Date: July 11th 2006

SHUTTLE TRAJECTORY DATA

Lift off time (UTC) : 2006/185/18:37:54 951 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 79 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 22 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 19144

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


196/10:36:58 213 1 2 0 4 1 6
010/15:59:03 262 1 0 -0 0 190 1
000/00:00:06 524 -0 0 -1 5 176 9

196/11:04:57 052 -0 7 1 0 1 0
010/16:27:02 101 -0 7 -0 0 190 7
000/00:00:04 202 -0 1 -0 0 176 9

196/19:23:29 469 -0 6 -0 7 0 7
011/00:45:34 518 -0 4 -0 0 190 6
000/00:00:03 115 0 1 -0 0 176 5

197/09:47:55 045 0 6 -0 7 0 7
011/15:10:00 093 0 3 0 0 190 3
000/00:00:03 021 -0 2 -0 0 176 4

197/17:58:55 823 -31 2 -47 0 47 0
011/23:21:00 872 10 5 -0 0 188 1
000/00:00:31 005 33 6 0 1 152 6

Coasting Arc #1 (begining on orbit 94)
---------------------------------------

Vector Time (GMT): 2006/191/15:10:49
000
Vector Time (MET): 005/20:32:54
049
Weight (LBS)     : 219138
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         393370
15                 A    =         6722590
89  meter
 Y    =        6127105
84  meter          E    =           
0023655
 Z    =        2707844
48                 I    =           51
92607
 XDOT =      -5336
648500                 Wp   =           70
50370
 YDOT =      -1972
430070  meter/sec      RA   =           66
11465  deg
 ZDOT =       5209
511591                 TA   =          320
33404
                                          MA   =          320
50682
                                          Ha   =            190
261  n
mi
                                          Hp   =            176
897

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1290584
48                 X    =          311587
18
 Y    =       20102053
27  feet           Y    =         6131051
65  meter
 Z    =        8884004
20                 Z    =         2709558
42
 XDOT =     -17508
689306                 XDOT =       -5339
473999
 YDOT =      -6471
227263  feet/sec       YDOT =       -2032
199104  meter/sec
 ZDOT =      17091
573461                 ZDOT =        5183
579152

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7244548
44                 X    =         2208138
36
 Y    =      -18792247
15  feet           Y    =        -5727876
93  meter
 Z    =        8891099
46                 Z    =         2710007
12
 XDOT =      11936
539709                 XDOT =        3638
257303
 YDOT =      12687
122365  feet/sec       YDOT =        3867
034897  meter/sec
 ZDOT =      16995
076072                 ZDOT =        5180
099187


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 29251U 06028A   06191
69046264  
00014500  00000-0  95600-4 0  9005
2 29251  51
6289  66
4160 0010327  60
0014 300
2174 15
76246560   952


Satellite: SHUTTLE
Catalog Number: 29251
Epoch time:      06191
69046264   =   yrday
fracday
Element set:     900
Inclination:       51
6289  deg
RA of node:        66
4160  deg
Eccentricity:     
0010327     
Arg of perigee:    60
0014  deg
Mean anomaly:     300
2174  deg
Mean motion:   15
76246560  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:              95
Checksum:              264


Coasting Arc #2 (begining on orbit 109)
---------------------------------------

Vector Time (GMT): 2006/192/15:15:15
602
Vector Time (MET): 006/20:37:20
650
Weight (LBS)     : 219138
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4723779
41                 A    =         6722130
52  meter
 Y    =        3794910
28  meter          E    =           
0014986
 Z    =       -2913595
06                 I    =           51
91147
 XDOT =      -1412
329455                 Wp   =           64
07218
 YDOT =       5625
156140  meter/sec      RA   =           60
91736  deg
 ZDOT =       5063
284057                 TA   =          262
52004
                                          MA   =          262
69034
                                          Ha   =            190
339  n
mi
                                          Hp   =            176
833

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15497963
95                 X    =         4695092
84
 Y    =       12450493
04  feet           Y    =         3847640
24  meter
 Z    =       -9559038
91                 Z    =        -2890716
15
 XDOT =      -4633
626821                 XDOT =       -1499
800042
 YDOT =      18455
236681  feet/sec       YDOT =        5608
852046  meter/sec
 ZDOT =      16611
824334                 ZDOT =        5056
212030

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9596653
14                 X    =        -2925059
88
 Y    =      -17456548
92  feet           Y    =        -5320756
11  meter
 Z    =       -9473649
59                 Z    =        -2887568
40
 XDOT =      10159
308122                 XDOT =        3096
557116
 YDOT =     -14538
931190  feet/sec       YDOT =       -4431
466227  meter/sec
 ZDOT =      16586
244451                 ZDOT =        5055
487309


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 29251U 06028A   06192
64145184  
00014500  00000-0  95600-4 0  9013
2 29251  51
6285  61
5140 0010388  64
0512 296
1721 15
76252688  1103


Satellite: SHUTTLE
Catalog Number: 29251
Epoch time:      06192
64145184   =   yrday
fracday
Element set:     901
Inclination:       51
6285  deg
RA of node:        61
5140  deg
Eccentricity:     
0010388     
Arg of perigee:    64
0512  deg
Mean anomaly:     296
1721  deg
Mean motion:   15
76252688  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             110
Checksum:              273


Coasting Arc #3 (begining on orbit 125)
---------------------------------------

Vector Time (GMT): 2006/193/15:19:52
862
Vector Time (MET): 007/20:41:57
911
Weight (LBS)     : 219138
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2978446
33                 A    =         6713725
14  meter
 Y    =       -2961670
07  meter          E    =           
0025010
 Z    =       -5258908
00                 I    =           51
86848
 XDOT =       4743
175252                 Wp   =           77
73970
 YDOT =       6007
980994  meter/sec      RA   =           55
79524  deg
 ZDOT =       -694
745126                 TA   =          185
64757
                                          MA   =          185
67583
                                          Ha   =            190
279  n
mi
                                          Hp   =            176
700

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9771805
54                 X    =         3036929
84
 Y    =       -9716765
31  feet           Y    =        -2927993
31  meter
 Z    =      -17253635
19                 Z    =        -5244297
65
 XDOT =      15561
598597                 XDOT =        4678
930937
 YDOT =      19711
223734  feet/sec       YDOT =        6060
728498  meter/sec
 ZDOT =      -2279
347527                 ZDOT =        -671
858065

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12631971
97                 X    =        -3850225
06
 Y    =        5673936
92  feet           Y    =         1729415
97  meter
 Z    =      -17199748
91                 Z    =        -5242483
47
 XDOT =      -7323
718551                 XDOT =       -2232
269414
 YDOT =     -22978
874243  feet/sec       YDOT =       -7003
960869  meter/sec
 ZDOT =      -2193
653332                 ZDOT =        -668
625535


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 29251U 06028A   06193
65581613  
00014500  00000-0  95600-4 0  9027
2 29251  51
6284  56
2857 0010438  68
2991 291
9283 15
76296385  1266


Satellite: SHUTTLE
Catalog Number: 29251
Epoch time:      06193
65581613   =   yrday
fracday
Element set:     902
Inclination:       51
6284  deg
RA of node:        56
2857  deg
Eccentricity:     
0010438     
Arg of perigee:    68
2991  deg
Mean anomaly:     291
9283  deg
Mean motion:   15
76296385  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             126
Checksum:              320


Coasting Arc #4 (begining on orbit 141)
---------------------------------------

Vector Time (GMT): 2006/194/15:24:26
675
Vector Time (MET): 008/20:46:31
723
Weight (LBS)     : 219138
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2901404
37                 A    =         6724027
62  meter
 Y    =       -5788996
37  meter          E    =           
0014577
 Z    =       -1818640
07                 I    =           51
88696
 XDOT =       5122
495460                 Wp   =           98
85189
 YDOT =       -792
542105  meter/sec      RA   =           50
65240  deg
 ZDOT =      -5690
210834                 TA   =          101
24834
                                          MA   =          101
08447
                                          Ha   =            190
214  n
mi
                                          Hp   =            176
508

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9519043
20                 X    =        -2827539
72
 Y    =      -18992770
23  feet           Y    =        -5821068
12  meter
 Z    =       -5966666
90                 Z    =        -1832556
41
 XDOT =      16806
087468                 XDOT =        5158
628666
 YDOT =      -2600
203755  feet/sec       YDOT =        -734
984696  meter/sec
 ZDOT =     -18668
670715                 ZDOT =       -5665
238728

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3063426
54                 X    =          933732
41
 Y    =       21007742
41  feet           Y    =         6403159
89  meter
 Z    =       -6019036
07                 Z    =        -1834602
19
 XDOT =     -15340
566029                 XDOT =       -4675
804526
 YDOT =      -3047
366038  feet/sec       YDOT =        -928
837168  meter/sec
 ZDOT =     -18576
050373                 ZDOT =       -5661
980154


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 29251U 06028A   06194
67016022  
00014500  00000-0  95600-4 0  9038
2 29251  51
6286  51
0563 0010446  71
0545 289
1750 15
76347875  1428


Satellite: SHUTTLE
Catalog Number: 29251
Epoch time:      06194
67016022   =   yrday
fracday
Element set:     903
Inclination:       51
6286  deg
RA of node:        51
0563  deg
Eccentricity:     
0010446     
Arg of perigee:    71
0545  deg
Mean anomaly:     289
1750  deg
Mean motion:   15
76347875  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             142
Checksum:              283


Coasting Arc #5 (begining on orbit 157)
---------------------------------------

Vector Time (GMT): 2006/195/15:28:58
094
Vector Time (MET): 009/20:51:03
143
Weight (LBS)     : 219138
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5449467
85                 A    =         6719928
54  meter
 Y    =       -1471585
98  meter          E    =           
0022249
 Z    =        3630601
25                 I    =           51
85321
 XDOT =      -1268
342653                 Wp   =           80
99060
 YDOT =      -6208
728429  meter/sec      RA   =           45
45481  deg
 ZDOT =      -4394
213062                 TA   =           55
54823
                                          MA   =           55
33819
                                          Ha   =            190
327  n
mi
                                          Hp   =            176
579

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17878831
52                 X    =        -5450222
40
 Y    =       -4828038
01  feet           Y    =        -1532605
80  meter
 Z    =       11911421
41                 Z    =         3604126
22
 XDOT =      -4161
229177                 XDOT =       -1177
388845
 YDOT =     -20369
843928  feet/sec       YDOT =       -6222
419571  meter/sec
 ZDOT =     -14416
709522                 ZDOT =       -4400
154591

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15897290
97                 X    =         4845494
29
 Y    =        9621590
81  feet           Y    =         2932660
88  meter
 Z    =       11812944
50                 Z    =         3600585
48
 XDOT =      -1034
067328                 XDOT =        -315
183722
 YDOT =      19542
814347  feet/sec       YDOT =        5956
649813  meter/sec
 ZDOT =     -14439
524390                 ZDOT =       -4401
167034


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 29251U 06028A   06195
68449239  
00014500  00000-0  95600-4 0  9041
2 29251  51
6282  45
8271 0010290  76
0188 284
2119 15
76318021  1589


Satellite: SHUTTLE
Catalog Number: 29251
Epoch time:      06195
68449239   =   yrday
fracday
Element set:     904
Inclination:       51
6282  deg
RA of node:        45
8271  deg
Eccentricity:     
0010290     
Arg of perigee:    76
0188  deg
Mean anomaly:     284
2119  deg
Mean motion:   15
76318021  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             158
Checksum:              297


Coasting Arc #6 (begining on orbit 169)
---------------------------------------

Vector Time (GMT): 2006/196/10:37:01
475
Vector Time (MET): 010/15:59:06
524
Weight (LBS)     : 237059
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5614749
07                 A    =         6724750
33  meter
 Y    =        3376868
72  meter          E    =           
0017151
 Z    =       -1499030
68                 I    =           51
85690
 XDOT =      -1386
883185                 Wp   =           56
16183
 YDOT =       4861
008106  meter/sec      RA   =           41
37456  deg
 ZDOT =       5812
215938                 TA   =          287
36419
                                          MA   =          287
55170
                                          Ha   =            190
070  n
mi
                                          Hp   =            176
904

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18421092
74                 X    =         5583805
05
 Y    =       11078965
62  feet           Y    =         3439561
30  meter
 Z    =       -4918079
66                 Z    =        -1471829
38
 XDOT =      -4550
141684                 XDOT =       -1469
438400
 YDOT =      15948
189324  feet/sec       YDOT =        4845
016865  meter/sec
 ZDOT =      19068
949928                 ZDOT =        5805
278740

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10534775
82                 X    =         3210999
67
 Y    =      -18763949
35  feet           Y    =        -5719251
76  meter
 Z    =       -4816673
93                 Z    =        -1468122
21
 XDOT =      14709
051627                 XDOT =        4483
318936
 YDOT =       3418
289683  feet/sec       YDOT =        1041
894695  meter/sec
 ZDOT =      19043
784964                 ZDOT =        5804
545657


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 29251U 06028A   06196
44523008  
00014500  00000-0  95600-4 0  9054
2 29251  51
6323  41
9111 0009587  73
3938 286
8278 15
76279385  1702


Satellite: SHUTTLE
Catalog Number: 29251
Epoch time:      06196
44523008   =   yrday
fracday
Element set:     905
Inclination:       51
6323  deg
RA of node:        41
9111  deg
Eccentricity:     
0009587     
Arg of perigee:    73
3938  deg
Mean anomaly:     286
8278  deg
Mean motion:   15
76279385  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             170
Checksum:              313


Coasting Arc #7 (begining on orbit 170)
---------------------------------------

Vector Time (GMT): 2006/196/11:04:59
153
Vector Time (MET): 010/16:27:04
202
Weight (LBS)     : 237032
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3082916
13                 A    =         6714173
03  meter
 Y    =        2795842
26  meter          E    =           
0012976
 Z    =        5258244
64                 I    =           51
81891
 XDOT =      -5562
679731                 Wp   =           74
02544
 YDOT =      -5328
112959  meter/sec      RA   =           41
28491  deg
 ZDOT =       -424
052194                 TA   =           20
00991
                                          MA   =           19
95908
                                          Ha   =            190
689  n
mi
                                          Hp   =            176
876

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10114554
22                 X    =        -3139532
19
 Y    =        9172710
83  feet           Y    =         2761006
66  meter
 Z    =       17251458
78                 Z    =         5243130
96
 XDOT =     -18250
261584                 XDOT =       -5500
551448
 YDOT =     -17480
685561  feet/sec       YDOT =       -5390
047690  meter/sec
 ZDOT =      -1391
247355                 ZDOT =        -450
925081

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10609044
94                 X    =         3233636
90
 Y    =        8707024
03  feet           Y    =         2653900
93  meter
 Z    =       17195684
32                 Z    =         5241244
58
 XDOT =     -13890
578282                 XDOT =       -4233
848260
 YDOT =      19899
223648  feet/sec       YDOT =        6065
283368  meter/sec
 ZDOT =      -1491
671320                 ZDOT =        -454
661418


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 29251U 06028A   06196
50863446  
00014500  00000-0  95600-4 0  9065
2 29251  51
6320  41
5842 0010316  75
6735 284
5574 15
76100909  1718


Satellite: SHUTTLE
Catalog Number: 29251
Epoch time:      06196
50863446   =   yrday
fracday
Element set:     906
Inclination:       51
6320  deg
RA of node:        41
5842  deg
Eccentricity:     
0010316     
Arg of perigee:    75
6735  deg
Mean anomaly:     284
5574  deg
Mean motion:   15
76100909  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             171
Checksum:              290


Coasting Arc #8 (begining on orbit 175)
---------------------------------------

Vector Time (GMT): 2006/196/19:23:31
027
Vector Time (MET): 011/00:45:36
075
Weight (LBS)     : 237011
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1672176
08                 A    =         6714151
89  meter
 Y    =       -3927311
52  meter          E    =           
0025226
 Z    =       -5204572
87                 I    =           51
81293
 XDOT =       6375
668451                 Wp   =           80
57373
 YDOT =       4152
301113  meter/sec      RA   =           39
51668  deg
 ZDOT =      -1085
246072                 TA   =          179
07917
                                          MA   =          179
07451
                                          Ha   =            190
565  n
mi
                                          Hp   =            176
532

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5486142
00                 X    =         1741304
58
 Y    =      -12884880
33  feet           Y    =        -3908201
27  meter
 Z    =      -17075370
31                 Z    =        -5196282
19
 XDOT =      20917
547410                 XDOT =        6333
975899
 YDOT =      13623
035147  feet/sec       YDOT =        4223
453095  meter/sec
 ZDOT =      -3560
518609                 ZDOT =       -1054
374237

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4858394
06                 X    =         1480838
51
 Y    =       13173757
33  feet           Y    =         4015361
23  meter
 Z    =      -17045066
48                 Z    =        -5195336
26
 XDOT =     -23591
181179                 XDOT =       -7190
592023
 YDOT =       4244
117495  feet/sec       YDOT =        1293
607012  meter/sec
 ZDOT =      -3445
390612                 ZDOT =       -1050
155059


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 29251U 06028A   06196
82565958  
00014500  00000-0  95600-4 0  9078
2 29251  51
6325  39
9485 0010745  79
5836 280
6539 15
76222052  1765


Satellite: SHUTTLE
Catalog Number: 29251
Epoch time:      06196
82565958   =   yrday
fracday
Element set:     907
Inclination:       51
6325  deg
RA of node:        39
9485  deg
Eccentricity:     
0010745     
Arg of perigee:    79
5836  deg
Mean anomaly:     280
6539  deg
Mean motion:   15
76222052  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             176
Checksum:              330


Coasting Arc #9 (begining on orbit 185)
---------------------------------------

Vector Time (GMT): 2006/197/09:47:56
555
Vector Time (MET): 011/15:10:01
604
Weight (LBS)     : 236991
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -286388
88                 A    =         6714946
93  meter
 Y    =        4575079
20  meter          E    =           
0015793
 Z    =        4893939
54                 I    =           51
80423
 XDOT =      -6814
845691                 Wp   =           95
54345
 YDOT =      -2836
310579  meter/sec      RA   =           36
44231  deg
 ZDOT =       2245
063849                 TA   =          332
68365
                                          MA   =          332
76661
                                          Ha   =            190
262  n
mi
                                          Hp   =            176
368

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -939596
05                 X    =         -361364
15
 Y    =       15010102
36  feet           Y    =         4571452
24  meter
 Z    =       16056232
07                 Z    =         4892366
79
 XDOT =     -22358
417622                 XDOT =       -6793
488518
 YDOT =      -9305
480901  feet/sec       YDOT =       -2912
493813  meter/sec
 ZDOT =       7365
695044                 ZDOT =        2212
009206

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14625737
84                 X    =         4457924
89
 Y    =        3527524
07  feet           Y    =         1075189
34  meter
 Z    =       16050949
14                 Z    =         4892329
30
 XDOT =     -12668
666991                 XDOT =       -3861
409699
 YDOT =      19456
871578  feet/sec       YDOT =        5930
454457  meter/sec
 ZDOT =       7242
623931                 ZDOT =        2207
551774


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 29251U 06028A   06197
45964535  
00014500  00000-0  95600-4 0  9083
2 29251  51
6329  36
6835 0010461  79
8825 280
3519 15
76373531  1863


Satellite: SHUTTLE
Catalog Number: 29251
Epoch time:      06197
45964535   =   yrday
fracday
Element set:     908
Inclination:       51
6329  deg
RA of node:        36
6835  deg
Eccentricity:     
0010461     
Arg of perigee:    79
8825  deg
Mean anomaly:     280
3519  deg
Mean motion:   15
76373531  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             186
Checksum:              323


Coasting Arc #10 (begining on orbit 190)
---------------------------------------

Vector Time (GMT): 2006/197/17:59:11
326
Vector Time (MET): 011/23:21:16
374
Weight (LBS)     : 235899
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3952703
03                 A    =         6698134
51  meter
 Y    =       -4932440
65  meter          E    =           
0042909
 Z    =       -2297416
76                 I    =           51
82328
 XDOT =       5173
054652                 Wp   =           44
14132
 YDOT =      -1624
490466  meter/sec      RA   =           34
68682  deg
 ZDOT =      -5443
095603                 TA   =          161
61534
                                          MA   =          161
45978
                                          Ha   =            188
126  n
mi
                                          Hp   =            152
619

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12968185
81                 X    =        -3886024
26
 Y    =      -16182548
06  feet           Y    =        -4976323
52  meter
 Z    =       -7537456
56                 Z    =        -2316457
52
 XDOT =      16971
964083                 XDOT =        5217
298623
 YDOT =      -5329
693129  feet/sec       YDOT =       -1566
321861  meter/sec
 ZDOT =     -17857
925207                 ZDOT =       -5417
857913

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18308048
04                 X    =         5580293
04
 Y    =        9684226
80  feet           Y    =         2951752
33  meter
 Z    =       -7608750
51                 Z    =        -2319147
16
 XDOT =     -12821
706516                 XDOT =       -3908
056146
 YDOT =      10360
264286  feet/sec       YDOT =        3157
808554  meter/sec
 ZDOT =     -17764
419601                 ZDOT =       -5414
595094


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 29251U 06028A   06197
77649183  
00014500  00000-0  95600-4 0  9098
2 29251  51
6323  35
0441 0043399  36
8956 323
5185 15
85192528  1917


Satellite: SHUTTLE
Catalog Number: 29251
Epoch time:      06197
77649183   =   yrday
fracday
Element set:     909
Inclination:       51
6323  deg
RA of node:        35
0441  deg
Eccentricity:     
0043399     
Arg of perigee:    36
8956  deg
Mean anomaly:     323
5185  deg
Mean motion:   15
85192528  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             191
Checksum:              322


Coasting Arc #11 (begining on orbit 206)
---------------------------------------

Vector Time (GMT): 2006/198/18:03:42
443
Vector Time (MET): 012/23:25:47
491
Weight (LBS)     : 235899
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6015342
11                 A    =         6700310
51  meter
 Y    =       -2939970
82  meter          E    =           
0045399
 Z    =         502987
22                 I    =           51
80641
 XDOT =       1661
392383                 Wp   =           57
08568
 YDOT =      -4500
090891  meter/sec      RA   =           29
43523  deg
 ZDOT =      -6019
329633                 TA   =          117
44463
                                          MA   =          116
98223
                                          Ha   =            188
149  n
mi
                                          Hp   =            152
440

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19735374
39                 X    =        -5984421
32
 Y    =       -9645573
57  feet           Y    =        -3007148
64  meter
 Z    =        1650220
52                 Z    =          473839
51
 XDOT =       5450
762410                 XDOT =        1740
892723
 YDOT =     -14764
077728  feet/sec       YDOT =       -4481
043110  meter/sec
 ZDOT =     -19748
456800                 ZDOT =       -6011
066218

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21973700
46                 X    =         6697583
90
 Y    =         158542
50  feet           Y    =           48323
75  meter
 Z    =        1541645
79                 Z    =          469893
64
 XDOT =       1383
785609                 XDOT =         421
777854
 YDOT =      14113
733803  feet/sec       YDOT =        4301
866063  meter/sec
 ZDOT =     -19718
319785                 ZDOT =       -6010
143870


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 29251U 06028A   06198
78514818  
00014500  00000-0  95600-4 0  9108
2 29251  51
6323  29
7770 0043347  40
6846 319
7547 15
85223382  2076


Satellite: SHUTTLE
Catalog Number: 29251
Epoch time:      06198
78514818   =   yrday
fracday
Element set:     910
Inclination:       51
6323  deg
RA of node:        29
7770  deg
Eccentricity:     
0043347     
Arg of perigee:    40
6846  deg
Mean anomaly:     319
7547  deg
Mean motion:   15
85223382  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             207
Checksum:              311


Coasting Arc #12 (begining on orbit 222)
---------------------------------------

Vector Time (GMT): 2006/199/18:08:23
752
Vector Time (MET): 013/23:30:28
801
Weight (LBS)     : 235899
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5939983
56                 A    =         6696163
23  meter
 Y    =            129
00  meter          E    =           
0052691
 Z    =        3089098
86                 I    =           51
76715
 XDOT =      -2587
235568                 Wp   =           55
26289
 YDOT =      -5382
423439  meter/sec      RA   =           24
18622  deg
 ZDOT =      -4886
641901                 TA   =           88
76575
                                          MA   =           88
16215
                                          Ha   =            188
186  n
mi
                                          Hp   =            152
160

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19488135
02                 X    =        -5954548
82
 Y    =            423
24  feet           Y    =          -66460
17  meter
 Z    =       10134838
79                 Z    =         3060207
15
 XDOT =      -8488
305669                 XDOT =       -2503
042428
 YDOT =     -17658
869549  feet/sec       YDOT =       -5410
919253  meter/sec
 ZDOT =     -16032
289700                 ZDOT =       -4899
007089

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17290170
70                 X    =         5270044
03
 Y    =       -9110446
45  feet           Y    =        -2776864
08  meter
 Z    =       10027568
35                 Z    =         3056402
83
 XDOT =      14998
799458                 XDOT =        4571
634075
 YDOT =      10446
358230  feet/sec       YDOT =        3184
049988  meter/sec
 ZDOT =     -16078
844700                 ZDOT =       -4900
831864


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 29251U 06028A   06199
79376688  
00014500  00000-0  95600-4 0  9112
2 29251  51
6325  24
5097 0043354  44
5060 315
9579 15
85281644  2238


Satellite: SHUTTLE
Catalog Number: 29251
Epoch time:      06199
79376688   =   yrday
fracday
Element set:     911
Inclination:       51
6325  deg
RA of node:        24
5097  deg
Eccentricity:     
0043354     
Arg of perigee:    44
5060  deg
Mean anomaly:     315
9579  deg
Mean motion:   15
85281644  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             223
Checksum:              317


Coasting Arc #13 (begining on orbit 237)
---------------------------------------

Vector Time (GMT): 2006/200/18:12:49
499
Vector Time (MET): 014/23:34:54
548
Weight (LBS)     : 235899
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3659727
37                 A    =         6689656
44  meter
 Y    =        2781208
04  meter          E    =           
0049975
 Z    =        4839696
47                 I    =           51
71979
 XDOT =      -6180
434007                 Wp   =           48
88211
 YDOT =      -4044
232364  meter/sec      RA   =           18
96131  deg
 ZDOT =      -2301
822471                 TA   =           63
64722
                                          MA   =           63
13492
                                          Ha   =            188
093  n
mi
                                          Hp   =            151
813

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12006979
55                 X    =        -3714103
73
 Y    =        9124698
29  feet           Y    =         2739926
48  meter
 Z    =       15878269
27                 Z    =         4821786
07
 XDOT =     -20277
014458                 XDOT =       -6123
512307
 YDOT =     -13268
478883  feet/sec       YDOT =       -4113
112532  meter/sec
 ZDOT =      -7551
910993                 ZDOT =       -2331
709445

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5940615
21                 X    =         1810699
52
 Y    =      -13936775
69  feet           Y    =        -4247929
23  meter
 Z    =       15812099
37                 Z    =         4819527
89
 XDOT =      23139
196803                 XDOT =        7052
827186
 YDOT =        990
450466  feet/sec       YDOT =         301
889302  meter/sec
 ZDOT =      -7663
360863                 ZDOT =       -2335
792391


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 29251U 06028A   06200
80234140  
00014500  00000-0  95600-4 0  9124
2 29251  51
6328  19
2415 0043254  48
0057 312
4783 15
85390400  2386


Satellite: SHUTTLE
Catalog Number: 29251
Epoch time:      06200
80234140   =   yrday
fracday
Element set:     912
Inclination:       51
6328  deg
RA of node:        19
2415  deg
Eccentricity:     
0043254     
Arg of perigee:    48
0057  deg
Mean anomaly:     312
4783  deg
Mean motion:   15
85390400  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             238
Checksum:              257

SPACE SHUTTLE ORBITAL DATA:

The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:

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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