Date: June 3rd 2008

SHUTTLE TRAJECTORY DATA

Lift off time (UTC) : 2008/152/21:02:11 970 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 69 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


There are no maneuvers



Coasting Arc #1 (Orbit 30)
---------------------------------------

Vector Time (GMT): 2008/154/17:38:39
000
Vector Time (MET): 001/20:36:27
030
Weight (LBS)     : 247599
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -205777
21                 A    =         6724583
95  meter
 Y    =       -6711145
83  meter          E    =           
0007231
 Z    =         286615
08                 I    =           51
98361
 XDOT =       4738
749174                 Wp   =          145
90374
 YDOT =       -406
989843  meter/sec      RA   =           90
15610  deg
 ZDOT =      -6060
305610                 TA   =           30
99311
                                          MA   =           30
95046
                                          Ha   =            184
768  n
mi
                                          Hp   =            181
777

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -675122
08                 X    =         -132109
18
 Y    =      -22018194
97  feet           Y    =        -6713035
10  meter
 Z    =         940338
18                 Z    =          285793
05
 XDOT =      15547
077343                 XDOT =        4772
388440
 YDOT =      -1335
268514  feet/sec       YDOT =        -353
809190  meter/sec
 ZDOT =     -19882
892420                 ZDOT =       -6037
202679

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8521528
37                 X    =        -2597361
85
 Y    =       20313722
24  feet           Y    =         6191622
54  meter
 Z    =         936577
85                 Z    =          285468
93
 XDOT =     -13319
919504                 XDOT =       -4059
911465
 YDOT =      -4664
828810  feet/sec       YDOT =       -1421
839821  meter/sec
 ZDOT =     -19794
030822                 ZDOT =       -6033
220594


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 32960U 08027A   08154
76742797  
00020000  00000-0  70000-3 0  9008
2 32960  51
6369  90
7419 0006025 295
4669  64
5872 15
76665272   319


Satellite: SHUTTLE
Catalog Number: 32960
Epoch time:      08154
76742797   =   yrday
fracday
Element set:     900
Inclination:       51
6369  deg
RA of node:        90
7419  deg
Eccentricity:     
0006025     
Arg of perigee:   295
4669  deg
Mean anomaly:      64
5872  deg
Mean motion:   15
76665272  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              31
Checksum:              317


Coasting Arc #2 (Orbit 46)
---------------------------------------

Vector Time (GMT): 2008/155/17:42:59
711
Vector Time (MET): 002/20:40:47
741
Weight (LBS)     : 247599
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4007379
38                 A    =         6714397
88  meter
 Y    =       -2381405
32  meter          E    =           
0006598
 Z    =        4834421
85                 I    =           51
94822
 XDOT =       1299
452496                 Wp   =            5
58295
 YDOT =      -7184
912583  meter/sec      RA   =           84
99007  deg
 ZDOT =      -2455
387954                 TA   =          108
33030
                                          MA   =          108
25852
                                          Ha   =            184
924  n
mi
                                          Hp   =            181
671

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13147570
13                 X    =        -4003937
35
 Y    =       -7813009
60  feet           Y    =        -2426199
94  meter
 Z    =       15860964
08                 Z    =         4814961
57
 XDOT =       4263
295591                 XDOT =        1391
626733
 YDOT =     -23572
547843  feet/sec       YDOT =       -7169
865452  meter/sec
 ZDOT =      -8055
734758                 ZDOT =       -2448
852802

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9250193
96                 X    =         2819459
12
 Y    =       12276489
53  feet           Y    =         3741874
01  meter
 Z    =       15785867
66                 Z    =         4811532
46
 XDOT =     -12090
244012                 XDOT =       -3685
106375
 YDOT =      19465
302515  feet/sec       YDOT =        5933
024207  meter/sec
 ZDOT =      -8031
211083                 ZDOT =       -2447
913138


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 32960U 08027A   08155
78152934  
00020000  00000-0  70000-3 0  9010
2 32960  51
6367  85
5119 0006176 298
8471  61
2073 15
76709957   474


Satellite: SHUTTLE
Catalog Number: 32960
Epoch time:      08155
78152934   =   yrday
fracday
Element set:     901
Inclination:       51
6367  deg
RA of node:        85
5119  deg
Eccentricity:     
0006176     
Arg of perigee:   298
8471  deg
Mean anomaly:      61
2073  deg
Mean motion:   15
76709957  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              47
Checksum:              314


Coasting Arc #3 (Orbit 62)
---------------------------------------

Vector Time (GMT): 2008/156/17:47:19
397
Vector Time (MET): 003/20:45:07
427
Weight (LBS)     : 247599
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2414402
43                 A    =         6717217
55  meter
 Y    =        4737104
73  meter          E    =           
0005104
 Z    =        4100192
69                 I    =           51
95297
 XDOT =      -4001
250915                 Wp   =           80
73748
 YDOT =      -5357
916418  meter/sec      RA   =           79
88477  deg
 ZDOT =       3830
850317                 TA   =          330
10835
                                          MA   =          330
13749
                                          Ha   =            185
156  n
mi
                                          Hp   =            181
560

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7921267
83                 X    =        -2487112
15
 Y    =       15541682
17  feet           Y    =         4709698
02  meter
 Z    =       13452075
74                 Z    =         4088287
92
 XDOT =     -13127
463633                 XDOT =       -3959
650154
 YDOT =     -17578
465937  feet/sec       YDOT =       -5402
428969  meter/sec
 ZDOT =      12568
406552                 ZDOT =        3811
511941

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12909981
26                 X    =         3934962
29
 Y    =      -11783143
88  feet           Y    =        -3591502
25  meter
 Z    =       13406663
07                 Z    =         4086350
90
 XDOT =       5390
879626                 XDOT =        1643
140110
 YDOT =      20133
351219  feet/sec       YDOT =        6136
645452  meter/sec
 ZDOT =      12493
519077                 ZDOT =        3808
024615


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 32960U 08027A   08156
79562149  
00020000  00000-0  70000-3 0  9026
2 32960  51
6358  80
2819 0006206 302
8716  57
1850 15
76708850   631


Satellite: SHUTTLE
Catalog Number: 32960
Epoch time:      08156
79562149   =   yrday
fracday
Element set:     902
Inclination:       51
6358  deg
RA of node:        80
2819  deg
Eccentricity:     
0006206     
Arg of perigee:   302
8716  deg
Mean anomaly:      57
1850  deg
Mean motion:   15
76708850  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              63
Checksum:              297


Coasting Arc #4 (Orbit 77)
---------------------------------------

Vector Time (GMT): 2008/157/17:51:22
499
Vector Time (MET): 004/20:49:10
528
Weight (LBS)     : 247599
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2663170
55                 A    =         6724142
82  meter
 Y    =        6039356
36  meter          E    =           
0010833
 Z    =       -1246584
26                 I    =           51
96820
 XDOT =      -3972
939922                 Wp   =            3
00434
 YDOT =       2967
176093  meter/sec      RA   =           74
69908  deg
 ZDOT =       5900
325402                 TA   =          343
36813
                                          MA   =          343
40364
                                          Ha   =            185
380  n
mi
                                          Hp   =            181
610

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8737436
20                 X    =         2601495
26
 Y    =       19814161
29  feet           Y    =         6068792
89  meter
 Z    =       -4089843
36                 Z    =        -1233795
06
 XDOT =     -13034
579797                 XDOT =       -4034
486749
 YDOT =       9734
829701  feet/sec       YDOT =        2922
402978  meter/sec
 ZDOT =      19358
022974                 ZDOT =        5880
876036

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2065470
67                 X    =         -629555
46
 Y    =      -21565759
73  feet           Y    =        -6573243
57  meter
 Z    =       -4040103
41                 Z    =        -1231423
52
 XDOT =      13971
183521                 XDOT =        4258
416737
 YDOT =      -4942
623828  feet/sec       YDOT =       -1506
511743  meter/sec
 ZDOT =      19283
410722                 ZDOT =        5877
583588


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 32960U 08027A   08157
74639290  
00020000  00000-0  70000-3 0  9035
2 32960  51
6352  75
3793 0006107 305
2887  54
7705 15
76594006   781


Satellite: SHUTTLE
Catalog Number: 32960
Epoch time:      08157
74639290   =   yrday
fracday
Element set:     903
Inclination:       51
6352  deg
RA of node:        75
3793  deg
Eccentricity:     
0006107     
Arg of perigee:   305
2887  deg
Mean anomaly:      54
7705  deg
Mean motion:   15
76594006  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              78
Checksum:              306


Coasting Arc #5 (Orbit 93)
---------------------------------------

Vector Time (GMT): 2008/158/17:55:46
844
Vector Time (MET): 005/20:53:34
874
Weight (LBS)     : 247599
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4319816
80                 A    =         6713293
71  meter
 Y    =          44690
04  meter          E    =           
0009259
 Z    =       -5146232
79                 I    =           51
92229
 XDOT =       1588
638103                 Wp   =           82
87705
 YDOT =       7401
701195  meter/sec      RA   =           69
54901  deg
 ZDOT =       1401
058663                 TA   =          200
47125
                                          MA   =          200
50839
                                          Ha   =            185
483  n
mi
                                          Hp   =            181
513

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14172627
30                 X    =         4343995
33
 Y    =         146620
87  feet           Y    =           93132
92  meter
 Z    =      -16883965
83                 Z    =        -5125188
50
 XDOT =       5212
067268                 XDOT =        1498
946996
 YDOT =      24283
796571  feet/sec       YDOT =        7418
964487  meter/sec
 ZDOT =       4596
649156                 ZDOT =        1408
559838

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13654574
10                 X    =        -4161914
18
 Y    =       -4143257
21  feet           Y    =        -1262864
80  meter
 Z    =      -16802951
84                 Z    =        -5121539
72
 XDOT =       1532
349520                 XDOT =         467
060134
 YDOT =     -23767
794544  feet/sec       YDOT =       -7244
423777  meter/sec
 ZDOT =       4626
149978                 ZDOT =        1410
050513


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 32960U 08027A   08158
76054307  
00020000  00000-0  70000-3 0  9049
2 32960  51
6346  70
1499 0005919 309
1286  50
9351 15
76623728   943


Satellite: SHUTTLE
Catalog Number: 32960
Epoch time:      08158
76054307   =   yrday
fracday
Element set:     904
Inclination:       51
6346  deg
RA of node:        70
1499  deg
Eccentricity:     
0005919     
Arg of perigee:   309
1286  deg
Mean anomaly:      50
9351  deg
Mean motion:   15
76623728  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              94
Checksum:              302


Coasting Arc #6 (Orbit 109)
---------------------------------------

Vector Time (GMT): 2008/159/18:00:25
258
Vector Time (MET): 006/20:58:13
288
Weight (LBS)     : 247599
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         287508
69                 A    =         6719683
11  meter
 Y    =       -5736904
16  meter          E    =           
0004584
 Z    =       -3492043
32                 I    =           51
93171
 XDOT =       5409
891241                 Wp   =            8
89517
 YDOT =       3044
991302  meter/sec      RA   =           64
43547  deg
 ZDOT =      -4553
413963                 TA   =          212
39215
                                          MA   =          212
42029
                                          Ha   =            185
723  n
mi
                                          Hp   =            181
443

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         943270
00                 X    =          368601
87
 Y    =      -18821864
06  feet           Y    =        -5733235
06  meter
 Z    =      -11456835
04                 Z    =        -3490450
63
 XDOT =      17748
987011                 XDOT =        5397
559080
 YDOT =       9990
128944  feet/sec       YDOT =        3105
419635  meter/sec
 ZDOT =     -14939
022187                 ZDOT =       -4527
162340

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5576740
87                 X    =        -1699790
62
 Y    =       18005045
57  feet           Y    =         5487937
89  meter
 Z    =      -11451187
24                 Z    =        -3490321
87
 XDOT =     -13539
472837                 XDOT =       -4126
831321
 YDOT =     -13637
971483  feet/sec       YDOT =       -4156
853708  meter/sec
 ZDOT =     -14837
703191                 ZDOT =       -4522
531933


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 32960U 08027A   08159
77469545  
00020000  00000-0  70000-3 0  9056
2 32960  51
6348  64
9213 0006002 313
0864  46
9798 15
76532402  1107


Satellite: SHUTTLE
Catalog Number: 32960
Epoch time:      08159
77469545   =   yrday
fracday
Element set:     905
Inclination:       51
6348  deg
RA of node:        64
9213  deg
Eccentricity:     
0006002     
Arg of perigee:   313
0864  deg
Mean anomaly:      46
9798  deg
Mean motion:   15
76532402  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             110
Checksum:              293


Coasting Arc #7 (Orbit 125)
---------------------------------------

Vector Time (GMT): 2008/160/18:04:24
120
Vector Time (MET): 007/21:02:12
149
Weight (LBS)     : 247599
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4576980
91                 A    =         6723022
24  meter
 Y    =       -4439389
50  meter          E    =           
0008881
 Z    =        2122662
05                 I    =           51
92883
 XDOT =       2154
051288                 Wp   =           93
26849
 YDOT =      -4885
049748  meter/sec      RA   =           59
24067  deg
 ZDOT =      -5552
750251                 TA   =           63
07712
                                          MA   =           62
98641
                                          Ha   =            185
798  n
mi
                                          Hp   =            181
386

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15016341
57                 X    =        -4537310
22
 Y    =      -14564926
19  feet           Y    =        -4490350
43  meter
 Z    =        6964114
34                 Z    =         2100522
93
 XDOT =       7067
097401                 XDOT =        2235
490657
 YDOT =     -16027
066101  feet/sec       YDOT =       -4860
505739  meter/sec
 ZDOT =     -18217
684551                 ZDOT =       -5542
088850

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11650381
64                 X    =         3551036
33
 Y    =       17409227
99  feet           Y    =         5306332
69  meter
 Z    =        6878507
55                 Z    =         2096569
10
 XDOT =      -9116
069419                 XDOT =       -2778
577959
 YDOT =      13307
753542  feet/sec       YDOT =        4056
203280  meter/sec
 ZDOT =     -18177
050548                 ZDOT =       -5540
365007


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 32960U 08027A   08160
78890265  
00020000  00000-0  70000-3 0  9067
2 32960  51
6345  59
6917 0006144 315
0785  44
9882 15
76553974  1263


Satellite: SHUTTLE
Catalog Number: 32960
Epoch time:      08160
78890265   =   yrday
fracday
Element set:     906
Inclination:       51
6345  deg
RA of node:        59
6917  deg
Eccentricity:     
0006144     
Arg of perigee:   315
0785  deg
Mean anomaly:      44
9882  deg
Mean motion:   15
76553974  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             126
Checksum:              320


Coasting Arc #8 (Orbit 141)
---------------------------------------

Vector Time (GMT): 2008/161/18:09:02
610
Vector Time (MET): 008/21:06:50
640
Weight (LBS)     : 247599
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3621834
78                 A    =         6713062
44  meter
 Y    =        2048307
31  meter          E    =           
0005498
 Z    =        5269411
41                 I    =           51
87857
 XDOT =      -4242
255202                 Wp   =          346
63269
 YDOT =      -6417
762450  meter/sec      RA   =           54
10270  deg
 ZDOT =       -415
994300                 TA   =          107
33290
                                          MA   =          107
27276
                                          Ha   =            186
109  n
mi
                                          Hp   =            181
170

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11882660
02                 X    =        -3670067
83
 Y    =        6720168
33  feet           Y    =         2007535
50  meter
 Z    =       17288095
18                 Z    =         5251699
72
 XDOT =     -13918
160113                 XDOT =       -4168
154661
 YDOT =     -21055
651084  feet/sec       YDOT =       -6464
787406  meter/sec
 ZDOT =      -1364
810694                 ZDOT =        -436
423939

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12966669
84                 X    =         3952240
97
 Y    =       -4535513
93  feet           Y    =        -1382424
65  meter
 Z    =       17220078
20                 Z    =         5248679
83
 XDOT =       9707
963208                 XDOT =        2958
987186
 YDOT =      22207
376080  feet/sec       YDOT =        6768
808229  meter/sec
 ZDOT =      -1444
001703                 ZDOT =        -440
131719


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 32960U 08027A   08161
80310364  
00020000  00000-0  70000-3 0  9079
2 32960  51
6344  54
4624 0005826 320
2208  39
8529 15
76502853  1423


Satellite: SHUTTLE
Catalog Number: 32960
Epoch time:      08161
80310364   =   yrday
fracday
Element set:     907
Inclination:       51
6344  deg
RA of node:        54
4624  deg
Eccentricity:     
0005826     
Arg of perigee:   320
2208  deg
Mean anomaly:      39
8529  deg
Mean motion:   15
76502853  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             142
Checksum:              272


Coasting Arc #9 (Orbit 157)
---------------------------------------

Vector Time (GMT): 2008/162/18:13:38
515
Vector Time (MET): 009/21:11:26
545
Weight (LBS)     : 247599
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2140064
35                 A    =         6721906
71  meter
 Y    =        5741273
40  meter          E    =           
0012100
 Z    =        2746084
13                 I    =           51
89069
 XDOT =      -5697
783767                 Wp   =           53
85678
 YDOT =       -358
224076  meter/sec      RA   =           48
97565  deg
 ZDOT =       5180
578854                 TA   =          337
46103
                                          MA   =          337
51414
                                          Ha   =            186
181  n
mi
                                          Hp   =            181
149

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7021208
51                 X    =         2062365
50
 Y    =       18836198
82  feet           Y    =         5764770
06  meter
 Z    =        9009462
38                 Z    =         2756292
53
 XDOT =     -18693
516296                 XDOT =       -5718
520880
 YDOT =      -1175
275840  feet/sec       YDOT =        -422
056534  meter/sec
 ZDOT =      16996
649783                 ZDOT =        5152
848614

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4324538
52                 X    =        -1318119
34
 Y    =      -19613254
46  feet           Y    =        -5978119
96  meter
 Z    =        9049242
14                 Z    =         2758209
01
 XDOT =      17021
870268                 XDOT =        5188
266058
 YDOT =       4052
710075  feet/sec       YDOT =        1235
266031  meter/sec
 ZDOT =      16889
860715                 ZDOT =        5148
029546


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 32960U 08027A   08162
81730915  
00020000  00000-0  70000-3 0  9080
2 32960  51
6354  49
2337 0005855 322
6524  37
4233 15
76457400  1586


Satellite: SHUTTLE
Catalog Number: 32960
Epoch time:      08162
81730915   =   yrday
fracday
Element set:     908
Inclination:       51
6354  deg
RA of node:        49
2337  deg
Eccentricity:     
0005855     
Arg of perigee:   322
6524  deg
Mean anomaly:      37
4233  deg
Mean motion:   15
76457400  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             158
Checksum:              286


Coasting Arc #10 (Orbit 172)
---------------------------------------

Vector Time (GMT): 2008/163/18:18:25
852
Vector Time (MET): 010/21:16:13
881
Weight (LBS)     : 247599
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5635935
70                 A    =         6722085
36  meter
 Y    =        2455623
16  meter          E    =           
0007702
 Z    =       -2708667
16                 I    =           51
87208
 XDOT =         22
670482                 Wp   =            6
01642
 YDOT =       5680
556811  meter/sec      RA   =           43
77512  deg
 ZDOT =       5205
870614                 TA   =          323
14893
                                          MA   =          323
20184
                                          Ha   =            186
416  n
mi
                                          Hp   =            181
025

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18490602
71                 X    =         5621215
93
 Y    =        8056506
42  feet           Y    =         2518565
45  meter
 Z    =       -8886703
28                 Z    =        -2681323
13
 XDOT =         74
378222                 XDOT =         -66
141356
 YDOT =      18636
997410  feet/sec       YDOT =        5680
313116  meter/sec
 ZDOT =      17079
627998                 ZDOT =        5205
765717

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17651671
70                 X    =        -5380229
53
 Y    =       -9853510
65  feet           Y    =        -3003350
04  meter
 Z    =       -8781229
61                 Z    =        -2676518
78
 XDOT =       1150
497407                 XDOT =         350
671610
 YDOT =     -17255
951761  feet/sec       YDOT =       -5259
614097  meter/sec
 ZDOT =      17079
692394                 ZDOT =        5205
890242


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 32960U 08027A   08163
76817713  
00020000  00000-0  70000-3 0  9098
2 32960  51
6366  44
3327 0005832 326
7772  33
3025 15
76450177  1734


Satellite: SHUTTLE
Catalog Number: 32960
Epoch time:      08163
76817713   =   yrday
fracday
Element set:     909
Inclination:       51
6366  deg
RA of node:        44
3327  deg
Eccentricity:     
0005832     
Arg of perigee:   326
7772  deg
Mean anomaly:      33
3025  deg
Mean motion:   15
76450177  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             173
Checksum:              292

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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