Date: March 23rd 2008

SHUTTLE TRAJECTORY DATA

Lift off time (UTC) : 2008/071/06:28:13 948 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 10 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : -0 34056

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


085/01:11:19 576 -0 7 -0 0 2 9
013/18:43:05 628 2 7 -0 0 185 6
000/00:00:11 257 0 9 -2 9 180 8

085/01:39:16 805 0 6 1 5 1 5
013/19:11:02 857 -1 1 -0 0 186 4
000/00:00:05 714 -0 8 -0 0 181 0

085/17:53:21 706 -2 5 4 0 4 0
014/11:25:07 758 -0 7 0 0 188 3
000/00:00:15 516 3 1 -0 0 181 7

Coasting Arc #1 (Orbit 188)
---------------------------------------

Vector Time (GMT): 2008/083/02:03:54
000
Vector Time (MET): 011/19:35:40
052
Weight (LBS)     : 219017
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3130520
87                 A    =         6721987
56  meter
 Y    =        5214561
32  meter          E    =           
0012318
 Z    =        2848654
84                 I    =           51
96460
 XDOT =      -3259
638715                 Wp   =           77
78508
 YDOT =      -4758
298890  meter/sec      RA   =           99
48469  deg
 ZDOT =       5112
190887                 TA   =          314
79748
                                          MA   =          314
89758
                                          Ha   =            186
072  n
mi
                                          Hp   =            180
641

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10270737
76                 X    =        -3202307
88
 Y    =       17108140
80  feet           Y    =         5179231
80  meter
 Z    =        9345980
44                 Z    =         2833271
47
 XDOT =     -10694
352739                 XDOT =       -3231
141616
 YDOT =     -15611
216830  feet/sec       YDOT =       -4794
509194  meter/sec
 ZDOT =      16772
279813                 ZDOT =        5096
425609

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         -20236
69                 X    =           -6168
14
 Y    =      -19981595
98  feet           Y    =        -6090390
46  meter
 Z    =        9287588
42                 Z    =         2830856
95
 XDOT =      15854
236707                 XDOT =        4832
371348
 YDOT =       7775
814071  feet/sec       YDOT =        2370
068129  meter/sec
 ZDOT =      16711
271162                 ZDOT =        5093
595450


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 32699U 08009A   08083
14371426  
00020000  00000-0  70000-3 0  9007
2 32699  51
6352  99
9518 0001374 289
5544  70
5472 15
76367239  1898


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08083
14371426   =   yrday
fracday
Element set:     900
Inclination:       51
6352  deg
RA of node:        99
9518  deg
Eccentricity:     
0001374     
Arg of perigee:   289
5544  deg
Mean anomaly:      70
5472  deg
Mean motion:   15
76367239  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             189
Checksum:              325


Coasting Arc #2 (Orbit 203)
---------------------------------------

Vector Time (GMT): 2008/084/02:08:49
570
Vector Time (MET): 012/19:40:35
623
Weight (LBS)     : 219017
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1578481
82                 A    =         6722478
63  meter
 Y    =        5999532
64  meter          E    =           
0004638
 Z    =       -2586459
17                 I    =           51
97125
 XDOT =      -4410
534930                 Wp   =           38
41488
 YDOT =       3439
284189  meter/sec      RA   =           94
29002  deg
 ZDOT =       5294
633259                 TA   =          292
34113
                                          MA   =          292
39028
                                          Ha   =            186
037  n
mi
                                          Hp   =            180
538

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5178746
14                 X    =         1523990
84
 Y    =       19683506
05  feet           Y    =         6016840
52  meter
 Z    =       -8485758
43                 Z    =        -2578924
19
 XDOT =     -14470
258957                 XDOT =       -4474
302045
 YDOT =      11283
740777  feet/sec       YDOT =        3389
717701  meter/sec
 ZDOT =      17370
844024                 ZDOT =        5273
051352

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15195871
19                 X    =        -4631701
54
 Y    =      -13558999
49  feet           Y    =        -4132783
04  meter
 Z    =       -8456178
20                 Z    =        -2577443
11
 XDOT =       4966
412053                 XDOT =        1513
762394
 YDOT =     -16330
432855  feet/sec       YDOT =       -4977
515934  meter/sec
 ZDOT =      17288
469247                 ZDOT =        5269
525427


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 32699U 08009A   08084
09462384  
00020000  00000-0  70000-3 0  9017
2 32699  51
6363  95
0505 0001239 292
6265  67
4768 15
76392041  2048


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08084
09462384   =   yrday
fracday
Element set:     901
Inclination:       51
6363  deg
RA of node:        95
0505  deg
Eccentricity:     
0001239     
Arg of perigee:   292
6265  deg
Mean anomaly:      67
4768  deg
Mean motion:   15
76392041  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             204
Checksum:              305


Coasting Arc #3 (Orbit 219)
---------------------------------------

Vector Time (GMT): 2008/085/01:11:25
204
Vector Time (MET): 013/18:43:11
257
Weight (LBS)     : 218943
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1568570
92                 A    =         6723358
30  meter
 Y    =        6188213
48  meter          E    =           
0012535
 Z    =        2088017
22                 I    =           51
97475
 XDOT =      -4392
453601                 Wp   =           61
22703
 YDOT =      -3001
539667  meter/sec      RA   =           89
40433  deg
 ZDOT =       5576
772168                 TA   =          322
01613
                                          MA   =          322
10447
                                          Ha   =            185
640  n
mi
                                          Hp   =            180
839

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5146230
05                 X    =        -1647641
94
 Y    =       20302537
67  feet           Y    =         6170270
95  meter
 Z    =        6850450
18                 Z    =         2080204
12
 XDOT =     -14410
937010                 XDOT =       -4385
730340
 YDOT =      -9847
571085  feet/sec       YDOT =       -3050
511215  meter/sec
 ZDOT =      18296
496615                 ZDOT =        5555
450255

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2064824
21                 X    =         -629358
42
 Y    =      -20852179
12  feet           Y    =        -6355744
20  meter
 Z    =        6821181
27                 Z    =         2079096
05
 XDOT =      15485
348826                 XDOT =        4719
934322
 YDOT =       4445
509826  feet/sec       YDOT =        1354
991395  meter/sec
 ZDOT =      18214
388117                 ZDOT =        5551
745498


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 32699U 08009A   08085
10889797  
00020000  00000-0  70000-3 0  9022
2 32699  51
6355  89
8227 0002484 296
5581  63
5329 15
76452509  2202


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08085
10889797   =   yrday
fracday
Element set:     902
Inclination:       51
6355  deg
RA of node:        89
8227  deg
Eccentricity:     
0002484     
Arg of perigee:   296
5581  deg
Mean anomaly:      63
5329  deg
Mean motion:   15
76452509  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             220
Checksum:              334


Coasting Arc #4 (Orbit 219)
---------------------------------------

Vector Time (GMT): 2008/085/01:39:19
662
Vector Time (MET): 013/19:11:05
714
Weight (LBS)     : 218899
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3063865
60                 A    =         6719725
85  meter
 Y    =       -4579141
81  meter          E    =           
0010160
 Z    =        3839944
48                 I    =           51
95948
 XDOT =       3190
287689                 Wp   =           79
25705
 YDOT =      -5640
926603  meter/sec      RA   =           89
25998  deg
 ZDOT =      -4170
209656                 TA   =           54
19039
                                          MA   =           54
09602
                                          Ha   =            186
403  n
mi
                                          Hp   =            180
985

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10052052
50                 X    =        -3031201
65
 Y    =      -15023431
15  feet           Y    =        -4613144
85  meter
 Z    =       12598243
05                 Z    =         3825140
12
 XDOT =      10466
823125                 XDOT =        3273
247352
 YDOT =     -18506
977043  feet/sec       YDOT =       -5604
867977  meter/sec
 ZDOT =     -13681
790211                 ZDOT =       -4154
508851

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15837073
36                 X    =         4827139
96
 Y    =        8796282
07  feet           Y    =         2681106
78  meter
 Z    =       12540952
91                 Z    =         3822482
45
 XDOT =       -359
967813                 XDOT =        -109
718189
 YDOT =      20121
574620  feet/sec       YDOT =        6133
055944  meter/sec
 ZDOT =     -13622
209522                 ZDOT =       -4152
049462


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 32699U 08009A   08085
10890757  
00020000  00000-0  70000-3 0  9031
2 32699  51
6354  89
8226 0001339 280
1486  79
9527 15
76145040  2201


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08085
10890757   =   yrday
fracday
Element set:     903
Inclination:       51
6354  deg
RA of node:        89
8226  deg
Eccentricity:     
0001339     
Arg of perigee:   280
1486  deg
Mean anomaly:      79
9527  deg
Mean motion:   15
76145040  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             220
Checksum:              312


Coasting Arc #5 (Orbit 230)
---------------------------------------

Vector Time (GMT): 2008/085/17:53:29
464
Vector Time (MET): 014/11:25:15
516
Weight (LBS)     : 218797
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -557714
60                 A    =         6727427
82  meter
 Y    =        6563435
17  meter          E    =           
0015906
 Z    =        1321446
33                 I    =           51
98116
 XDOT =      -4724
197865                 Wp   =           46
26448
 YDOT =      -1591
622420  meter/sec      RA   =           85
83333  deg
 ZDOT =       5878
712244                 TA   =          328
19355
                                          MA   =          328
28952
                                          Ha   =            188
287  n
mi
                                          Hp   =            181
700

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1829772
31                 X    =         -637323
05
 Y    =       21533579
96  feet           Y    =         6556768
38  meter
 Z    =        4335453
83                 Z    =         1318542
74
 XDOT =     -15499
336828                 XDOT =       -4734
647729
 YDOT =      -5221
858333  feet/sec       YDOT =       -1644
391331  meter/sec
 ZDOT =      19287
113663                 ZDOT =        5855
736767

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21567318
21                 X    =         6573718
59
 Y    =        1408560
79  feet           Y    =          429329
33  meter
 Z    =        4325047
32                 Z    =         1318274
42
 XDOT =      -4795
229317                 XDOT =       -1461
585896
 YDOT =      14140
509751  feet/sec       YDOT =        4310
027372  meter/sec
 ZDOT =      19198
821890                 ZDOT =        5851
800912


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 32699U 08009A   08085
80636409  
00020000  00000-0  70000-3 0  9041
2 32699  51
6390  86
2344 0003943 352
0609   8
0492 15
75417670  2318


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08085
80636409   =   yrday
fracday
Element set:     904
Inclination:       51
6390  deg
RA of node:        86
2344  deg
Eccentricity:     
0003943     
Arg of perigee:   352
0609  deg
Mean anomaly:       8
0492  deg
Mean motion:   15
75417670  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             231
Checksum:              299


Coasting Arc #6 (Orbit 245)
---------------------------------------

Vector Time (GMT): 2008/086/17:53:40
870
Vector Time (MET): 015/11:25:26
922
Weight (LBS)     : 218797
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4212561
05                 A    =         6717511
50  meter
 Y    =        1701033
63  meter          E    =           
0011898
 Z    =       -4958287
46                 I    =           51
94546
 XDOT =       -478
469703                 Wp   =           87
50471
 YDOT =       7378
562042  meter/sec      RA   =           80
67935  deg
 ZDOT =       2129
712772                 TA   =          203
04753
                                          MA   =          203
10095
                                          Ha   =            188
324  n
mi
                                          Hp   =            181
681

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13820738
37                 X    =         4217356
76
 Y    =        5580819
01  feet           Y    =         1748062
50  meter
 Z    =      -16267347
30                 Z    =        -4937811
26
 XDOT =      -1569
782489                 XDOT =        -571
105087
 YDOT =      24207
880715  feet/sec       YDOT =        7372
706831  meter/sec
 ZDOT =       6987
246627                 ZDOT =        2127
162550

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5038112
07                 X    =         1535616
56
 Y    =      -14118451
76  feet           Y    =        -4303304
10  meter
 Z    =      -16188628
25                 Z    =        -4934293
89
 XDOT =      23222
488705                 XDOT =        7078
214557
 YDOT =        303
754770  feet/sec       YDOT =          92
584454  meter/sec
 ZDOT =       6978
273360                 ZDOT =        2126
977720


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 32699U 08009A   08086
75784449  
00020000  00000-0  70000-3 0  9055
2 32699  51
6399  81
3377 0003942 355
1052   5
0073 15
75435239  2463


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08086
75784449   =   yrday
fracday
Element set:     905
Inclination:       51
6399  deg
RA of node:        81
3377  deg
Eccentricity:     
0003942     
Arg of perigee:   355
1052  deg
Mean anomaly:       5
0073  deg
Mean motion:   15
75435239  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             246
Checksum:              318


Coasting Arc #7 (Orbit 261)
---------------------------------------

Vector Time (GMT): 2008/087/17:58:53
003
Vector Time (MET): 016/11:30:39
056
Weight (LBS)     : 218797
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1763082
72                 A    =         6721599
35  meter
 Y    =       -5229949
62  meter          E    =           
0008261
 Z    =       -3846263
07                 I    =           51
95430
 XDOT =       4549
378387                 Wp   =           46
57632
 YDOT =       4598
163506  meter/sec      RA   =           75
57962  deg
 ZDOT =      -4166
966695                 TA   =          179
97715
                                          MA   =          179
97712
                                          Ha   =            188
297  n
mi
                                          Hp   =            181
495

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5784392
14                 X    =         1839988
93
 Y    =      -17158627
37  feet           Y    =        -5209848
92  meter
 Z    =      -12618973
33                 Z    =        -3837510
69
 XDOT =      14925
782110                 XDOT =        4517
980786
 YDOT =      15085
838275  feet/sec       YDOT =        4648
748713  meter/sec
 ZDOT =     -13671
150573                 ZDOT =       -4144
942435

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17565800
36                 X    =        -5354055
95
 Y    =       -4489123
68  feet           Y    =        -1368284
90  meter
 Z    =      -12585968
38                 Z    =        -3836203
16
 XDOT =      13532
573496                 XDOT =        4124
728402
 YDOT =     -14861
573044  feet/sec       YDOT =       -4529
807464  meter/sec
 ZDOT =     -13586
179734                 ZDOT =       -4141
067583


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 32699U 08009A   08087
77274320  
00020000  00000-0  70000-3 0  9061
2 32699  51
6406  76
1144 0003969 358
1655   1
9493 15
75472853  2629


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08087
77274320   =   yrday
fracday
Element set:     906
Inclination:       51
6406  deg
RA of node:        76
1144  deg
Eccentricity:     
0003969     
Arg of perigee:   358
1655  deg
Mean anomaly:       1
9493  deg
Mean motion:   15
75472853  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             262
Checksum:              320


Coasting Arc #8 (Orbit 277)
---------------------------------------

Vector Time (GMT): 2008/088/18:03:59
758
Vector Time (MET): 017/11:35:45
811
Weight (LBS)     : 218797
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3334455
05                 A    =         6726911
95  meter
 Y    =       -5611433
25  meter          E    =           
0013024
 Z    =        1608566
46                 I    =           51
96339
 XDOT =       3470
141720                 Wp   =          101
22525
 YDOT =      -3728
827444  meter/sec      RA   =           70
39572  deg
 ZDOT =      -5777
837597                 TA   =           61
08901
                                          MA   =           60
95842
                                          Ha   =            188
391  n
mi
                                          Hp   =            181
360

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10939813
15                 X    =        -3279413
71
 Y    =      -18410214
07  feet           Y    =        -5648331
01  meter
 Z    =        5277449
03                 Z    =         1592501
86
 XDOT =      11384
979397                 XDOT =        3539
556222
 YDOT =     -12233
685841  feet/sec       YDOT =       -3689
721771  meter/sec
 ZDOT =     -18956
160095                 ZDOT =       -5760
810705

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16987479
04                 X    =        -5177783
61
 Y    =       13064987
10  feet           Y    =         3982208
07  meter
 Z    =        5215230
58                 Z    =         1589602
28
 XDOT =     -12551
352190                 XDOT =       -3825
652148
 YDOT =      -8730
093380  feet/sec       YDOT =       -2660
932462  meter/sec
 ZDOT =     -18891
248249                 ZDOT =       -5758
052466


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 32699U 08009A   08088
78762346  
00020000  00000-0  70000-3 0  9074
2 32699  51
6405  70
8910 0003854   3
4246 356
6944 15
75471565  2786


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08088
78762346   =   yrday
fracday
Element set:     907
Inclination:       51
6405  deg
RA of node:        70
8910  deg
Eccentricity:     
0003854     
Arg of perigee:     3
4246  deg
Mean anomaly:     356
6944  deg
Mean motion:   15
75471565  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             278
Checksum:              330


Coasting Arc #9 (Orbit 293)
---------------------------------------

Vector Time (GMT): 2008/089/18:04:15
796
Vector Time (MET): 018/11:36:01
849
Weight (LBS)     : 218797
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3151232
92                 A    =         6716160
34  meter
 Y    =        2872621
00  meter          E    =           
0004010
 Z    =        5185523
40                 I    =           51
91730
 XDOT =      -3992
760973                 Wp   =           63
87492
 YDOT =      -6487
516976  meter/sec      RA   =           65
29347  deg
 ZDOT =       1168
529051                 TA   =           15
02479
                                          MA   =           15
01288
                                          Ha   =            188
468  n
mi
                                          Hp   =            181
152

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10338690
68                 X    =        -3208240
63
 Y    =        9424609
59  feet           Y    =         2837142
80  meter
 Z    =       17012872
05                 Z    =         5170076
03
 XDOT =     -13099
609491                 XDOT =       -3925
758504
 YDOT =     -21284
504513  feet/sec       YDOT =       -6531
693246  meter/sec
 ZDOT =       3833
756728                 ZDOT =        1149
295586

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10758021
39                 X    =         3279044
92
 Y    =        9054231
79  feet           Y    =         2759729
85  meter
 Z    =       16953921
94                 Z    =         5167555
41
 XDOT =     -18638
813663                 XDOT =       -5681
110404
 YDOT =      15113
363213  feet/sec       YDOT =        4606
553107  meter/sec
 ZDOT =       3759
291836                 ZDOT =        1145
832152


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 32699U 08009A   08089
80248136  
00020000  00000-0  70000-3 0  9085
2 32699  51
6410  65
6673 0003979   5
7703 354
3506 15
75541297  2948


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08089
80248136   =   yrday
fracday
Element set:     908
Inclination:       51
6410  deg
RA of node:        65
6673  deg
Eccentricity:     
0003979     
Arg of perigee:     5
7703  deg
Mean anomaly:     354
3506  deg
Mean motion:   15
75541297  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             294
Checksum:              323

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 may contain past, current and future orbital data 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

The following information is a reminder of your current mailing list subscription:

You are subscribed to the following list: [list_name]

using the following email: example@example.com

You may automatically unsubscribe from this list at any time by visiting the following URL:

http://www aus-city com/cgi-bin/dada/mail cgi/u/[list]/

If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism

You may also change your subscription by visiting this list's main screen:

http://www aus-city com/cgi-bin/dada/mail cgi/list/[list]

If you're still having trouble, please contact the list owner at:

<mailto:list
admin@aus-city
com>

The following physical address is associated with this mailing list:

http://www aus-city com

Forward to a Friend
 
  • This mailing list is a public mailing list - anyone may join or leave, at any time.
  • This mailing list is announce-only.

Shuttle TLE list

Privacy Policy:

Private list