Date: November 25th 2009

SHUTTLE TRAJECTORY DATA

Lift off time (UTC) : 2009/320/19:28:09 949 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 36 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


329/09:11:00 142 -0 0 -0 1 0 1
008/13:42:50 193 0 1 0 0 189 0
000/00:00:00 386 -0 1 -0 0 179 5

329/11:08:15 737 1 7 -0 0 3 0
008/15:40:05 788 -1 2 0 0 189 2
000/00:00:11 576 2 1 -3 0 179 1

329/11:36:12 842 -1 2 1 5 1 5
008/16:08:02 893 0 3 0 0 189 3
000/00:00:05 786 -0 8 -0 0 180 1

330/09:29:19 511 17 5 0 1 18 0
009/14:01:09 562 4 1 0 0 191 5
000/00:00:12 225 -0 4 18 0 177 4

331/18:20:07 542 30 1 -55 0 55 0
010/22:51:57 593 -26 9 -0 0 190 7
000/00:00:33 186 37 3 1 0 147 7

Coasting Arc #1 (Orbit 122)
---------------------------------------

Vector Time (GMT): 2009/328/11:39:31
000
Vector Time (MET): 007/16:11:21
051
Weight (LBS)     : 217729
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5840286
72                 A    =         6721777
43  meter
 Y    =         448752
53  meter          E    =           
0010061
 Z    =       -3294212
31                 I    =           51
52213
 XDOT =      -3050
919872                 Wp   =           38
49593
 YDOT =      -5280
191378  meter/sec      RA   =          202
15705  deg
 ZDOT =       4705
080370                 TA   =          282
73657
                                          MA   =          282
84900
                                          Ha   =            188
869  n
mi
                                          Hp   =            179
622

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19161045
68                 X    =        -5828867
78
 Y    =        1472285
21  feet           Y    =          383507
02  meter
 Z    =      -10807783
17                 Z    =        -3322557
05
 XDOT =     -10009
579631                 XDOT =       -3014
505836
 YDOT =     -17323
462527  feet/sec       YDOT =       -5314
105215  meter/sec
 ZDOT =      15436
615388                 ZDOT =        4690
346967

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8968376
68                 X    =         2733561
21
 Y    =      -16924840
95  feet           Y    =        -5158691
52  meter
 Z    =      -10919681
82                 Z    =        -3328319
02
 XDOT =      18804
843526                 XDOT =        5731
716307
 YDOT =         75
065265  feet/sec       YDOT =          22
879893  meter/sec
 ZDOT =      15378
205364                 ZDOT =        4687
276995


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 36094U 09062A   09328
49267330  
00020000  00000-0  20000-3 0  9004
2 36094  51
6463 203
1597 0007847  10
5406 349
5922 15
75956971  1233


Satellite: SHUTTLE
Catalog Number: 36094
Epoch time:      09328
49267330   =   yrday
fracday
Element set:     900
Inclination:       51
6463  deg
RA of node:       203
1597  deg
Eccentricity:     
0007847     
Arg of perigee:    10
5406  deg
Mean anomaly:     349
5922  deg
Mean motion:   15
75956971  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             123
Checksum:              302


Coasting Arc #2 (Orbit 137)
---------------------------------------

Vector Time (GMT): 2009/329/09:11:00
335
Vector Time (MET): 008/13:42:50
386
Weight (LBS)     : 217726
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5949441
50                 A    =         6725937
76  meter
 Y    =       -2874904
74  meter          E    =           
0020311
 Z    =        1190776
04                 I    =           51
56043
 XDOT =       3081
128781                 Wp   =           42
92220
 YDOT =      -3921
678516  meter/sec      RA   =          197
56726  deg
 ZDOT =       5882
143170                 TA   =          330
16482
                                          MA   =          330
28046
                                          Ha   =            188
991  n
mi
                                          Hp   =            179
486

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19519165
01                 X    =        -5922636
29
 Y    =       -9432102
17  feet           Y    =        -2941285
08  meter
 Z    =        3906745
53                 Z    =         1161938
18
 XDOT =      10108
690227                 XDOT =        3096
177838
 YDOT =     -12866
399331  feet/sec       YDOT =       -3887
139628  meter/sec
 ZDOT =      19298
369980                 ZDOT =        5897
147914

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21636769
35                 X    =         6594887
30
 Y    =        1640224
12  feet           Y    =          499940
31  meter
 Z    =        3792741
98                 Z    =         1156027
76
 XDOT =      -4484
325042                 XDOT =       -1366
822273
 YDOT =      14050
725235  feet/sec       YDOT =        4282
661052  meter/sec
 ZDOT =      19357
443675                 ZDOT =        5900
148832


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 36094U 09062A   09329
44382445  
00020000  00000-0  20000-3 0  9016
2 36094  51
6451 198
2607 0007793  15
1389 345
0007 15
75995357  1389


Satellite: SHUTTLE
Catalog Number: 36094
Epoch time:      09329
44382445   =   yrday
fracday
Element set:     901
Inclination:       51
6451  deg
RA of node:       198
2607  deg
Eccentricity:     
0007793     
Arg of perigee:    15
1389  deg
Mean anomaly:     345
0007  deg
Mean motion:   15
75995357  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             138
Checksum:              310


Coasting Arc #3 (Orbit 138)
---------------------------------------

Vector Time (GMT): 2009/329/11:08:21
525
Vector Time (MET): 008/15:40:11
576
Weight (LBS)     : 217651
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3920093
87                 A    =         6716492
53  meter
 Y    =       -2720287
84  meter          E    =           
0015157
 Z    =        4724369
61                 I    =           51
53299
 XDOT =       6005
673030                 Wp   =           36
26006
 YDOT =       4043
121973  meter/sec      RA   =          197
11549  deg
 ZDOT =      -2638
910761                 TA   =           79
76265
                                          MA   =           79
59176
                                          Ha   =            189
203  n
mi
                                          Hp   =            179
063

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12861200
36                 X    =         3927270
75
 Y    =       -8924828
87  feet           Y    =        -2676411
11  meter
 Z    =       15499900
28                 Z    =         4743431
05
 XDOT =      19703
651674                 XDOT =        5972
835332
 YDOT =      13264
835868  feet/sec       YDOT =        4110
097460  meter/sec
 ZDOT =      -8657
843705                 ZDOT =       -2609
814324

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1142155
56                 X    =         -348129
01
 Y    =       15537803
25  feet           Y    =         4735922
43  meter
 Z    =       15575047
51                 Z    =         4747274
48
 XDOT =     -21625
557188                 XDOT =       -6591
469831
 YDOT =       7027
038260  feet/sec       YDOT =        2141
841262  meter/sec
 ZDOT =      -8542
765613                 ZDOT =       -2603
834959


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 36094U 09062A   09329
50723378  
00020000  00000-0  20000-3 0  9028
2 36094  51
6463 197
9344 0008961  15
3883 344
7552 15
76059170  1392


Satellite: SHUTTLE
Catalog Number: 36094
Epoch time:      09329
50723378   =   yrday
fracday
Element set:     902
Inclination:       51
6463  deg
RA of node:       197
9344  deg
Eccentricity:     
0008961     
Arg of perigee:    15
3883  deg
Mean anomaly:     344
7552  deg
Mean motion:   15
76059170  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             139
Checksum:              315


Coasting Arc #4 (Orbit 138)
---------------------------------------

Vector Time (GMT): 2009/329/11:36:15
735
Vector Time (MET): 008/16:08:05
786
Weight (LBS)     : 217613
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3595506
45                 A    =         6721130
26  meter
 Y    =        4246686
28  meter          E    =           
0011719
 Z    =       -3783752
55                 I    =           51
54549
 XDOT =      -6257
637738                 Wp   =           39
13912
 YDOT =       1561
569853  meter/sec      RA   =          197
06206  deg
 ZDOT =      -4191
800726                 TA   =          186
75489
                                          MA   =          186
77070
                                          Ha   =            189
317  n
mi
                                          Hp   =            180
115

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11796281
00                 X    =         3566133
11
 Y    =       13932697
75  feet           Y    =         4286729
28  meter
 Z    =      -12413886
30                 Z    =        -3766356
46
 XDOT =     -20530
307540                 XDOT =       -6254
271062
 YDOT =       5123
260672  feet/sec       YDOT =        1491
612258  meter/sec
 ZDOT =     -13752
627053                 ZDOT =       -4222
192576

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18112072
74                 X    =        -5520559
77
 Y    =        2632612
75  feet           Y    =          802420
37  meter
 Z    =      -12345001
27                 Z    =        -3762756
39
 XDOT =       6738
908167                 XDOT =        2054
019209
 YDOT =     -18718
347955  feet/sec       YDOT =       -5705
352457  meter/sec
 ZDOT =     -13872
568086                 ZDOT =       -4228
358753


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 36094U 09062A   09329
50723702  
00020000  00000-0  20000-3 0  9030
2 36094  51
6461 197
9346 0007840  10
6243 349
5085 15
75720780  1390


Satellite: SHUTTLE
Catalog Number: 36094
Epoch time:      09329
50723702   =   yrday
fracday
Element set:     903
Inclination:       51
6461  deg
RA of node:       197
9346  deg
Eccentricity:     
0007840     
Arg of perigee:    10
6243  deg
Mean anomaly:     349
5085  deg
Mean motion:   15
75720780  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             139
Checksum:              295


Coasting Arc #5 (Orbit 153)
---------------------------------------

Vector Time (GMT): 2009/330/09:29:25
623
Vector Time (MET): 009/14:01:15
675
Weight (LBS)     : 217227
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6520318
98                 A    =         6727320
39  meter
 Y    =       -1595745
43  meter          E    =           
0024552
 Z    =         209032
30                 I    =           51
59247
 XDOT =       1335
240100                 Wp   =           49
11351
 YDOT =      -4607
081638  meter/sec      RA   =          192
33730  deg
 ZDOT =       6036
779154                 TA   =          313
16284
                                          MA   =          313
36779
                                          Ha   =            191
528  n
mi
                                          Hp   =            177
409

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21392122
64                 X    =        -6503005
93
 Y    =       -5235385
26  feet           Y    =        -1668562
69  meter
 Z    =         685801
51                 Z    =          177397
98
 XDOT =       4380
708991                 XDOT =        1357
331909
 YDOT =     -15115
097236  feet/sec       YDOT =       -4592
026897  meter/sec
 ZDOT =      19805
705886                 ZDOT =        6043
319366

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21437643
01                 X    =         6534193
59
 Y    =       -5061171
40  feet           Y    =        -1542645
04  meter
 Z    =         560802
97                 Z    =          170932
74
 XDOT =       2701
813508                 XDOT =         823
512757
 YDOT =      13838
397827  feet/sec       YDOT =        4217
943658  meter/sec
 ZDOT =      19831
325407                 ZDOT =        6044
587984


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 36094U 09062A   09330
45853197  
00020000  00000-0  20000-3 0  9049
2 36094  51
6457 193
0367 0011958  50
8054 309
4170 15
75709243  1544


Satellite: SHUTTLE
Catalog Number: 36094
Epoch time:      09330
45853197   =   yrday
fracday
Element set:     904
Inclination:       51
6457  deg
RA of node:       193
0367  deg
Eccentricity:     
0011958     
Arg of perigee:    50
8054  deg
Mean anomaly:     309
4170  deg
Mean motion:   15
75709243  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             154
Checksum:              298


Coasting Arc #6 (Orbit 168)
---------------------------------------

Vector Time (GMT): 2009/331/09:34:24
013
Vector Time (MET): 010/14:06:14
064
Weight (LBS)     : 217227
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3630453
00                 A    =         6717802
40  meter
 Y    =        3251706
78  meter          E    =           
0020197
 Z    =       -4638933
95                 I    =           51
59104
 XDOT =      -6426
450401                 Wp   =           80
88942
 YDOT =      -3099
251073  meter/sec      RA   =          187
14393  deg
 ZDOT =       2870
654571                 TA   =          217
48750
                                          MA   =          217
62852
                                          Ha   =            191
512  n
mi
                                          Hp   =            177
170

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11910935
03                 X    =        -3644008
70
 Y    =       10668329
35  feet           Y    =         3211033
30  meter
 Z    =      -15219599
58                 Z    =        -4656603
90
 XDOT =     -21084
154859                 XDOT =       -6405
261843
 YDOT =     -10168
146566  feet/sec       YDOT =       -3170
997075  meter/sec
 ZDOT =       9418
158040                 ZDOT =        2839
485502

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5097702
69                 X    =         1553779
78
 Y    =      -15085504
47  feet           Y    =        -4598061
76  meter
 Z    =      -15289238
63                 Z    =        -4660159
93
 XDOT =      22311
404122                 XDOT =        6800
515976
 YDOT =      -1835
511470  feet/sec       YDOT =        -559
463896  meter/sec
 ZDOT =       9294
920224                 ZDOT =        2833
091684


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 36094U 09062A   09331
40983142  
00020000  00000-0  20000-3 0  9050
2 36094  51
6462 188
1395 0011910  54
1877 306
0393 15
75735961  1696


Satellite: SHUTTLE
Catalog Number: 36094
Epoch time:      09331
40983142   =   yrday
fracday
Element set:     905
Inclination:       51
6462  deg
RA of node:       188
1395  deg
Eccentricity:     
0011910     
Arg of perigee:    54
1877  deg
Mean anomaly:     306
0393  deg
Mean motion:   15
75735961  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             169
Checksum:              301


Coasting Arc #7 (Orbit 174)
---------------------------------------

Vector Time (GMT): 2009/331/18:20:24
135
Vector Time (MET): 010/22:52:14
186
Weight (LBS)     : 216054
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5467285
95                 A    =         6694765
66  meter
 Y    =        2742194
45  meter          E    =           
0054646
 Z    =       -2809626
69                 I    =           51
62083
 XDOT =      -4436
437460                 Wp   =           41
23915
 YDOT =       3641
004066  meter/sec      RA   =          185
30236  deg
 ZDOT =      -5095
214840                 TA   =          170
93416
                                          MA   =          170
83509
                                          Ha   =            190
658  n
mi
                                          Hp   =            147
710

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17937289
87                 X    =         5449864
90
 Y    =        8996700
95  feet           Y    =         2803235
58  meter
 Z    =       -9217935
33                 Z    =        -2783108
17
 XDOT =     -14555
241011                 XDOT =       -4452
069837
 YDOT =      11945
551399  feet/sec       YDOT =        3591
306013  meter/sec
 ZDOT =     -16716
584121                 ZDOT =       -5116
805400

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14113330
26                 X    =         4301743
06
 Y    =       14332586
92  feet           Y    =         4368572
49  meter
 Z    =       -9113077
91                 Z    =        -2777666
15
 XDOT =     -16498
854714                 XDOT =       -5028
850917
 YDOT =       5597
036997  feet/sec       YDOT =        1705
976877  meter/sec
 ZDOT =     -16801
692652                 ZDOT =       -5121
155920


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 36094U 09062A   09331
79022018  
00020000  00000-0  20000-3 0  9069
2 36094  51
6447 186
1738 0054007  35
9695 324
5090 15
86031855  1756


Satellite: SHUTTLE
Catalog Number: 36094
Epoch time:      09331
79022018   =   yrday
fracday
Element set:     906
Inclination:       51
6447  deg
RA of node:       186
1738  deg
Eccentricity:     
0054007     
Arg of perigee:    35
9695  deg
Mean anomaly:     324
5090  deg
Mean motion:   15
86031855  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             175
Checksum:              300

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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