Date: February 17th 2008

SHUTTLE TRAJECTORY DATA

Lift off time (UTC) : 2008/038/19:45:29 952 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 65 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : -0 31789

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


049/10:41:35 731 1 1 -0 0 3 0
010/14:56:05 779 2 4 0 0 187 7
000/00:00:11 559 1 5 -3 0 175 5

049/11:09:35 729 0 5 -3 0 3 0
010/15:24:05 777 2 8 0 0 187 7
000/00:00:11 554 0 8 0 0 173 7

Coasting Arc #1 (Orbit 123)
---------------------------------------

Vector Time (GMT): 2008/046/12:47:18
000
Vector Time (MET): 007/17:01:48
048
Weight (LBS)     : 217404
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         560746
52                 A    =         6716303
29  meter
 Y    =        5987838
44  meter          E    =           
0017344
 Z    =        2978631
32                 I    =           51
33862
 XDOT =      -5121
501891                 Wp   =           80
97655
 YDOT =       2954
335625  meter/sec      RA   =          287
99371  deg
 ZDOT =      -4947
695806                 TA   =           64
38557
                                          MA   =           64
20645
                                          Ha   =            185
396  n
mi
                                          Hp   =            175
718

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1839719
54                 X    =          479417
42
 Y    =       19645139
24  feet           Y    =         5993642
30  meter
 Z    =        9772412
48                 Z    =         2981157
71
 XDOT =     -16802
827726                 XDOT =       -5130
055308
 YDOT =       9692
702182  feet/sec       YDOT =        2897
134962  meter/sec
 ZDOT =     -16232
597788                 ZDOT =       -4972
596499

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6363947
41                 X    =        -1939731
17
 Y    =       18671233
30  feet           Y    =         5690991
91  meter
 Z    =        9782705
65                 Z    =         2981768
68
 XDOT =     -17847
115323                 XDOT =       -5439
800750
 YDOT =       2518
304757  feet/sec       YDOT =         767
579290  meter/sec
 ZDOT =     -16327
549080                 ZDOT =       -4976
636960


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 32486U 08005A   08046
57063319  
00014500  00000-0  95600-3 0  9003
2 32486  51
6403 288
4877 0005801  42
9338 317
2288 15
78233922  1241


Satellite: SHUTTLE
Catalog Number: 32486
Epoch time:      08046
57063319   =   yrday
fracday
Element set:     900
Inclination:       51
6403  deg
RA of node:       288
4877  deg
Eccentricity:     
0005801     
Arg of perigee:    42
9338  deg
Mean anomaly:     317
2288  deg
Mean motion:   15
78233922  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             124
Checksum:              305


Coasting Arc #2 (Orbit 139)
---------------------------------------

Vector Time (GMT): 2008/047/12:50:46
617
Vector Time (MET): 008/17:05:16
665
Weight (LBS)     : 784954
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4212307
58                 A    =         6710196
55  meter
 Y    =         292514
94  meter          E    =           
0009005
 Z    =        5208304
97                 I    =           51
30289
 XDOT =      -1245
921020                 Wp   =           55
85214
 YDOT =       7589
527275  meter/sec      RA   =          282
82003  deg
 ZDOT =        585
684124                 TA   =           28
58941
                                          MA   =           28
54006
                                          Ha   =            187
026  n
mi
                                          Hp   =            176
303

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13819906
74                 X    =         4183430
98
 Y    =         959694
68  feet           Y    =          339360
70  meter
 Z    =       17087614
75                 Z    =         5228697
77
 XDOT =      -4087
667390                 XDOT =       -1333
365176
 YDOT =      24900
023869  feet/sec       YDOT =        7575
135658  meter/sec
 ZDOT =       1921
535839                 ZDOT =         579
419026

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12347859
67                 X    =         3763627
63
 Y    =        6063631
44  feet           Y    =         1848194
86  meter
 Z    =       17165667
75                 Z    =         5232095
53
 XDOT =     -12743
413031                 XDOT =       -3884
192292
 YDOT =      20615
833961  feet/sec       YDOT =        6283
706191  meter/sec
 ZDOT =       1898
368290                 ZDOT =         578
622655


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 32486U 08005A   08047
58377434  
00014500  00000-0  95600-3 0  9012
2 32486  51
6397 283
2519 0007907  38
3491 321
8234 15
77528618  1405


Satellite: SHUTTLE
Catalog Number: 32486
Epoch time:      08047
58377434   =   yrday
fracday
Element set:     901
Inclination:       51
6397  deg
RA of node:       283
2519  deg
Eccentricity:     
0007907     
Arg of perigee:    38
3491  deg
Mean anomaly:     321
8234  deg
Mean motion:   15
77528618  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             140
Checksum:              318


Coasting Arc #3 (Orbit 155)
---------------------------------------

Vector Time (GMT): 2008/048/12:54:39
373
Vector Time (MET): 009/17:09:09
421
Weight (LBS)     : 217404
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2405826
25                 A    =         6720416
91  meter
 Y    =       -5936616
53  meter          E    =           
0021519
 Z    =        1994195
63                 I    =           51
33102
 XDOT =       4024
080025                 Wp   =           59
12265
 YDOT =       3511
959594  meter/sec      RA   =          277
63378  deg
 ZDOT =       5566
858174                 TA   =          323
25529
                                          MA   =          323
40263
                                          Ha   =            187
162  n
mi
                                          Hp   =            176
155

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7893130
73                 X    =         2462207
45
 Y    =      -19477088
36  feet           Y    =        -5909454
33  meter
 Z    =        6542636
58                 Z    =         2006019
95
 XDOT =      13202
362286                 XDOT =        3957
550073
 YDOT =      11522
177147  feet/sec       YDOT =        3556
494830  meter/sec
 ZDOT =      18263
970387                 ZDOT =        5586
244902

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14096974
03                 X    =         4296757
68
 Y    =      -15567533
94  feet           Y    =        -4744984
35  meter
 Z    =        6587244
30                 Z    =         2007792
06
 XDOT =       7180
330533                 XDOT =        2188
564746
 YDOT =      14307
805703  feet/sec       YDOT =        4361
019178  meter/sec
 ZDOT =      18338
525532                 ZDOT =        5589
582582


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 32486U 08005A   08048
59736377  
00014500  00000-0  95600-3 0  9020
2 32486  51
6385 278
0190 0007917  42
4310 317
7466 15
77540346  1566


Satellite: SHUTTLE
Catalog Number: 32486
Epoch time:      08048
59736377   =   yrday
fracday
Element set:     902
Inclination:       51
6385  deg
RA of node:       278
0190  deg
Eccentricity:     
0007917     
Arg of perigee:    42
4310  deg
Mean anomaly:     317
7466  deg
Mean motion:   15
77540346  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             156
Checksum:              317


Coasting Arc #4 (Orbit 169)
---------------------------------------

Vector Time (GMT): 2008/049/10:41:41
511
Vector Time (MET): 010/14:56:11
559
Weight (LBS)     : 217328
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2380305
82                 A    =         6717273
42  meter
 Y    =        5335428
93  meter          E    =           
0020449
 Z    =        3304675
41                 I    =           51
31938
 XDOT =      -3973
613066                 Wp   =           72
49655
 YDOT =       4679
359344  meter/sec      RA   =          272
88368  deg
 ZDOT =      -4662
989145                 TA   =           68
40277
                                          MA   =           68
18502
                                          Ha   =            187
696  n
mi
                                          Hp   =            175
523

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7809402
31                 X    =         2304538
59
 Y    =       17504688
10  feet           Y    =         5361569
11  meter
 Z    =       10842110
94                 Z    =         3316054
26
 XDOT =     -13036
788273                 XDOT =       -4002
884371
 YDOT =      15352
228818  feet/sec       YDOT =        4634
852679  meter/sec
 ZDOT =     -15298
520816                 ZDOT =       -4682
363696

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9183197
38                 X    =        -2799038
56
 Y    =       16796162
50  feet           Y    =         5119470
33  meter
 Z    =       10886232
15                 Z    =         3318123
56
 XDOT =     -18837
650714                 XDOT =       -5741
715938
 YDOT =       -273
090542  feet/sec       YDOT =         -83
237997  meter/sec
 ZDOT =     -15372
150479                 ZDOT =       -4685
431466


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 32486U 08005A   08049
48423772  
00014500  00000-0  95600-3 0  9032
2 32486  51
6396 273
4414 0009340  47
0597 313
1350 15
77565927  1706


Satellite: SHUTTLE
Catalog Number: 32486
Epoch time:      08049
48423772   =   yrday
fracday
Element set:     903
Inclination:       51
6396  deg
RA of node:       273
4414  deg
Eccentricity:     
0009340     
Arg of perigee:    47
0597  deg
Mean anomaly:     313
1350  deg
Mean motion:   15
77565927  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             170
Checksum:              309


Coasting Arc #5 (Orbit 169)
---------------------------------------

Vector Time (GMT): 2008/049/11:09:41
506
Vector Time (MET): 010/15:24:11
554
Weight (LBS)     : 217253
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4082669
45                 A    =         6709638
08  meter
 Y    =        1969695
39  meter          E    =           
0023962
 Z    =       -4968470
99                 I    =           51
29882
 XDOT =      -1188
237509                 Wp   =           64
10101
 YDOT =      -7346
871025  meter/sec      RA   =          272
82412  deg
 ZDOT =      -1933
106926                 TA   =          187
08973
                                          MA   =          187
12368
                                          Ha   =            187
656  n
mi
                                          Hp   =            173
725

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13394584
80                 X    =        -4080211
67
 Y    =        6462255
20  feet           Y    =         1924148
74  meter
 Z    =      -16300757
83                 Z    =        -4988298
11
 XDOT =      -3898
417023                 XDOT =       -1096
775561
 YDOT =     -24103
907563  feet/sec       YDOT =       -7359
620803  meter/sec
 ZDOT =      -6342
214323                 ZDOT =       -1938
656655

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13930699
08                 X    =        -4246077
08
 Y    =       -4963773
83  feet           Y    =        -1512958
26  meter
 Z    =      -16376413
61                 Z    =        -4991530
87
 XDOT =      14130
871277                 XDOT =        4307
089565
 YDOT =     -18627
827046  feet/sec       YDOT =       -5677
761683  meter/sec
 ZDOT =      -6364
248772                 ZDOT =       -1939
823026


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 32486U 08005A   08049
48423442  
00014500  00000-0  95600-3 0  9047
2 32486  51
6394 273
4411 0011415  51
1964 309
0219 15
78126882  1703


Satellite: SHUTTLE
Catalog Number: 32486
Epoch time:      08049
48423442   =   yrday
fracday
Element set:     904
Inclination:       51
6394  deg
RA of node:       273
4411  deg
Eccentricity:     
0011415     
Arg of perigee:    51
1964  deg
Mean anomaly:     309
0219  deg
Mean motion:   15
78126882  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             170
Checksum:              291


Coasting Arc #6 (Orbit 185)
---------------------------------------

Vector Time (GMT): 2008/050/11:12:54
201
Vector Time (MET): 011/15:27:24
249
Weight (LBS)     : 217253
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -393169
91                 A    =         6720254
54  meter
 Y    =        6656895
65  meter          E    =           
0015851
 Z    =        -837197
53                 I    =           51
33387
 XDOT =      -4797
442619                 Wp   =           95
91807
 YDOT =      -1017
741695  meter/sec      RA   =          267
61449  deg
 ZDOT =      -5937
311632                 TA   =           93
26202
                                          MA   =           93
08066
                                          Ha   =            187
709  n
mi
                                          Hp   =            173
845

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1289927
51                 X    =         -463358
10
 Y    =       21840208
82  feet           Y    =         6652116
41  meter
 Z    =       -2746711
06                 Z    =         -839278
51
 XDOT =     -15739
641139                 XDOT =       -4756
888910
 YDOT =      -3339
047557  feet/sec       YDOT =       -1071
052430  meter/sec
 ZDOT =     -19479
368871                 ZDOT =       -5960
518253

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16018744
35                 X    =        -4882513
28
 Y    =       14900292
18  feet           Y    =         4541609
06  meter
 Z    =       -2753938
65                 Z    =         -839400
50
 XDOT =      -7898
348888                 XDOT =       -2407
416741
 YDOT =     -12048
743563  feet/sec       YDOT =       -3672
457038  meter/sec
 ZDOT =     -19568
288517                 ZDOT =       -5964
414340


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 32486U 08005A   08050
49741707  
00014500  00000-0  95600-3 0  9058
2 32486  51
6390 268
2060 0011280  55
6583 304
5648 15
78096188  1865


Satellite: SHUTTLE
Catalog Number: 32486
Epoch time:      08050
49741707   =   yrday
fracday
Element set:     905
Inclination:       51
6390  deg
RA of node:       268
2060  deg
Eccentricity:     
0011280     
Arg of perigee:    55
6583  deg
Mean anomaly:     304
5648  deg
Mean motion:   15
78096188  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             186
Checksum:              314


Coasting Arc #7 (Orbit 201)
---------------------------------------

Vector Time (GMT): 2008/051/11:16:27
926
Vector Time (MET): 012/15:30:57
974
Weight (LBS)     : 217253
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3808338
72                 A    =         6712829
31  meter
 Y    =        3693860
10  meter          E    =           
0021508
 Z    =        4101656
82                 I    =           51
31191
 XDOT =      -2158
956413                 Wp   =           66
12933
 YDOT =       6396
203937  meter/sec      RA   =          262
37660  deg
 ZDOT =      -3731
725074                 TA   =           62
28111
                                          MA   =           62
06310
                                          Ha   =            187
534  n
mi
                                          Hp   =            173
592

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12494549
62                 X    =         3746912
50
 Y    =       12118963
58  feet           Y    =         3736016
54  meter
 Z    =       13456879
33                 Z    =         4120007
53
 XDOT =      -7083
190330                 XDOT =       -2212
044124
 YDOT =      20984
921052  feet/sec       YDOT =        6371
814680  meter/sec
 ZDOT =     -12243
192499                 ZDOT =       -3742
342594

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1163445
55                 X    =          354618
20
 Y    =       17312515
03  feet           Y    =         5276854
58  meter
 Z    =       13527522
60                 Z    =         4123188
89
 XDOT =     -17963
513688                 XDOT =       -5475
278972
 YDOT =      10866
048050  feet/sec       YDOT =        3311
971446  meter/sec
 ZDOT =     -12283
105947                 ZDOT =       -3743
890693


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 32486U 08005A   08051
51058606  
00014500  00000-0  95600-3 0  9062
2 32486  51
6385 262
9698 0011357  57
7803 302
4461 15
78204990  2021


Satellite: SHUTTLE
Catalog Number: 32486
Epoch time:      08051
51058606   =   yrday
fracday
Element set:     906
Inclination:       51
6385  deg
RA of node:       262
9698  deg
Eccentricity:     
0011357     
Arg of perigee:    57
7803  deg
Mean anomaly:     302
4461  deg
Mean motion:   15
78204990  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             202
Checksum:              304


Coasting Arc #8 (Orbit 217)
---------------------------------------

Vector Time (GMT): 2008/052/11:20:08
664
Vector Time (MET): 013/15:34:38
712
Weight (LBS)     : 217253
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3230497
58                 A    =         6709996
13  meter
 Y    =       -3309547
57  meter          E    =           
0015762
 Z    =        4847486
00                 I    =           51
30589
 XDOT =       3346
794234                 Wp   =           83
43421
 YDOT =       6579
442215  meter/sec      RA   =          257
21579  deg
 ZDOT =       2257
143060                 TA   =          344
53930
                                          MA   =          344
58740
                                          Ha   =            187
635  n
mi
                                          Hp   =            173
560

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10598745
35                 X    =         3243641
94
 Y    =      -10858095
71  feet           Y    =        -3273423
21  meter
 Z    =       15903825
45                 Z    =         4863211
67
 XDOT =      10980
296044                 XDOT =        3262
162044
 YDOT =      21586
096507  feet/sec       YDOT =        6616
318474  meter/sec
 ZDOT =       7405
324999                 ZDOT =        2273
194879

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15027902
89                 X    =         4580504
80
 Y    =       -1577318
46  feet           Y    =         -480766
67  meter
 Z    =       15963630
87                 Z    =         4865714
69
 XDOT =      -5588
943167                 XDOT =       -1703
509877
 YDOT =      22476
118328  feet/sec       YDOT =        6850
720866  meter/sec
 ZDOT =       7467
508386                 ZDOT =        2276
096556


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 32486U 08005A   08052
52373974  
00014500  00000-0  95600-3 0  9073
2 32486  51
6373 257
7336 0011412  62
1120 298
1199 15
78165530  2185


Satellite: SHUTTLE
Catalog Number: 32486
Epoch time:      08052
52373974   =   yrday
fracday
Element set:     907
Inclination:       51
6373  deg
RA of node:       257
7336  deg
Eccentricity:     
0011412     
Arg of perigee:    62
1120  deg
Mean anomaly:     298
1199  deg
Mean motion:   15
78165530  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             218
Checksum:              299


Coasting Arc #9 (Orbit 233)
---------------------------------------

Vector Time (GMT): 2008/053/11:23:21
488
Vector Time (MET): 014/15:37:51
536
Weight (LBS)     : 217253
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1655157
91                 A    =         6720088
62  meter
 Y    =       -6480517
05  meter          E    =           
0024222
 Z    =         535693
26                 I    =           51
34740
 XDOT =       4805
120388                 Wp   =           57
51355
 YDOT =       -716
886755  meter/sec      RA   =          251
99997  deg
 ZDOT =       5990
883144                 TA   =          308
35399
                                          MA   =          308
57141
                                          Ha   =            187
575  n
mi
                                          Hp   =            173
448

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5430308
12                 X    =        -1585321
64
 Y    =      -21261538
89  feet           Y    =        -6498597
86  meter
 Z    =        1757523
81                 Z    =          527823
28
 XDOT =      15764
830670                 XDOT =        4783
662287
 YDOT =      -2351
990667  feet/sec       YDOT =        -663
383386  meter/sec
 ZDOT =      19655
128424                 ZDOT =        6014
173843

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8857232
43                 X    =         2699684
45
 Y    =      -20079797
56  feet           Y    =        -6120322
30  meter
 Z    =        1726654
47                 Z    =          526284
28
 XDOT =      12297
602238                 XDOT =        3748
309162
 YDOT =       7174
907670  feet/sec       YDOT =        2186
911858  meter/sec
 ZDOT =      19744
182700                 ZDOT =        6018
026887


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 32486U 08005A   08053
53686777  
00014500  00000-0  95600-3 0  9084
2 32486  51
6363 252
4969 0011220  65
7382 294
4954 15
78236995  2344


Satellite: SHUTTLE
Catalog Number: 32486
Epoch time:      08053
53686777   =   yrday
fracday
Element set:     908
Inclination:       51
6363  deg
RA of node:       252
4969  deg
Eccentricity:     
0011220     
Arg of perigee:    65
7382  deg
Mean anomaly:     294
4954  deg
Mean motion:   15
78236995  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             234
Checksum:              339


Coasting Arc #10 (Orbit 248)
---------------------------------------

Vector Time (GMT): 2008/054/11:26:55
007
Vector Time (MET): 015/15:41:25
055
Weight (LBS)     : 217253
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4681943
93                 A    =         6712050
78  meter
 Y    =       -2236288
67  meter          E    =           
0018691
 Z    =       -4273502
16                 I    =           51
33013
 XDOT =         98
950160                 Wp   =           87
53589
 YDOT =      -6855
660911  meter/sec      RA   =          246
76564  deg
 ZDOT =       3493
035941                 TA   =          217
94809
                                          MA   =          218
07995
                                          Ha   =            187
538  n
mi
                                          Hp   =            173
236

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15360708
43                 X    =        -4635882
96
 Y    =       -7336905
09  feet           Y    =        -2288279
96  meter
 Z    =      -14020676
38                 Z    =        -4296134
39
 XDOT =        324
639632                 XDOT =         158
476761
 YDOT =     -22492
325823  feet/sec       YDOT =       -6854
224009  meter/sec
 ZDOT =      11460
091669                 ZDOT =        3493
662274

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7977857
24                 X    =        -2431650
89
 Y    =      -14956321
75  feet           Y    =        -4558686
87  meter
 Z    =      -14107556
11                 Z    =        -4299983
10
 XDOT =      12427
184380                 XDOT =        3787
805799
 YDOT =     -17397
181579  feet/sec       YDOT =       -5302
660945  meter/sec
 ZDOT =      11461
688524                 ZDOT =        3493
522662


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 32486U 08005A   08054
48665752  
00014500  00000-0  95600-3 0  9090
2 32486  51
6354 247
5868 0011199  69
4421 290
7945 15
78250395  2492


Satellite: SHUTTLE
Catalog Number: 32486
Epoch time:      08054
48665752   =   yrday
fracday
Element set:     909
Inclination:       51
6354  deg
RA of node:       247
5868  deg
Eccentricity:     
0011199     
Arg of perigee:    69
4421  deg
Mean anomaly:     290
7945  deg
Mean motion:   15
78250395  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             249
Checksum:              343

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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