Date: September 10th 2009

SHUTTLE TRAJECTORY DATA

Lift off time (UTC) : 2009/241/03:59:36 958 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 70 ET - UTC (sec) : 66 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


253/00:08:53 330 1 9 -0 1 17 0
011/20:09:16 372 -12 3 0 0 192 2
000/00:00:12 743 11 6 -17 0 179 7

Coasting Arc #1 (Orbit 173)
---------------------------------------

Vector Time (GMT): 2009/252/01:17:33
000
Vector Time (MET): 010/21:17:56
042
Weight (LBS)     : 232963
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         892721
90                 A    =         6720683
13  meter
 Y    =       -4955723
76  meter          E    =           
0014557
 Z    =        4436770
51                 I    =           51
35322
 XDOT =       5816
102699                 Wp   =           73
56579
 YDOT =       3921
277495  meter/sec      RA   =          235
41838  deg
 ZDOT =       3205
078749                 TA   =          344
26271
                                          MA   =          344
30791
                                          Ha   =            191
423  n
mi
                                          Hp   =            179
773

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2928877
61                 X    =          926518
04
 Y    =      -16258936
21  feet           Y    =        -4945551
65  meter
 Z    =       14556333
68                 Z    =         4441189
71
 XDOT =      19081
701767                 XDOT =        5756
252168
 YDOT =      12865
083645  feet/sec       YDOT =        3985
982078  meter/sec
 ZDOT =      10515
350226                 ZDOT =        3233
188121

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         884619
68                 X    =          269632
08
 Y    =      -16481845
82  feet           Y    =        -5023666
60  meter
 Z    =       14573413
72                 Z    =         4441976
50
 XDOT =      19216
807981                 XDOT =        5857
283073
 YDOT =      10440
525344  feet/sec       YDOT =        3182
272125  meter/sec
 ZDOT =      10626
192794                 ZDOT =        3238
863564


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 00128U          09252
10718062  
00020000  00000-0  20000-3 0  9003
2 00128  51
6377 236
0350 0009354  36
2501 323
9295 15
75011526  1747


Satellite: SHUTTLE
Catalog Number: 00128
Epoch time:      09252
10718062   =   yrday
fracday
Element set:     900
Inclination:       51
6377  deg
RA of node:       236
0350  deg
Eccentricity:     
0009354     
Arg of perigee:    36
2501  deg
Mean anomaly:     323
9295  deg
Mean motion:   15
75011526  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             174
Checksum:              242


Coasting Arc #2 (Orbit 188)
---------------------------------------

Vector Time (GMT): 2009/253/00:08:59
701
Vector Time (MET): 011/20:09:22
743
Weight (LBS)     : 232573
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         808735
33                 A    =         6719922
34  meter
 Y    =       -4810264
88  meter          E    =           
0013859
 Z    =        4609096
78                 I    =           51
36713
 XDOT =       6083
301623                 Wp   =           46
62690
 YDOT =       3770
920422  meter/sec      RA   =          230
50035  deg
 ZDOT =       2872
100456                 TA   =           14
92023
                                          MA   =           14
87938
                                          Ha   =            192
225  n
mi
                                          Hp   =            179
652

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2653331
12                 X    =          840074
03
 Y    =      -15781708
94  feet           Y    =        -4801045
80  meter
 Z    =       15121708
60                 Z    =         4613101
89
 XDOT =      19958
338659                 XDOT =        6026
730116
 YDOT =      12371
786160  feet/sec       YDOT =        3838
631236  meter/sec
 ZDOT =       9422
901757                 ZDOT =        2901
515954

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5095123
94                 X    =         1552993
78
 Y    =      -15155012
11  feet           Y    =        -4619247
69  meter
 Z    =       15137169
29                 Z    =         4613809
20
 XDOT =      16523
391029                 XDOT =        5036
329586
 YDOT =      15069
725366  feet/sec       YDOT =        4593
252292  meter/sec
 ZDOT =       9538
882064                 ZDOT =        2907
451253


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 00128U          09253
05893100  
00020000  00000-0  20000-3 0  9016
2 00128  51
6367 231
1401 0013431  11
5174 348
6294 15
75038481  1890


Satellite: SHUTTLE
Catalog Number: 00128
Epoch time:      09253
05893100   =   yrday
fracday
Element set:     901
Inclination:       51
6367  deg
RA of node:       231
1401  deg
Eccentricity:     
0013431     
Arg of perigee:    11
5174  deg
Mean anomaly:     348
6294  deg
Mean motion:   15
75038481  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             189
Checksum:              248


Coasting Arc #3 (Orbit 203)
---------------------------------------

Vector Time (GMT): 2009/254/00:09:02
517
Vector Time (MET): 012/20:09:25
560
Weight (LBS)     : 232573
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5536503
35                 A    =         6727109
21  meter
 Y    =       -3118083
34  meter          E    =           
0019071
 Z    =       -2182974
04                 I    =           51
41263
 XDOT =        863
166142                 Wp   =           24
45877
 YDOT =      -5347
356352  meter/sec      RA   =          225
29772  deg
 ZDOT =       5482
905350                 TA   =          310
97977
                                          MA   =          311
14459
                                          Ha   =            192
330  n
mi
                                          Hp   =            179
388

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18164381
07                 X    =        -5490620
33
 Y    =      -10229932
21  feet           Y    =        -3179739
23  meter
 Z    =       -7161988
31                 Z    =        -2209759
15
 XDOT =       2831
909916                 XDOT =         896
261852
 YDOT =     -17543
820054  feet/sec       YDOT =       -5337
518861  meter/sec
 ZDOT =      17988
534614                 ZDOT =        5487
179051

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16443921
51                 X    =        -5012107
28
 Y    =      -12754212
62  feet           Y    =        -3887484
01  meter
 Z    =       -7267587
96                 Z    =        -2215160
81
 XDOT =       4316
624481                 XDOT =        1315
707142
 YDOT =     -15762
150908  feet/sec       YDOT =       -4804
303597  meter/sec
 ZDOT =      18005
019844                 ZDOT =        5487
930048


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 00128U          09254
01065643  
00020000  00000-0  20000-3 0  9027
2 00128  51
6379 226
2454 0013443  15
8435 344
3146 15
75028082  2049


Satellite: SHUTTLE
Catalog Number: 00128
Epoch time:      09254
01065643   =   yrday
fracday
Element set:     902
Inclination:       51
6379  deg
RA of node:       226
2454  deg
Eccentricity:     
0013443     
Arg of perigee:    15
8435  deg
Mean anomaly:     344
3146  deg
Mean motion:   15
75028082  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             204
Checksum:              248


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

Vector Time (GMT): 2009/255/00:09:06
343
Vector Time (MET): 013/20:09:29
385
Weight (LBS)     : 232573
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -765658
53                 A    =         6718567
08  meter
 Y    =        4512001
05  meter          E    =           
0023296
 Z    =       -4938424
64                 I    =           51
40597
 XDOT =      -6578
837356                 Wp   =           46
48489
 YDOT =      -3392
535581  meter/sec      RA   =          220
17532  deg
 ZDOT =      -2069
927449                 TA   =          203
30667
                                          MA   =          203
41246
                                          Ha   =            192
495  n
mi
                                          Hp   =            179
085

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2512003
05                 X    =         -792065
51
 Y    =       14803153
04  feet           Y    =         4503291
41  meter
 Z    =      -16202180
56                 Z    =        -4942208
32
 XDOT =     -21584
112060                 XDOT =       -6530
357101
 YDOT =     -11130
366079  feet/sec       YDOT =       -3465
832918  meter/sec
 ZDOT =      -6791
100555                 ZDOT =       -2101
769870

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4291755
21                 X    =        -1308126
99
 Y    =       14371872
45  feet           Y    =         4380546
72  meter
 Z    =      -16216789
87                 Z    =        -4942877
55
 XDOT =     -18894
830942                 XDOT =       -5759
144471
 YDOT =     -13482
732322  feet/sec       YDOT =       -4109
536812  meter/sec
 ZDOT =      -6916
634007                 ZDOT =       -2108
190045


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 00128U          09255
02581758  
00020000  00000-0  20000-3 0  9030
2 00128  51
6380 221
0246 0013507  19
8066 340
3619 15
75062476  2202


Satellite: SHUTTLE
Catalog Number: 00128
Epoch time:      09255
02581758   =   yrday
fracday
Element set:     903
Inclination:       51
6380  deg
RA of node:       221
0246  deg
Eccentricity:     
0013507     
Arg of perigee:    19
8066  deg
Mean anomaly:     340
3619  deg
Mean motion:   15
75062476  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             220
Checksum:              254


Coasting Arc #5 (Orbit 235)
---------------------------------------

Vector Time (GMT): 2009/256/00:14:11
069
Vector Time (MET): 014/20:14:34
111
Weight (LBS)     : 232573
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5328635
52                 A    =         6729007
80  meter
 Y    =        4096931
01  meter          E    =           
0013665
 Z    =        -378555
86                 I    =           51
46477
 XDOT =      -3186
007154                 Wp   =           73
74113
 YDOT =       3605
418594  meter/sec      RA   =          214
98407  deg
 ZDOT =      -6002
526428                 TA   =          110
38116
                                          MA   =          110
23432
                                          Ha   =            192
546  n
mi
                                          Hp   =            178
916

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17482400
01                 X    =         5284265
85
 Y    =       13441374
71  feet           Y    =         4156270
87  meter
 Z    =       -1241981
16                 Z    =         -352777
08
 XDOT =     -10452
779375                 XDOT =       -3196
927594
 YDOT =      11828
801161  feet/sec       YDOT =        3569
729799  meter/sec
 ZDOT =     -19693
328175                 ZDOT =       -6018
030529

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16227142
10                 X    =         4946032
91
 Y    =       14940785
25  feet           Y    =         4553951
34  meter
 Z    =       -1140253
06                 Z    =         -347549
13
 XDOT =     -10257
465325                 XDOT =       -3126
475431
 YDOT =       9680
820789  feet/sec       YDOT =        2950
714176  meter/sec
 ZDOT =     -19754
127197                 ZDOT =       -6021
057970


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 00128U          09256
04096566  
00020000  00000-0  20000-3 0  9042
2 00128  51
6374 215
8016 0013519  23
3313 336
8461 15
75092891  2365


Satellite: SHUTTLE
Catalog Number: 00128
Epoch time:      09256
04096566   =   yrday
fracday
Element set:     904
Inclination:       51
6374  deg
RA of node:       215
8016  deg
Eccentricity:     
0013519     
Arg of perigee:    23
3313  deg
Mean anomaly:     336
8461  deg
Mean motion:   15
75092891  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             236
Checksum:              269


Coasting Arc #6 (Orbit 251)
---------------------------------------

Vector Time (GMT): 2009/257/00:14:19
852
Vector Time (MET): 015/20:14:42
894
Weight (LBS)     : 232573
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2951947
37                 A    =         6717285
08  meter
 Y    =       -3072176
14  meter          E    =           
0016497
 Z    =        5187166
71                 I    =           51
45137
 XDOT =       6245
680239                 Wp   =           33
79985
 YDOT =       4423
629728  meter/sec      RA   =          209
81568  deg
 ZDOT =       -919
461501                 TA   =           65
05840
                                          MA   =           64
88707
                                          Ha   =            192
576  n
mi
                                          Hp   =            178
742

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9684866
71                 X    =         2960883
39
 Y    =      -10079318
03  feet           Y    =        -3039115
75  meter
 Z    =       17018263
50                 Z    =         5201528
91
 XDOT =      20491
076898                 XDOT =        6200
216810
 YDOT =      14513
220894  feet/sec       YDOT =        4493
218396  meter/sec
 ZDOT =      -3016
605975                 ZDOT =        -889
230579

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10276731
48                 X    =         3132347
75
 Y    =       -9373218
27  feet           Y    =        -2856956
93  meter
 Z    =       17074605
62                 Z    =         5204339
79
 XDOT =      18742
900201                 XDOT =        5712
835981
 YDOT =      15182
904564  feet/sec       YDOT =        4627
749311  meter/sec
 ZDOT =      -2897
313770                 ZDOT =        -883
101237


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 00128U          09257
05610257  
00020000  00000-0  20000-3 0  9054
2 00128  51
6383 210
5800 0013527  27
4545 332
7331 15
75078399  2525


Satellite: SHUTTLE
Catalog Number: 00128
Epoch time:      09257
05610257   =   yrday
fracday
Element set:     905
Inclination:       51
6383  deg
RA of node:       210
5800  deg
Eccentricity:     
0013527     
Arg of perigee:    27
4545  deg
Mean anomaly:     332
7331  deg
Mean motion:   15
75078399  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             252
Checksum:              261

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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