
                                          Ha   =            188
824  n
mi
                                          Hp   =            181
524

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7289742
50                 X    =         2296892
34
 Y    =      -20545749
15  feet           Y    =        -6237078
48  meter
 Z    =       -3456237
24                 Z    =        -1042484
64
 XDOT =      13812
403485                 XDOT =        4210
673333
 YDOT =       8183
499724  feet/sec       YDOT =        2541
412950  meter/sec
 ZDOT =     -19489
483177                 ZDOT =       -5919
940525

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17859396
01                 X    =        -5443543
90
 Y    =       12513391
47  feet           Y    =         3814081
72  meter
 Z    =       -3416246
20                 Z    =        -1041271
84
 XDOT =      -5692
923996                 XDOT =       -1735
203234
 YDOT =     -13431
900883  feet/sec       YDOT =       -4094
043389  meter/sec
 ZDOT =     -19412
962514                 ZDOT =       -5917
070974


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
46033411  
00014500  00000-0  95600-4 0  9099
2 99115  51
6335 103
0257 0012282 324
7213  35
3137 15
75854449   616


Satellite: SHUTTLE
Catalog Number: 99115
Epoch time:      06254
46033411   =   yrday
fracday
Element set:     909
Inclination:       51
6335  deg
RA of node:       103
0257  deg
Eccentricity:     
0012282     
Arg of perigee:   324
7213  deg
Mean anomaly:      35
3137  deg
Mean motion:   15
75854449  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:              61
Checksum:              278


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

Vector Time (GMT): 2006/255/10:24:50
403
Vector Time (MET): 004/18:21:41
403
Weight (LBS)     : 248157
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2755697
61                 A    =         6718924
71  meter
 Y    =       -4459770
19  meter          E    =           
0013988
 Z    =        4208467
04                 I    =           51
94157
 XDOT =       3621
500091                 Wp   =           13
62250
 YDOT =      -5716
007787  meter/sec      RA   =           97
22819  deg
 ZDOT =      -3670
222304                 TA   =          113
71746
                                          MA   =          113
57064
                                          Ha   =            188
963  n
mi
                                          Hp   =            181
032

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9041002
65                 X    =        -2726067
16
 Y    =      -14631791
98  feet           Y    =        -4490420
22  meter
 Z    =       13807306
57                 Z    =         4195151
77
 XDOT =      11881
561979                 XDOT =        3702
977531
 YDOT =     -18753
306389  feet/sec       YDOT =       -5675
054637  meter/sec
 ZDOT =     -12041
411757                 ZDOT =       -3652
430967

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -391448
27                 X    =         -119313
43
 Y    =       17235424
19  feet           Y    =         5253357
29  meter
 Z    =       13757096
39                 Z    =         4193162
98
 XDOT =     -19013
568400                 XDOT =       -5795
335648
 YDOT =       9168
633945  feet/sec       YDOT =        2794
599626  meter/sec
 ZDOT =     -11975
953214                 ZDOT =       -3650
270540


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
47493549  
00014500  00000-0  95600-4 0  9105
2 99115  51
6336  97
7988 0012600 329
0242  31
0178 15
75969942   771


Satellite: SHUTTLE
Catalog Number: 99115
Epoch time:      06255
47493549   =   yrday
fracday
Element set:     910
Inclination:       51
6336  deg
RA of node:        97
7988  deg
Eccentricity:     
0012600     
Arg of perigee:   329
0242  deg
Mean anomaly:      31
0178  deg
Mean motion:   15
75969942  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:              77
Checksum:              329

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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