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


085/01:11:19 531 -0 7 -0 0 2 9
013/18:43:05 583 2 7 -0 0 185 6
000/00:00:11 167 0 9 -2 9 180 8

085/01:39:16 782 0 6 1 5 1 5
013/19:11:02 834 -1 1 -0 0 186 3
000/00:00:05 669 -0 8 -0 0 181 0

085/17:53:51 644 -2 4 4 0 4 0
014/11:25:37 696 -0 9 0 0 188 3
000/00:00:15 393 3 0 -0 0 181 6

Coasting Arc #1 (Orbit 174)
---------------------------------------

Vector Time (GMT): 2008/082/04:54:18
000
Vector Time (MET): 010/22:26:04
052
Weight (LBS)     : 219350
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4329235
04                 A    =         6715363
99  meter
 Y    =        1738767
78  meter          E    =           
0005673
 Z    =        4827573
59                 I    =           51
94047
 XDOT =       -172
123588                 Wp   =          126
66069
 YDOT =      -7298
222106  meter/sec      RA   =          104
00407  deg
 ZDOT =       2468
976042                 TA   =          299
30102
                                          MA   =          299
35769
                                          Ha   =            186
018  n
mi
                                          Hp   =            180
704

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14203527
05                 X    =        -4371765
90
 Y    =        5704618
69  feet           Y    =         1690226
94  meter
 Z    =       15838496
03                 Z    =         4806438
60
 XDOT =       -564
709933                 XDOT =        -102
676037
 YDOT =     -23944
298249  feet/sec       YDOT =       -7299
754718  meter/sec
 ZDOT =       8100
315100                 ZDOT =        2468
309915

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1248879
43                 X    =         -380658
45
 Y    =      -15338762
65  feet           Y    =        -4675254
86  meter
 Z    =       15757648
05                 Z    =         4802931
13
 XDOT =      21946
547663                 XDOT =        6689
307728
 YDOT =       6549
097989  feet/sec       YDOT =        1996
165067  meter/sec
 ZDOT =       8096
908948                 ZDOT =        2467
937847


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   08082
25618133  
00020000  00000-0  70000-3 0  9007
2 32699  51
6385 104
5254 0001583 279
0250  81
0735 15
76381061  1757


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08082
25618133   =   yrday
fracday
Element set:     900
Inclination:       51
6385  deg
RA of node:       104
5254  deg
Eccentricity:     
0001583     
Arg of perigee:   279
0250  deg
Mean anomaly:      81
0735  deg
Mean motion:   15
76381061  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             175
Checksum:              284


Coasting Arc #2 (Orbit 190)
---------------------------------------

Vector Time (GMT): 2008/083/04:58:35
012
Vector Time (MET): 011/22:30:21
065
Weight (LBS)     : 219350
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1140059
34                 A    =         6725412
11  meter
 Y    =        6620291
40  meter          E    =           
0011896
 Z    =         139631
05                 I    =           51
98076
 XDOT =      -4655
912948                 Wp   =           40
48386
 YDOT =       -935
615729  meter/sec      RA   =           98
83976  deg
 ZDOT =       6068
338693                 TA   =          321
02768
                                          MA   =          321
11336
                                          Ha   =            185
963  n
mi
                                          Hp   =            180
630

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3740352
16                 X    =        -1214517
95
 Y    =       21720116
13  feet           Y    =         6607155
54  meter
 Z    =         458107
11                 Z    =          133910
61
 XDOT =     -15275
304947                 XDOT =       -4674
608182
 YDOT =      -3069
605410  feet/sec       YDOT =        -987
668414  meter/sec
 ZDOT =      19909
247680                 ZDOT =        6045
674992

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20004297
69                 X    =        -6097309
94
 Y    =       -9252064
88  feet           Y    =        -2820029
38  meter
 Z    =         436933
08                 Z    =          133177
20
 XDOT =       6283
751487                 XDOT =        1915
287453
 YDOT =     -12605
234880  feet/sec       YDOT =       -3842
075591  meter/sec
 ZDOT =      19822
225566                 ZDOT =        6041
814352


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
27049098  
00020000  00000-0  70000-3 0  9019
2 32699  51
6391  99
2980 0001452 287
5372  72
5633 15
76391046  1918


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08083
27049098   =   yrday
fracday
Element set:     901
Inclination:       51
6391  deg
RA of node:        99
2980  deg
Eccentricity:     
0001452     
Arg of perigee:   287
5372  deg
Mean anomaly:      72
5633  deg
Mean motion:   15
76391046  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             191
Checksum:              317


Coasting Arc #3 (Orbit 205)
---------------------------------------

Vector Time (GMT): 2008/084/05:02:56
485
Vector Time (MET): 012/22:34:42
537
Weight (LBS)     : 219350
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3464340
75                 A    =         6715733
73  meter
 Y    =        3343525
26  meter          E    =           
0009522
 Z    =       -4690979
93                 I    =           51
95206
 XDOT =      -2630
892266                 Wp   =          109
32898
 YDOT =       6665
386581  meter/sec      RA   =           93
67119  deg
 ZDOT =       2809
365893                 TA   =          188
27617
                                          MA   =          188
29189
                                          Ha   =            185
869  n
mi
                                          Hp   =            180
611

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11365947
34                 X    =         3449567
49
 Y    =       10969571
05  feet           Y    =         3382096
30  meter
 Z    =      -15390354
10                 Z    =        -4674186
50
 XDOT =      -8631
536305                 XDOT =       -2718
712785
 YDOT =      21868
066211  feet/sec       YDOT =        6635
542283  meter/sec
 ZDOT =       9217
079703                 ZDOT =        2796
370598

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13259577
76                 X    =        -4041519
30
 Y    =        8699984
06  feet           Y    =         2651755
14  meter
 Z    =      -15325570
87                 Z    =        -4671234
00
 XDOT =     -18727
852563                 XDOT =       -5708
249461
 YDOT =     -12401
743886  feet/sec       YDOT =       -3780
051537  meter/sec
 ZDOT =       9168
000721                 ZDOT =        2794
406620


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
22137921  
00020000  00000-0  70000-3 0  9029
2 32699  51
6392  94
3980 0001463 289
2572  70
8434 15
76443270  2062


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08084
22137921   =   yrday
fracday
Element set:     902
Inclination:       51
6392  deg
RA of node:        94
3980  deg
Eccentricity:     
0001463     
Arg of perigee:   289
2572  deg
Mean anomaly:      70
8434  deg
Mean motion:   15
76443270  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             206
Checksum:              301


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

Vector Time (GMT): 2008/085/01:11:25
114
Vector Time (MET): 013/18:43:11
167
Weight (LBS)     : 217197
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1585205
96                 A    =         6723239
45  meter
 Y    =        6176616
21  meter          E    =           
0012479
 Z    =        2109270
98                 I    =           51
97490
 XDOT =      -4384
605525                 Wp   =           61
03585
 YDOT =      -3032
509562  meter/sec      RA   =           89
40342  deg
 ZDOT =       5566
293251                 TA   =          322
45847
                                          MA   =          322
54554
                                          Ha   =            185
576  n
mi
                                          Hp   =            180
828

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5200806
97                 X    =        -1664249
61
 Y    =       20264488
87  feet           Y    =         6158488
22  meter
 Z    =        6920180
39                 Z    =         2101377
14
 XDOT =     -14385
188731                 XDOT =       -4377
486400
 YDOT =      -9949
178353  feet/sec       YDOT =       -3081
391336  meter/sec
 ZDOT =      18262
116965                 ZDOT =        5545
010430

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2000023
20                 X    =         -609607
07
 Y    =      -20835218
52  feet           Y    =        -6350574
60  meter
 Z    =        6890600
51                 Z    =         2100255
03
 XDOT =      15496
896480                 XDOT =        4723
454047
 YDOT =       4545
251721  feet/sec       YDOT =        1385
392725  meter/sec
 ZDOT =      18180
154911                 ZDOT =        5541
311217


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
10885172  
00020000  00000-0  70000-3 0  9036
2 32699  51
6358  89
8219 0002599 297
2783  62
8116 15
76480750  2200


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08085
10885172   =   yrday
fracday
Element set:     903
Inclination:       51
6358  deg
RA of node:        89
8219  deg
Eccentricity:     
0002599     
Arg of perigee:   297
2783  deg
Mean anomaly:      62
8116  deg
Mean motion:   15
76480750  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             220
Checksum:              326


Coasting Arc #5 (Orbit 219)
---------------------------------------

Vector Time (GMT): 2008/085/01:39:19
616
Vector Time (MET): 013/19:11:05
669
Weight (LBS)     : 217153
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3051528
07                 A    =         6719699
51  meter
 Y    =       -4600899
53  meter          E    =           
0010129
 Z    =        3823770
79                 I    =           51
95995
 XDOT =       3205
738082                 Wp   =           79
10620
 YDOT =      -5617
561633  meter/sec      RA   =           89
25890  deg
 ZDOT =      -4189
773904                 TA   =           54
59603
                                          MA   =           54
50147
                                          Ha   =            186
327  n
mi
                                          Hp   =            180
975

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10011575
04                 X    =        -3018543
71
 Y    =      -15094814
72  feet           Y    =        -4634763
12  meter
 Z    =       12545179
75                 Z    =         3809027
14
 XDOT =      10517
513393                 XDOT =        3288
530951
 YDOT =     -18430
320317  feet/sec       YDOT =       -5581
331548  meter/sec
 ZDOT =     -13745
977375                 ZDOT =       -4173
998448

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15833085
67                 X    =         4825924
51
 Y    =        8878449
05  feet           Y    =         2706151
27  meter
 Z    =       12488120
03                 Z    =         3806378
98
 XDOT =       -434
319652                 XDOT =        -132
380630
 YDOT =      20076
706505  feet/sec       YDOT =        6119
380143  meter/sec
 ZDOT =     -13686
107772                 ZDOT =       -4171
525649


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
10886129  
00020000  00000-0  70000-3 0  9040
2 32699  51
6357  89
8217 0001445 282
5081  77
5921 15
76173198  2206


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08085
10886129   =   yrday
fracday
Element set:     904
Inclination:       51
6357  deg
RA of node:        89
8217  deg
Eccentricity:     
0001445     
Arg of perigee:   282
5081  deg
Mean anomaly:      77
5921  deg
Mean motion:   15
76173198  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             220
Checksum:              316


Coasting Arc #6 (Orbit 230)
---------------------------------------

Vector Time (GMT): 2008/085/17:53:59
340
Vector Time (MET): 014/11:25:45
393
Weight (LBS)     : 217052
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -721867
61                 A    =         6727092
89  meter
 Y    =        6502581
22  meter          E    =           
0015913
 Z    =        1525341
68                 I    =           51
98061
 XDOT =      -4694
877983                 Wp   =           48
49986
 YDOT =      -1891
494896  meter/sec      RA   =           85
83213  deg
 ZDOT =       5813
266067                 TA   =          328
25104
                                          MA   =          328
34689
                                          Ha   =            188
266  n
mi
                                          Hp   =            181
638

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2368332
05                 X    =         -801775
43
 Y    =       21333927
89  feet           Y    =         6494081
21  meter
 Z    =        5004401
84                 Z    =         1521639
91
 XDOT =     -15403
142988                 XDOT =       -4701
666316
 YDOT =      -6205
691917  feet/sec       YDOT =       -1943
916245  meter/sec
 ZDOT =      19072
395234                 ZDOT =        5790
441958

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21383133
33                 X    =         6517579
04
 Y    =        1908341
24  feet           Y    =          581662
41  meter
 Z    =        4990927
41                 Z    =         1521234
67
 XDOT =      -5710
343159                 XDOT =       -1740
512595
 YDOT =      14089
680716  feet/sec       YDOT =        4294
534682  meter/sec
 ZDOT =      18984
650667                 ZDOT =        5786
521523


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
80630511  
00020000  00000-0  70000-3 0  9050
2 32699  51
6393  86
2335 0003982 352
6941   7
4164 15
75446996  2311


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08085
80630511   =   yrday
fracday
Element set:     905
Inclination:       51
6393  deg
RA of node:        86
2335  deg
Eccentricity:     
0003982     
Arg of perigee:   352
6941  deg
Mean anomaly:       7
4164  deg
Mean motion:   15
75446996  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             231
Checksum:              311


Coasting Arc #7 (Orbit 245)
---------------------------------------

Vector Time (GMT): 2008/086/17:59:17
384
Vector Time (MET): 015/11:31:03
436
Weight (LBS)     : 217052
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3732237
54                 A    =         6721552
96  meter
 Y    =        4038994
60  meter          E    =           
0006327
 Z    =       -3867998
69                 I    =           51
95974
 XDOT =      -2285
553304                 Wp   =           69
27520
 YDOT =       6072
669697  meter/sec      RA   =           80
64917  deg
 ZDOT =       4143
394006                 TA   =          243
79905
                                          MA   =          243
86411
                                          Ha   =            188
311  n
mi
                                          Hp   =            181
560

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12244873
84                 X    =         3705686
98
 Y    =       13251294
63  feet           Y    =         4080489
39  meter
 Z    =      -12690284
41                 Z    =        -3849932
30
 XDOT =      -7498
534462                 XDOT =       -2373
266778
 YDOT =      19923
457011  feet/sec       YDOT =        6046
679199  meter/sec
 ZDOT =      13593
812356                 ZDOT =        4132
077021

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12446205
39                 X    =         3793603
40
 Y    =      -13129764
07  feet           Y    =        -4001952
09  meter
 Z    =      -12620551
88                 Z    =        -3846744
21
 XDOT =      19405
038632                 XDOT =        5914
655775
 YDOT =       5393
351683  feet/sec       YDOT =        1643
893593  meter/sec
 ZDOT =      13551
072698                 ZDOT =        4130
366958


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
75776746  
00020000  00000-0  70000-3 0  9067
2 32699  51
6402  81
3366 0003973 355
9609   4
1522 15
75470079  2466


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08086
75776746   =   yrday
fracday
Element set:     906
Inclination:       51
6402  deg
RA of node:        81
3366  deg
Eccentricity:     
0003973     
Arg of perigee:   355
9609  deg
Mean anomaly:       4
1522  deg
Mean motion:   15
75470079  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             246
Checksum:              323


Coasting Arc #8 (Orbit 261)
---------------------------------------

Vector Time (GMT): 2008/087/18:04:12
657
Vector Time (MET): 016/11:35:58
709
Weight (LBS)     : 217052
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3097592
19                 A    =         6717460
52  meter
 Y    =       -3393905
24  meter          E    =           
0014072
 Z    =       -4912791
61                 I    =           51
94097
 XDOT =       3495
451617                 Wp   =           57
47342
 YDOT =       6468
367912  meter/sec      RA   =           75
55112  deg
 ZDOT =      -2261
881308                 TA   =          190
58376
                                          MA   =          190
61341
                                          Ha   =            188
273  n
mi
                                          Hp   =            181
423

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10162704
03                 X    =         3159095
27
 Y    =      -11134859
73  feet           Y    =        -3359000
47  meter
 Z    =      -16118082
70                 Z    =        -4897593
74
 XDOT =      11468
017115                 XDOT =        3434
010985
 YDOT =      21221
679501  feet/sec       YDOT =        6507
026255  meter/sec
 ZDOT =      -7420
870433                 ZDOT =       -2245
050192

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12120980
70                 X    =        -3694474
92
 Y    =       -9067050
51  feet           Y    =        -2763637
00  meter
 Z    =      -16060157
73                 Z    =        -4895136
07
 XDOT =      19278
344779                 XDOT =        5876
039489
 YDOT =     -12726
954007  feet/sec       YDOT =       -3879
175581  meter/sec
 ZDOT =      -7355
615982                 ZDOT =       -2241
991751


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
77264720  
00020000  00000-0  70000-3 0  9075
2 32699  51
6409  76
1133 0004024 359
5938    
5222 15
75516859  2622


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08087
77264720   =   yrday
fracday
Element set:     907
Inclination:       51
6409  deg
RA of node:        76
1133  deg
Eccentricity:     
0004024     
Arg of perigee:   359
5938  deg
Mean anomaly:        
5222  deg
Mean motion:   15
75516859  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             262
Checksum:              307


Coasting Arc #9 (Orbit 277)
---------------------------------------

Vector Time (GMT): 2008/088/18:09:24
079
Vector Time (MET): 017/11:41:10
132
Weight (LBS)     : 217052
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1961306
44                 A    =         6727864
47  meter
 Y    =       -6420817
78  meter          E    =           
0009042
 Z    =        -392447
80                 I    =           51
96743
 XDOT =       4646
463582                 Wp   =          120
70474
 YDOT =      -1056
122780  meter/sec      RA   =           70
39348  deg
 ZDOT =      -6048
888111                 TA   =           63
54401
                                          MA   =           63
45127
                                          Ha   =            188
323  n
mi
                                          Hp   =            181
330

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6434732
42                 X    =        -1887615
64
 Y    =      -21065675
13  feet           Y    =        -6442290
44  meter
 Z    =       -1287558
40                 Z    =         -401796
28
 XDOT =      15244
303091                 XDOT =        4687
287472
 YDOT =      -3464
969752  feet/sec       YDOT =       -1004
051545  meter/sec
 ZDOT =     -19845
433436                 ZDOT =       -6026
216324

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19944933
74                 X    =        -6079215
81
 Y    =        9341982
01  feet           Y    =         2847436
12  meter
 Z    =       -1324102
21                 Z    =         -403586
35
 XDOT =      -4920
741031                 XDOT =       -1499
841866
 YDOT =     -13257
911220  feet/sec       YDOT =       -4041
011340  meter/sec
 ZDOT =     -19758
583939                 ZDOT =       -6022
416385


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
78750803  
00020000  00000-0  70000-3 0  9080
2 32699  51
6411  70
8897 0003851   2
5302 357
5881 15
75496053  2786


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08088
78750803   =   yrday
fracday
Element set:     908
Inclination:       51
6411  deg
RA of node:        70
8897  deg
Eccentricity:     
0003851     
Arg of perigee:     2
5302  deg
Mean anomaly:     357
5881  deg
Mean motion:   15
75496053  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             278
Checksum:              326


Coasting Arc #10 (Orbit 293)
---------------------------------------

Vector Time (GMT): 2008/089/18:09:36
545
Vector Time (MET): 018/11:41:22
597
Weight (LBS)     : 217052
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4220384
45                 A    =         6715992
07  meter
 Y    =         562767
75  meter          E    =           
0007157
 Z    =        5191875
04                 I    =           51
91749
 XDOT =      -2364
905441                 Wp   =           29
37667
 YDOT =      -7246
242707  meter/sec      RA   =           65
25316  deg
 ZDOT =      -1130
183347                 TA   =           71
40113
                                          MA   =           71
32341
                                          Ha   =            188
376  n
mi
                                          Hp   =            181
089

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13846405
68                 X    =        -4251572
07
 Y    =        1846350
87  feet           Y    =          515504
28  meter
 Z    =       17033710
78                 Z    =         5171296
67
 XDOT =      -7758
876120                 XDOT =       -2278
391454
 YDOT =     -23773
762162  feet/sec       YDOT =       -7272
147146  meter/sec
 ZDOT =      -3707
950612                 ZDOT =       -1141
461249

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4044288
68                 X    =         1232699
19
 Y    =       13470582
78  feet           Y    =         4105833
63  meter
 Z    =       16954833
93                 Z    =         5167833
38
 XDOT =     -21254
887791                 XDOT =       -6478
489799
 YDOT =      11131
869342  feet/sec       YDOT =        3392
993776  meter/sec
 ZDOT =      -3751
979166                 ZDOT =       -1143
603250


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
80234578  
00020000  00000-0  70000-3 0  9091
2 32699  51
6413  65
6659 0004047   4
5671 355
5529 15
75601086  2944


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08089
80234578   =   yrday
fracday
Element set:     909
Inclination:       51
6413  deg
RA of node:        65
6659  deg
Eccentricity:     
0004047     
Arg of perigee:     4
5671  deg
Mean anomaly:     355
5529  deg
Mean motion:   15
75601086  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             294
Checksum:              325

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

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