Date: November 17th 2008

SHUTTLE TRAJECTORY DATA

Lift off time (UTC) : 2008/320/00:55:39 000 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 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


320/01:06:52 546 0 0 0 0 0 0
000/00:11:13 546 0 0 0 0 124 3
000/00:00:00 000 0 0 0 0 31 9

320/01:34:32 283 -43 5 97 4 97 4
000/00:38:53 283 -43 0 -0 1 124 3
000/00:01:06 366 -75 8 0 2 85 1

320/04:30:55 000 -29 4 63 5 63 5
000/03:35:16 000 -26 9 0 0 123 8
000/00:00:43 828 -49 4 -0 0 119 9

320/17:57:10 595 -4 1 7 0 7 6
000/17:01:31 595 -3 5 -0 8 123 9
000/00:10:31 355 -5 4 -3 0 122 4

321/02:46:33 346 -1 3 3 0 3 0
001/01:50:54 346 -1 3 -0 0 125 9
000/00:00:13 433 -2 3 0 0 123 2

321/17:09:33 703 -56 8 122 7 122 7
001/16:13:54 703 102 0 0 0 192 1
000/00:01:21 430 37 4 0 1 124 8

321/17:55:12 396 46 3 95 7 95 7
001/16:59:33 396 -79 3 0 0 192 3
000/00:01:03 457 -26 9 0 1 179 0

321/19:26:54 966 4 4 8 9 8 9
001/18:31:15 966 -7 4 0 1 192 4
000/00:00:13 932 -2 5 -0 1 184 2

321/20:43:48 500 0 4 2 5 3 0
001/19:48:09 500 -2 4 -0 0 192 4
000/00:00:13 001 -1 6 1 6 185 7

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

Vector Time (GMT): 2008/320/01:06:07
160
Vector Time (MET): 000/00:10:28
160
Weight (LBS)     : 256958
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4758205
39                 A    =         6519789
10  meter
 Y    =         758457
46  meter          E    =           
0127678
 Z    =        4341247
31                 I    =           51
43172
 XDOT =      -3796
725320                 Wp   =          352
51195
 YDOT =       6073
728152  meter/sec      RA   =          323
13096  deg
 ZDOT =       3236
895759                 TA   =           66
37211
                                          MA   =           65
03684
                                          Ha   =            124
349  n
mi
                                          Hp   =             31
933

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15610910
08                 X    =         4728280
98
 Y    =        2488377
49  feet           Y    =          811498
60  meter
 Z    =       14242937
37                 Z    =         4364290
71
 XDOT =     -12456
447899                 XDOT =       -3880
085235
 YDOT =      19926
929631  feet/sec       YDOT =        6030
804479  meter/sec
 ZDOT =      10619
736741                 ZDOT =        3218
249037

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7584384
28                 X    =         2311720
33
 Y    =      -13777368
58  feet           Y    =        -4199341
94  meter
 Z    =       14332307
25                 Z    =         4368487
25
 XDOT =      13527
381577                 XDOT =        4123
145905
 YDOT =      17956
027882  feet/sec       YDOT =        5472
997298  meter/sec
 ZDOT =      10547
878429                 ZDOT =        3214
993345


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 00126U          08320
09487515  
00020000  00000-0  70000-3 0  9005
2 00126  51
6395 323
3439 0350483 169
7501 191
1173 17
96085154    20


Satellite: SHUTTLE
Catalog Number: 00126
Epoch time:      08320
09487515   =   yrday
fracday
Element set:     900
Inclination:       51
6395  deg
RA of node:       323
3439  deg
Eccentricity:     
0350483     
Arg of perigee:   169
7501  deg
Mean anomaly:     191
1173  deg
Mean motion:   17
96085154  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:               2
Checksum:              262


Coasting Arc #2 (Orbit 1)
---------------------------------------

Vector Time (GMT): 2008/320/01:06:52
546
Vector Time (MET): 000/00:11:13
546
Weight (LBS)     : 256958
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4578835
07                 A    =         6519158
65  meter
 Y    =        1032842
10  meter          E    =           
0127644
 Z    =        4481548
09                 I    =           51
42965
 XDOT =      -4105
438132                 Wp   =          352
05172
 YDOT =       6014
484561  meter/sec      RA   =          323
12630  deg
 ZDOT =       2944
246052                 TA   =           69
98452
                                          MA   =           68
61469
                                          Ha   =            124
325  n
mi
                                          Hp   =             31
910

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15022424
77                 X    =         4545174
20
 Y    =        3388589
56  feet           Y    =         1083856
51  meter
 Z    =       14703241
76                 Z    =         4503711
05
 XDOT =     -13469
285209                 XDOT =       -4186
690953
 YDOT =      19732
560895  feet/sec       YDOT =        5968
120502  meter/sec
 ZDOT =       9659
599908                 ZDOT =        2924
104673

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8189426
76                 X    =         2496137
28
 Y    =      -12944243
06  feet           Y    =        -3945405
28  meter
 Z    =       14789217
84                 Z    =         4507753
60
 XDOT =      13129
239429                 XDOT =        4001
792178
 YDOT =      18748
005881  feet/sec       YDOT =        5714
392192  meter/sec
 ZDOT =       9581
944135                 ZDOT =        2920
576572


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 00126U          08320
09490780  
00020000  00000-0  70000-3 0  9014
2 00126  51
6395 323
3441 0347446 169
7174 191
1457 17
95107691    29


Satellite: SHUTTLE
Catalog Number: 00126
Epoch time:      08320
09490780   =   yrday
fracday
Element set:     901
Inclination:       51
6395  deg
RA of node:       323
3441  deg
Eccentricity:     
0347446     
Arg of perigee:   169
7174  deg
Mean anomaly:     191
1457  deg
Mean motion:   17
95107691  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:               2
Checksum:              270


Coasting Arc #3 (Orbit 1)
---------------------------------------

Vector Time (GMT): 2008/320/01:35:05
466
Vector Time (MET): 000/00:39:26
466
Weight (LBS)     : 254491
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5135273
61                 A    =         6577926
50  meter
 Y    =        4149723
33  meter          E    =           
0046479
 Z    =         279326
84                 I    =           51
46263
 XDOT =      -3232
664957                 Wp   =          349
93300
 YDOT =      -3600
015938  meter/sec      RA   =          322
99004  deg
 ZDOT =      -6052
266698                 TA   =          186
96930
                                          MA   =          187
03415
                                          Ha   =            124
344  n
mi
                                          Hp   =             85
050

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16848010
52                 X    =        -5182651
77
 Y    =       13614577
85  feet           Y    =         4092032
79  meter
 Z    =         916426
63                 Z    =          254264
43
 XDOT =     -10605
856159                 XDOT =       -3162
767117
 YDOT =     -11811
075913  feet/sec       YDOT =       -3635
773884  meter/sec
 ZDOT =     -19856
518038                 ZDOT =       -6067
802081

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9655853
22                 X    =         2943104
06
 Y    =       19394453
66  feet           Y    =         5911429
47  meter
 Z    =         819568
33                 Z    =          249804
43
 XDOT =     -12383
203140                 XDOT =       -3774
400317
 YDOT =       6990
732675  feet/sec       YDOT =        2130
775319  meter/sec
 ZDOT =     -19916
981720                 ZDOT =       -6070
696028


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 00126U          08320
09713556  
00020000  00000-0  70000-3 0  9024
2 00126  51
6395 323
3649 0056664 342
3971  17
5256 16
30124981    29


Satellite: SHUTTLE
Catalog Number: 00126
Epoch time:      08320
09713556   =   yrday
fracday
Element set:     902
Inclination:       51
6395  deg
RA of node:       323
3649  deg
Eccentricity:     
0056664     
Arg of perigee:   342
3971  deg
Mean anomaly:      17
5256  deg
Mean motion:   16
30124981  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:               2
Checksum:              260


Coasting Arc #4 (Orbit 3)
---------------------------------------

Vector Time (GMT): 2008/320/04:31:16
914
Vector Time (MET): 000/03:35:37
914
Weight (LBS)     : 252896
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5005854
15                 A    =         6610332
88  meter
 Y    =        4292405
75  meter          E    =           
0004571
 Z    =         421483
72                 I    =           51
46270
 XDOT =      -3449
550244                 Wp   =          202
50832
 YDOT =      -3430
710781  meter/sec      RA   =          322
30587  deg
 ZDOT =      -6056
361771                 TA   =          332
81412
                                          MA   =          332
83804
                                          Ha   =            123
829  n
mi
                                          Hp   =            119
939

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16423406
00                 X    =        -5055528
02
 Y    =       14082696
02  feet           Y    =         4236149
60  meter
 Z    =        1382820
60                 Z    =          397044
52
 XDOT =     -11317
422062                 XDOT =       -3381
509615
 YDOT =     -11255
612797  feet/sec       YDOT =       -3468
904439  meter/sec
 ZDOT =     -19869
953318                 ZDOT =       -6072
955291

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20616096
42                 X    =         6283786
19
 Y    =        6578709
01  feet           Y    =         2005190
51  meter
 Z    =        1288386
87                 Z    =          392700
32
 XDOT =      -3209
150387                 XDOT =        -978
149038
 YDOT =      13943
187661  feet/sec       YDOT =        4249
883599  meter/sec
 ZDOT =     -19934
507264                 ZDOT =       -6076
037814


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 00126U          08320
22001256  
00020000  00000-0  70000-3 0  9037
2 00126  51
6431 322
6843 0012609 291
3546  68
6295 16
17854369    47


Satellite: SHUTTLE
Catalog Number: 00126
Epoch time:      08320
22001256   =   yrday
fracday
Element set:     903
Inclination:       51
6431  deg
RA of node:       322
6843  deg
Eccentricity:     
0012609     
Arg of perigee:   291
3546  deg
Mean anomaly:      68
6295  deg
Mean motion:   16
17854369  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:               4
Checksum:              251


Coasting Arc #5 (Orbit 12)
---------------------------------------

Vector Time (GMT): 2008/320/18:02:26
272
Vector Time (MET): 000/17:06:47
272
Weight (LBS)     : 252671
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5592061
16                 A    =         6609380
97  meter
 Y    =        1442195
61  meter          E    =           
0006403
 Z    =       -3208088
36                 I    =           51
43221
 XDOT =       1180
099274                 Wp   =          261
25641
 YDOT =      -6026
668742  meter/sec      RA   =          319
24650  deg
 ZDOT =      -4759
369961                 TA   =          317
13934
                                          MA   =          317
18923
                                          Ha   =            123
920  n
mi
                                          Hp   =            122
383

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18346657
35                 X    =        -5592187
75
 Y    =        4731612
91  feet           Y    =         1379661
66  meter
 Z    =      -10525224
28                 Z    =        -3235255
32
 XDOT =       3871
716779                 XDOT =        1270
523426
 YDOT =     -19772
535242  feet/sec       YDOT =       -6012
965988  meter/sec
 ZDOT =     -15614
730843                 ZDOT =       -4753
418044

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17698245
27                 X    =        -5394425
16
 Y    =       -6598059
62  feet           Y    =        -2011088
57  meter
 Z    =      -10630431
15                 Z    =        -3240155
42
 XDOT =      14093
513067                 XDOT =        4295
702783
 YDOT =     -12646
063096  feet/sec       YDOT =       -3854
520032  meter/sec
 ZDOT =     -15592
074337                 ZDOT =       -4752
464258


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 00126U          08320
77595007  
00020000  00000-0  70000-3 0  9040
2 00126  51
6425 319
6438 0010897 266
6983  93
2956 16
16437751   132


Satellite: SHUTTLE
Catalog Number: 00126
Epoch time:      08320
77595007   =   yrday
fracday
Element set:     904
Inclination:       51
6425  deg
RA of node:       319
6438  deg
Eccentricity:     
0010897     
Arg of perigee:   266
6983  deg
Mean anomaly:      93
2956  deg
Mean motion:   16
16437751  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              13
Checksum:              289


Coasting Arc #6 (Orbit 18)
---------------------------------------

Vector Time (GMT): 2008/321/02:46:40
062
Vector Time (MET): 001/01:51:01
062
Weight (LBS)     : 252584
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4768231
11                 A    =         6615325
86  meter
 Y    =        4571512
64  meter          E    =           
0012324
 Z    =         146190
96                 I    =           51
43725
 XDOT =      -3449
590912                 Wp   =          187
60457
 YDOT =      -3405
991460  meter/sec      RA   =          317
21757  deg
 ZDOT =      -6074
573290                 TA   =          350
77394
                                          MA   =          350
79657
                                          Ha   =            125
923  n
mi
                                          Hp   =            123
171

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15643802
86                 X    =        -4819706
30
 Y    =       14998401
06  feet           Y    =         4517903
70  meter
 Z    =         479629
12                 Z    =          122901
98
 XDOT =     -11317
555484                 XDOT =       -3381
738423
 YDOT =     -11174
512663  feet/sec       YDOT =       -3444
186622  meter/sec
 ZDOT =     -19929
702395                 ZDOT =       -6091
167350

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16664294
26                 X    =         5079276
89
 Y    =       13858575
03  feet           Y    =         4224093
67  meter
 Z    =         389667
96                 Z    =          118770
79
 XDOT =      -8832
030575                 XDOT =       -2692
002919
 YDOT =      11174
424344  feet/sec       YDOT =        3405
964540  meter/sec
 ZDOT =     -19994
261727                 ZDOT =       -6094
250974


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 00126U          08321
14688114  
00020000  00000-0  70000-3 0  9055
2 00126  51
6397 317
6111 0011208 253
1648 106
8309 16
16034984   192


Satellite: SHUTTLE
Catalog Number: 00126
Epoch time:      08321
14688114   =   yrday
fracday
Element set:     905
Inclination:       51
6397  deg
RA of node:       317
6111  deg
Eccentricity:     
0011208     
Arg of perigee:   253
1648  deg
Mean anomaly:     106
8309  deg
Mean motion:   16
16034984  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              19
Checksum:              254


Coasting Arc #7 (Orbit 28)
---------------------------------------

Vector Time (GMT): 2008/321/17:10:14
418
Vector Time (MET): 001/16:14:35
418
Weight (LBS)     : 249533
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4375415
32                 A    =         6668395
17  meter
 Y    =        1035590
32  meter          E    =           
0088803
 Z    =        4844025
77                 I    =           51
38850
 XDOT =      -3862
942452                 Wp   =           68
97414
 YDOT =       6438
511215  meter/sec      RA   =          313
95665  deg
 ZDOT =       2113
979177                 TA   =             
73889
                                          MA   =             
72585
                                          Ha   =            192
085  n
mi
                                          Hp   =            124
751

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14355037
12                 X    =         4339978
21
 Y    =        3397606
02  feet           Y    =         1084320
02  meter
 Z    =       15892472
99                 Z    =         4865195
92
 XDOT =     -12673
695710                 XDOT =       -3944
921319
 YDOT =      21123
724459  feet/sec       YDOT =        6394
854940  meter/sec
 ZDOT =       6935
627222                 ZDOT =        2095
014346

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7231047
43                 X    =         2204023
26
 Y    =       12755597
22  feet           Y    =         3887906
03  meter
 Z    =       15974611
35                 Z    =         4869061
54
 XDOT =     -23193
944686                 XDOT =       -7069
514340
 YDOT =       4559
005195  feet/sec       YDOT =        1389
584784  meter/sec
 ZDOT =       6862
556277                 ZDOT =        2091
707153


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 00126U          08321
76616429  
00020000  00000-0  70000-3 0  9064
2 00126  51
6412 314
2443 0085412  66
1041 294
9052 15
92832385   297


Satellite: SHUTTLE
Catalog Number: 00126
Epoch time:      08321
76616429   =   yrday
fracday
Element set:     906
Inclination:       51
6412  deg
RA of node:       314
2443  deg
Eccentricity:     
0085412     
Arg of perigee:    66
1041  deg
Mean anomaly:     294
9052  deg
Mean motion:   15
92832385  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              29
Checksum:              258


Coasting Arc #8 (Orbit 28)
---------------------------------------

Vector Time (GMT): 2008/321/17:55:44
124
Vector Time (MET): 001/17:00:05
124
Weight (LBS)     : 247178
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4390867
10                 A    =         6718753
57  meter
 Y    =       -1158152
66  meter          E    =           
0023212
 Z    =       -4972640
58                 I    =           51
38869
 XDOT =       3895
218529                 Wp   =           60
79994
 YDOT =      -6327
366994  meter/sec      RA   =          313
78822  deg
 ZDOT =      -1961
572388                 TA   =          190
11029
                                          MA   =          190
15706
                                          Ha   =            192
341  n
mi
                                          Hp   =            178
985

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14405731
95                 X    =        -4353433
54
 Y    =       -3799713
46  feet           Y    =        -1207043
98  meter
 Z    =      -16314437
61                 Z    =        -4993880
96
 XDOT =      12779
588350                 XDOT =        3975
211786
 YDOT =     -20759
078063  feet/sec       YDOT =       -6283
360910  meter/sec
 ZDOT =      -6435
604946                 ZDOT =       -1942
455567

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9415450
18                 X    =        -2869829
22
 Y    =      -11428744
08  feet           Y    =        -3483481
20  meter
 Z    =      -16396856
91                 Z    =        -4997761
99
 XDOT =      21679
775555                 XDOT =        6607
995589
 YDOT =      -8713
256081  feet/sec       YDOT =       -2655
800453  meter/sec
 ZDOT =      -6361
937107                 ZDOT =       -1939
118430


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 00126U          08321
76624524  
00020000  00000-0  70000-3 0  9070
2 00126  51
6424 314
2466 0011036  44
0619 316
1422 15
74918117   298


Satellite: SHUTTLE
Catalog Number: 00126
Epoch time:      08321
76624524   =   yrday
fracday
Element set:     907
Inclination:       51
6424  deg
RA of node:       314
2466  deg
Eccentricity:     
0011036     
Arg of perigee:    44
0619  deg
Mean anomaly:     316
1422  deg
Mean motion:   15
74918117  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              29
Checksum:              245


Coasting Arc #9 (Orbit 29)
---------------------------------------

Vector Time (GMT): 2008/321/19:27:01
932
Vector Time (MET): 001/18:31:22
932
Weight (LBS)     : 246960
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4414662
35                 A    =         6723527
77  meter
 Y    =       -1104607
55  meter          E    =           
0016125
 Z    =       -4963652
30                 I    =           51
38799
 XDOT =       3834
669860                 Wp   =           56
39729
 YDOT =      -6358
377773  meter/sec      RA   =          313
46182  deg
 ZDOT =      -1991
421446                 TA   =          194
21919
                                          MA   =          194
26463
                                          Ha   =            192
385  n
mi
                                          Hp   =            184
189

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14483800
36                 X    =        -4377869
45
 Y    =       -3624040
51  feet           Y    =        -1153768
55  meter
 Z    =      -16284948
49                 Z    =        -4985009
82
 XDOT =      12580
937862                 XDOT =        3915
159385
 YDOT =     -20860
819466  feet/sec       YDOT =       -6315
046003  meter/sec
 ZDOT =      -6533
534927                 ZDOT =       -1972
597573

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13234085
23                 X    =        -4033749
18
 Y    =       -6713210
31  feet           Y    =        -2046186
50  meter
 Z    =      -16367818
59                 Z    =        -4988911
11
 XDOT =      16424
895710                 XDOT =        5006
308212
 YDOT =     -16593
380987  feet/sec       YDOT =       -5057
662525  meter/sec
 ZDOT =      -6461
004879                 ZDOT =       -1969
314287


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 00126U          08321
82970482  
00020000  00000-0  70000-3 0  9085
2 00126  51
6428 313
9211 0005624   9
2613 350
8652 15
73254509   308


Satellite: SHUTTLE
Catalog Number: 00126
Epoch time:      08321
82970482   =   yrday
fracday
Element set:     908
Inclination:       51
6428  deg
RA of node:       313
9211  deg
Eccentricity:     
0005624     
Arg of perigee:     9
2613  deg
Mean anomaly:     350
8652  deg
Mean motion:   15
73254509  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              30
Checksum:              250


Coasting Arc #10 (Orbit 30)
---------------------------------------

Vector Time (GMT): 2008/321/20:43:55
001
Vector Time (MET): 001/19:48:16
001
Weight (LBS)     : 246875
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5189921
42                 A    =         6735125
08  meter
 Y    =        4114790
45  meter          E    =           
0006434
 Z    =       -1214088
76                 I    =           51
42027
 XDOT =      -2193
642264                 Wp   =          124
50851
 YDOT =      -4486
501106  meter/sec      RA   =          313
18278  deg
 ZDOT =      -5853
986993                 TA   =           68
82650
                                          MA   =           68
75777
                                          Ha   =            192
384  n
mi
                                          Hp   =            185
711

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17027301
25                 X    =        -5229650
04
 Y    =       13499968
65  feet           Y    =         4056531
75  meter
 Z    =       -3983230
84                 Z    =        -1239397
80
 XDOT =      -7196
989056                 XDOT =       -2114
872407
 YDOT =     -14719
491818  feet/sec       YDOT =       -4510
590569  meter/sec
 ZDOT =     -19205
994071                 ZDOT =       -5864
453060

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15363201
30                 X    =        -4682703
76
 Y    =       15341489
17  feet           Y    =         4676085
90  meter
 Z    =       -4081056
88                 Z    =        -1243906
14
 XDOT =      -7591
692289                 XDOT =       -2313
947810
 YDOT =     -12700
577401  feet/sec       YDOT =       -3871
135992  meter/sec
 ZDOT =     -19246
878106                 ZDOT =       -5866
448447


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 00126U          08321
89323104  
00020000  00000-0  70000-3 0  9096
2 00126  51
6421 313
5954 0003575 356
0291   4
0843 15
72731994   317


Satellite: SHUTTLE
Catalog Number: 00126
Epoch time:      08321
89323104   =   yrday
fracday
Element set:     909
Inclination:       51
6421  deg
RA of node:       313
5954  deg
Eccentricity:     
0003575     
Arg of perigee:   356
0291  deg
Mean anomaly:       4
0843  deg
Mean motion:   15
72731994  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              31
Checksum:              250


Coasting Arc #11 (Orbit 46)
---------------------------------------

Vector Time (GMT): 2008/322/20:45:40
580
Vector Time (MET): 002/19:50:01
580
Weight (LBS)     : 246875
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2031138
57                 A    =         6724457
19  meter
 Y    =        3950981
58  meter          E    =           
0007904
 Z    =        5046117
09                 I    =           51
36557
 XDOT =      -5603
859127                 Wp   =           31
66074
 YDOT =       5013
567193  meter/sec      RA   =          308
00627  deg
 ZDOT =      -1662
047347                 TA   =           74
42230
                                          MA   =           74
33506
                                          Ha   =            192
326  n
mi
                                          Hp   =            185
513

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6663840
45                 X    =         1962293
70
 Y    =       12962538
01  feet           Y    =         3973309
54  meter
 Z    =       16555502
25                 Z    =         5055817
62
 XDOT =     -18385
364589                 XDOT =       -5651
431144
 YDOT =      16448
711264  feet/sec       YDOT =        4950
635771  meter/sec
 ZDOT =      -5452
911242                 ZDOT =       -1689
386273

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8296182
61                 X    =         2528676
46
 Y    =       11931120
97  feet           Y    =         3636605
67  meter
 Z    =       16593387
91                 Z    =         5057664
63
 XDOT =     -15035
790016                 XDOT =       -4582
908797
 YDOT =      18221
169158  feet/sec       YDOT =        5553
812359  meter/sec
 ZDOT =      -5558
544762                 ZDOT =       -1694
244444


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 00126U          08322
90985578  
00020000  00000-0  70000-3 0  9100
2 00126  51
6419 308
3834 0003720 359
6844    
4315 15
72812323   475


Satellite: SHUTTLE
Catalog Number: 00126
Epoch time:      08322
90985578   =   yrday
fracday
Element set:     910
Inclination:       51
6419  deg
RA of node:       308
3834  deg
Eccentricity:     
0003720     
Arg of perigee:   359
6844  deg
Mean anomaly:        
4315  deg
Mean motion:   15
72812323  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              47
Checksum:              262


Coasting Arc #12 (Orbit 62)
---------------------------------------

Vector Time (GMT): 2008/323/20:46:59
463
Vector Time (MET): 003/19:51:20
463
Weight (LBS)     : 246875
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4523316
85                 A    =         6734428
28  meter
 Y    =       -4733399
39  meter          E    =           
0016213
 Z    =        1537988
48                 I    =           51
38122
 XDOT =       2631
993017                 Wp   =           51
19817
 YDOT =       4394
691439  meter/sec      RA   =          302
88414  deg
 ZDOT =       5753
857232                 TA   =          325
82094
                                          MA   =          325
92521
                                          Ha   =            192
323  n
mi
                                          Hp   =            185
368

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14840278
39                 X    =         4568438
97
 Y    =      -15529525
57  feet           Y    =        -4682564
87  meter
 Z    =        5045893
96                 Z    =         1560072
24
 XDOT =       8635
147693                 XDOT =        2554
703772
 YDOT =      14418
279000  feet/sec       YDOT =        4423
691354  meter/sec
 ZDOT =      18877
484358                 ZDOT =        5766
456154

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12120772
93                 X    =         3694411
59
 Y    =      -17709291
78  feet           Y    =        -5397792
13  meter
 Z    =        5131171
52                 Z    =         1563981
08
 XDOT =       9443
028469                 XDOT =        2878
235077
 YDOT =      11975
629627  feet/sec       YDOT =        3650
171910  meter/sec
 ZDOT =      18926
645285                 ZDOT =        5768
841483


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 00126U          08323
92646307  
00020000  00000-0  70000-3 0  9118
2 00126  51
6407 303
1712 0003645   2
9738 357
1445 15
72848719   638


Satellite: SHUTTLE
Catalog Number: 00126
Epoch time:      08323
92646307   =   yrday
fracday
Element set:     911
Inclination:       51
6407  deg
RA of node:       303
1712  deg
Eccentricity:     
0003645     
Arg of perigee:     2
9738  deg
Mean anomaly:     357
1445  deg
Mean motion:   15
72848719  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              63
Checksum:              263

SPACE SHUTTLE ORBITAL DATA:

The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:

NASA Orbital Flight Dynamics 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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