Date: July 29th 2009

SHUTTLE TRAJECTORY DATA

Lift off time (UTC) : 2009/196/22:03:09 948 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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


209/16:18:10 854 0 2 -0 4 0 4
012/18:15:00 906 -0 4 0 0 188 4
000/00:00:01 813 -0 2 0 0 185 6

209/18:41:15 989 -0 9 -0 0 3 0
012/20:38:06 041 -2 5 -0 0 188 7
000/00:00:12 082 1 3 -3 0 185 1

209/19:09:30 069 -1 1 -10 0 10 0
012/21:06:20 121 -9 7 -0 0 188 5
000/00:00:40 241 2 0 0 2 179 3

210/17:28:37 425 -7 7 -0 1 17 0
013/19:25:27 477 -12 0 -0 0 191 0
000/00:00:12 054 9 2 -17 0 177 0

210/20:16:20 544 3 0 -16 0 16 0
013/22:13:10 596 15 5 0 0 182 6
000/00:00:21 193 -2 8 0 2 177 0

211/11:03:42 184 -4 8 0 1 17 0
014/13:00:32 236 -15 8 -0 0 184 8
000/00:00:12 471 3 9 17 0 174 3

211/17:33:10 948 -0 1 0 5 0 5
014/19:30:01 000 -0 5 0 0 185 1
000/00:00:02 001 0 1 -0 0 174 3

Coasting Arc #1 (Orbit 181)
---------------------------------------

Vector Time (GMT): 2009/208/07:33:41
000
Vector Time (MET): 011/09:30:31
052
Weight (LBS)     : 227255
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2604089
82                 A    =         6724025
07  meter
 Y    =       -4490497
06  meter          E    =           
0006086
 Z    =        4273970
74                 I    =           51
96061
 XDOT =       3835
550002                 Wp   =           35
98908
 YDOT =      -5636
404881  meter/sec      RA   =           99
99469  deg
 ZDOT =      -3577
617986                 TA   =           90
20180
                                          MA   =           90
13206
                                          Ha   =            188
401  n
mi
                                          Hp   =            185
900

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8543601
77                 X    =        -2574444
77
 Y    =      -14732601
92  feet           Y    =        -4519452
06  meter
 Z    =       14022213
71                 Z    =         4261391
88
 XDOT =      12583
825466                 XDOT =        3915
671454
 YDOT =     -18492
141999  feet/sec       YDOT =       -5593
065288  meter/sec
 ZDOT =     -11737
591818                 ZDOT =       -3558
790808

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17062247
96                 X    =        -5200573
18
 Y    =        -559993
32  feet           Y    =         -170685
96  meter
 Z    =       13972518
37                 Z    =         4258823
60
 XDOT =      -8937
486781                 XDOT =       -2724
145971
 YDOT =     -19320
015995  feet/sec       YDOT =       -5888
740875  meter/sec
 ZDOT =     -11663
863229                 ZDOT =       -3555
145512


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 35633U 09038A   09208
35632036  
00020000  00000-0  20000-3 0  9006
2 35633  51
6387 100
6169 0006213 288
4874  71
5613 15
74093951  1826


Satellite: SHUTTLE
Catalog Number: 35633
Epoch time:      09208
35632036   =   yrday
fracday
Element set:     900
Inclination:       51
6387  deg
RA of node:       100
6169  deg
Eccentricity:     
0006213     
Arg of perigee:   288
4874  deg
Mean anomaly:      71
5613  deg
Mean motion:   15
74093951  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             182
Checksum:              284


Coasting Arc #2 (Orbit 197)
---------------------------------------

Vector Time (GMT): 2009/209/07:34:50
941
Vector Time (MET): 012/09:31:40
993
Weight (LBS)     : 227255
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3154902
91                 A    =         6726547
50  meter
 Y    =        4800693
89  meter          E    =           
0006796
 Z    =        3492089
10                 I    =           51
97414
 XDOT =      -3116
173876                 Wp   =           74
07184
 YDOT =      -5368
717011  meter/sec      RA   =           94
92783  deg
 ZDOT =       4559
815292                 TA   =          327
18384
                                          MA   =          327
22603
                                          Ha   =            188
564  n
mi
                                          Hp   =            185
820

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10350731
32                 X    =        -3225314
45
 Y    =       15750308
05  feet           Y    =         4765019
95  meter
 Z    =       11456985
24                 Z    =         3476592
03
 XDOT =     -10223
667572                 XDOT =       -3078
058995
 YDOT =     -17613
900954  feet/sec       YDOT =       -5403
351149  meter/sec
 ZDOT =      14960
023925                 ZDOT =        4544
769153

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8150790
91                 X    =         2484361
07
 Y    =       17034124
09  feet           Y    =         5192001
02  meter
 Z    =       11396296
65                 Z    =         3473591
22
 XDOT =     -19166
213593                 XDOT =       -5841
861903
 YDOT =       -809
954772  feet/sec       YDOT =        -246
874215  meter/sec
 ZDOT =      14900
587297                 ZDOT =        4541
699008


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 35633U 09038A   09209
37208825  
00020000  00000-0  20000-3 0  9015
2 35633  51
6394  95
3996 0006226 291
1995  68
8503 15
74135161  1985


Satellite: SHUTTLE
Catalog Number: 35633
Epoch time:      09209
37208825   =   yrday
fracday
Element set:     901
Inclination:       51
6394  deg
RA of node:        95
3996  deg
Eccentricity:     
0006226     
Arg of perigee:   291
1995  deg
Mean anomaly:      68
8503  deg
Mean motion:   15
74135161  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             198
Checksum:              312


Coasting Arc #3 (Orbit 202)
---------------------------------------

Vector Time (GMT): 2009/209/16:18:11
761
Vector Time (MET): 012/18:15:01
813
Weight (LBS)     : 227243
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3315642
90                 A    =         6722930
01  meter
 Y    =        3758188
52  meter          E    =           
0003891
 Z    =       -4484949
33                 I    =           51
96174
 XDOT =      -2863
352911                 Wp   =          110
50444
 YDOT =       6374
876248  meter/sec      RA   =           93
01705  deg
 ZDOT =       3225
944250                 TA   =          191
64133
                                          MA   =          191
65033
                                          Ha   =            188
408  n
mi
                                          Hp   =            185
622

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10878093
50                 X    =         3295158
73
 Y    =       12330014
84  feet           Y    =         3795151
84  meter
 Z    =      -14714400
68                 Z    =        -4468891
45
 XDOT =      -9394
202463                 XDOT =       -2950
096027
 YDOT =      20914
948320  feet/sec       YDOT =        6342
371274  meter/sec
 ZDOT =      10583
806594                 ZDOT =        3211
824002

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12981881
00                 X    =        -3956877
33
 Y    =      -10182960
89  feet           Y    =        -3103766
48  meter
 Z    =      -14651069
75                 Z    =        -4465646
06
 XDOT =       4841
930867                 XDOT =        1475
820528
 YDOT =     -21316
881998  feet/sec       YDOT =       -6497
385633  meter/sec
 ZDOT =      10528
607707                 ZDOT =        3209
119629


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 35633U 09038A   09209
68951319  
00020000  00000-0  20000-3 0  9023
2 35633  51
6377  93
7656 0005802 290
6644  69
3897 15
74202004  2035


Satellite: SHUTTLE
Catalog Number: 35633
Epoch time:      09209
68951319   =   yrday
fracday
Element set:     902
Inclination:       51
6377  deg
RA of node:        93
7656  deg
Eccentricity:     
0005802     
Arg of perigee:   290
6644  deg
Mean anomaly:      69
3897  deg
Mean motion:   15
74202004  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             203
Checksum:              300


Coasting Arc #4 (Orbit 204)
---------------------------------------

Vector Time (GMT): 2009/209/18:41:22
030
Vector Time (MET): 012/20:38:12
082
Weight (LBS)     : 227164
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2066943
18                 A    =         6727866
99  meter
 Y    =       -5674493
86  meter          E    =           
0008881
 Z    =        2958494
13                 I    =           51
97926
 XDOT =       4117
112592                 Wp   =           85
33743
 YDOT =      -4129
058457  meter/sec      RA   =           92
50678  deg
 ZDOT =      -5029
715768                 TA   =           60
71490
                                          MA   =           60
62617
                                          Ha   =            188
725  n
mi
                                          Hp   =            185
115

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6781309
64                 X    =        -2017708
15
 Y    =      -18617105
83  feet           Y    =        -5697332
60  meter
 Z    =        9706345
58                 Z    =         2948572
07
 XDOT =      13507
587245                 XDOT =        4187
411761
 YDOT =     -13546
779715  feet/sec       YDOT =       -4082
624988  meter/sec
 ZDOT =     -16501
692153                 ZDOT =       -5009
544540

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18160858
68                 X    =         5535429
73
 Y    =        7970407
25  feet           Y    =         2429380
13  meter
 Z    =        9667044
76                 Z    =         2946515
24
 XDOT =        922
348370                 XDOT =         281
131783
 YDOT =      17870
957023  feet/sec       YDOT =        5447
067701  meter/sec
 ZDOT =     -16422
585644                 ZDOT =       -5005
604104


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 35633U 09038A   09209
81648163  
00020000  00000-0  20000-3 0  9039
2 35633  51
6386  93
1122 0005012 299
4159  60
6504 15
74189142  2056


Satellite: SHUTTLE
Catalog Number: 35633
Epoch time:      09209
81648163   =   yrday
fracday
Element set:     903
Inclination:       51
6386  deg
RA of node:        93
1122  deg
Eccentricity:     
0005012     
Arg of perigee:   299
4159  deg
Mean anomaly:      60
6504  deg
Mean motion:   15
74189142  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             205
Checksum:              277


Coasting Arc #5 (Orbit 204)
---------------------------------------

Vector Time (GMT): 2009/209/19:09:50
190
Vector Time (MET): 012/21:06:40
241
Weight (LBS)     : 226901
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4111879
05                 A    =         6714691
33  meter
 Y    =       -1215754
88  meter          E    =           
0018646
 Z    =       -5183384
71                 I    =           51
95434
 XDOT =        656
348614                 Wp   =           68
63798
 YDOT =       7559
933608  meter/sec      RA   =           92
44132  deg
 ZDOT =      -1249
444442                 TA   =          189
43888
                                          MA   =          189
47397
                                          Ha   =            188
517  n
mi
                                          Hp   =            179
334

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13490416
82                 X    =         4150348
04
 Y    =       -3988697
13  feet           Y    =        -1169557
90  meter
 Z    =      -17005855
34                 Z    =        -5163315
96
 XDOT =       2153
374718                 XDOT =         577
832907
 YDOT =      24802
931784  feet/sec       YDOT =        7566
834388  meter/sec
 ZDOT =      -4099
227173                 ZDOT =       -1246
445967

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4929007
87                 X    =        -1502361
60
 Y    =       13277106
61  feet           Y    =         4046862
09  meter
 Z    =      -16927004
70                 Z    =        -5159351
03
 XDOT =     -20213
309549                 XDOT =       -6161
016751
 YDOT =     -12727
454138  feet/sec       YDOT =       -3879
328021  meter/sec
 ZDOT =      -4087
055499                 ZDOT =       -1245
734516


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 35633U 09038A   09209
81647496  
00020000  00000-0  20000-3 0  9048
2 35633  51
6399  93
1132 0005526  36
8286 323
3257 15
76083285  2052


Satellite: SHUTTLE
Catalog Number: 35633
Epoch time:      09209
81647496   =   yrday
fracday
Element set:     904
Inclination:       51
6399  deg
RA of node:        93
1132  deg
Eccentricity:     
0005526     
Arg of perigee:    36
8286  deg
Mean anomaly:     323
3257  deg
Mean motion:   15
76083285  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             205
Checksum:              302


Coasting Arc #6 (Orbit 219)
---------------------------------------

Vector Time (GMT): 2009/210/17:28:43
452
Vector Time (MET): 013/19:25:33
504
Weight (LBS)     : 226519
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3008814
86                 A    =         6720703
50  meter
 Y    =       -4812853
39  meter          E    =           
0022696
 Z    =        3590200
69                 I    =           51
97266
 XDOT =       3260
796734                 Wp   =           64
68637
 YDOT =      -5381
176395  meter/sec      RA   =           87
63598  deg
 ZDOT =      -4449
800748                 TA   =           72
57719
                                          MA   =           72
32917
                                          Ha   =            191
032  n
mi
                                          Hp   =            176
993

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9871439
81                 X    =        -2972213
54
 Y    =      -15790201
42  feet           Y    =        -4846295
44  meter
 Z    =       11778873
67                 Z    =         3575672
35
 XDOT =      10698
152016                 XDOT =        3342
343838
 YDOT =     -17654
778198  feet/sec       YDOT =       -5344
255845  meter/sec
 ZDOT =     -14599
083818                 ZDOT =       -4433
762348

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16334889
42                 X    =         4978874
29
 Y    =        9016388
68  feet           Y    =         2748195
27  meter
 Z    =       11721508
97                 Z    =         3572715
93
 XDOT =       -245
836624                 XDOT =         -74
931003
 YDOT =      19476
581029  feet/sec       YDOT =        5936
461898  meter/sec
 ZDOT =     -14536
279844                 ZDOT =       -4430
658096


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 35633U 09038A   09210
76758499  
00020000  00000-0  20000-3 0  9051
2 35633  51
6379  88
2123 0012289  43
4152 316
7978 15
76080458  2207


Satellite: SHUTTLE
Catalog Number: 35633
Epoch time:      09210
76758499   =   yrday
fracday
Element set:     905
Inclination:       51
6379  deg
RA of node:        88
2123  deg
Eccentricity:     
0012289     
Arg of perigee:    43
4152  deg
Mean anomaly:     316
7978  deg
Mean motion:   15
76080458  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             220
Checksum:              310


Coasting Arc #7 (Orbit 221)
---------------------------------------

Vector Time (GMT): 2009/210/20:16:31
141
Vector Time (MET): 013/22:13:21
193
Weight (LBS)     : 226160
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3979987
40                 A    =         6705959
74  meter
 Y    =        1520501
51  meter          E    =           
0003931
 Z    =        5178597
29                 I    =           51
95593
 XDOT =      -1318
313109                 Wp   =          348
34321
 YDOT =      -7501
827243  meter/sec      RA   =           87
07543  deg
 ZDOT =       1193
371952                 TA   =           90
34418
                                          MA   =           90
29914
                                          Ha   =            182
647  n
mi
                                          Hp   =            176
965

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13057701
45                 X    =        -4021850
67
 Y    =        4988522
03  feet           Y    =         1475760
35  meter
 Z    =       16990148
59                 Z    =         5159161
08
 XDOT =      -4325
174243                 XDOT =       -1240
125570
 YDOT =     -24612
294105  feet/sec       YDOT =       -7516
132348  meter/sec
 ZDOT =       3915
262309                 ZDOT =        1187
156752

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -427763
29                 X    =         -130382
25
 Y    =      -14063948
98  feet           Y    =        -4286691
65  meter
 Z    =       16913793
95                 Z    =         5155324
40
 XDOT =      23659
631979                 XDOT =        7211
455827
 YDOT =       3943
622862  feet/sec       YDOT =        1202
016248  meter/sec
 ZDOT =       3890
456742                 ZDOT =        1185
811215


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 35633U 09038A   09210
89427388  
00020000  00000-0  20000-3 0  9066
2 35633  51
6418  87
5598 0007349 326
5706  33
4995 15
79135945  2229


Satellite: SHUTTLE
Catalog Number: 35633
Epoch time:      09210
89427388   =   yrday
fracday
Element set:     906
Inclination:       51
6418  deg
RA of node:        87
5598  deg
Eccentricity:     
0007349     
Arg of perigee:   326
5706  deg
Mean anomaly:      33
4995  deg
Mean motion:   15
79135945  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             222
Checksum:              327


Coasting Arc #8 (Orbit 230)
---------------------------------------

Vector Time (GMT): 2009/211/11:03:48
419
Vector Time (MET): 014/13:00:38
471
Weight (LBS)     : 225779
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1838214
91                 A    =         6716762
03  meter
 Y    =        6278739
15  meter          E    =           
0017449
 Z    =       -1482451
24                 I    =           51
99143
 XDOT =      -4305
062424                 Wp   =           26
47919
 YDOT =       2628
456557  meter/sec      RA   =           83
88196  deg
 ZDOT =       5835
598842                 TA   =          317
23217
                                          MA   =          317
36781
                                          Ha   =            184
805  n
mi
                                          Hp   =            174
288

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6030888
81                 X    =         1775069
79
 Y    =       20599537
88  feet           Y    =         6298942
25  meter
 Z    =       -4863685
17                 Z    =        -1473673
91
 XDOT =     -14124
220550                 XDOT =       -4362
482425
 YDOT =       8623
545133  feet/sec       YDOT =        2579
993113  meter/sec
 ZDOT =      19145
665492                 ZDOT =        5814
545796

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16497693
74                 X    =         5028497
05
 Y    =      -13743221
58  feet           Y    =        -4188933
94  meter
 Z    =       -4828869
04                 Z    =        -1471839
28
 XDOT =      12566
826662                 XDOT =        3830
368767
 YDOT =       8435
428882  feet/sec       YDOT =        2571
118723  meter/sec
 ZDOT =      19063
001499                 ZDOT =        5810
402857


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 35633U 09038A   09211
46383264  
00020000  00000-0  20000-3 0  9075
2 35633  51
6426  84
6170 0009279  16
8831 343
2641 15
79096291  2314


Satellite: SHUTTLE
Catalog Number: 35633
Epoch time:      09211
46383264   =   yrday
fracday
Element set:     907
Inclination:       51
6426  deg
RA of node:        84
6170  deg
Eccentricity:     
0009279     
Arg of perigee:    16
8831  deg
Mean anomaly:     343
2641  deg
Mean motion:   15
79096291  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             231
Checksum:              291


Coasting Arc #9 (Orbit 235)
---------------------------------------

Vector Time (GMT): 2009/211/17:33:11
949
Vector Time (MET): 014/19:30:02
001
Weight (LBS)     : 225766
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3937923
96                 A    =         6706131
01  meter
 Y    =        1438652
87  meter          E    =           
0009176
 Z    =        5228008
82                 I    =           51
94982
 XDOT =      -1641
796325                 Wp   =           42
08605
 YDOT =      -7492
384473  meter/sec      RA   =           82
50436  deg
 ZDOT =        830
946972                 TA   =           40
08662
                                          MA   =           40
01895
                                          Ha   =            185
114  n
mi
                                          Hp   =            174
305

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12919698
02                 X    =        -3979115
10
 Y    =        4719989
75  feet           Y    =         1394385
78  meter
 Z    =       17152259
91                 Z    =         5208778
62
 XDOT =      -5386
470884                 XDOT =       -1561
929743
 YDOT =     -24581
313887  feet/sec       YDOT =       -7510
297541  meter/sec
 ZDOT =       2726
203977                 ZDOT =         823
164297

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8724913
27                 X    =         2659353
57
 Y    =      -10754484
42  feet           Y    =        -3277966
85  meter
 Z    =       17076705
58                 Z    =         5204979
86
 XDOT =      16512
923244                 XDOT =        5033
139005
 YDOT =      17645
766461  feet/sec       YDOT =        5378
429617  meter/sec
 ZDOT =       2695
243770                 ZDOT =         821
510301


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 35633U 09038A   09211
78026173  
00020000  00000-0  20000-3 0  9084
2 35633  51
6388  82
9739 0009074  21
8890 338
2661 15
78988366  2360


Satellite: SHUTTLE
Catalog Number: 35633
Epoch time:      09211
78026173   =   yrday
fracday
Element set:     908
Inclination:       51
6388  deg
RA of node:        82
9739  deg
Eccentricity:     
0009074     
Arg of perigee:    21
8890  deg
Mean anomaly:     338
2661  deg
Mean motion:   15
78988366  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             236
Checksum:              326


Coasting Arc #10 (Orbit 251)
---------------------------------------

Vector Time (GMT): 2009/212/17:35:52
083
Vector Time (MET): 015/19:32:42
135
Weight (LBS)     : 225766
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -55554
07                 A    =         6716359
79  meter
 Y    =        6436948
06  meter          E    =           
0021711
 Z    =        1871649
51                 I    =           51
98097
 XDOT =      -4936
163575                 Wp   =           51
07643
 YDOT =      -1703
951595  meter/sec      RA   =           77
35521  deg
 ZDOT =       5683
446808                 TA   =          329
67988
                                          MA   =          329
80530
                                          Ha   =            184
968  n
mi
                                          Hp   =            174
103

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -182264
01                 X    =         -136621
04
 Y    =       21118596
00  feet           Y    =         6435873
32  meter
 Z    =        6140582
38                 Z    =         1871183
53
 XDOT =     -16194
762384                 XDOT =       -4944
351724
 YDOT =      -5590
392372  feet/sec       YDOT =       -1759
197167  meter/sec
 ZDOT =      18646
479030                 ZDOT =        5659
447045

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11217675
22                 X    =        -3419147
41
 Y    =      -17894438
92  feet           Y    =        -5454224
98  meter
 Z    =        6139046
17                 Z    =         1871181
27
 XDOT =      15436
093165                 XDOT =        4704
921197
 YDOT =      -3277
896736  feet/sec       YDOT =        -999
102925  meter/sec
 ZDOT =      18552
015854                 ZDOT =        5654
654432


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 35633U 09038A   09212
79287254  
00020000  00000-0  20000-3 0  9096
2 35633  51
6402  77
7355 0008911  26
1791 333
9824 15
79038296  2520


Satellite: SHUTTLE
Catalog Number: 35633
Epoch time:      09212
79287254   =   yrday
fracday
Element set:     909
Inclination:       51
6402  deg
RA of node:        77
7355  deg
Eccentricity:     
0008911     
Arg of perigee:    26
1791  deg
Mean anomaly:     333
9824  deg
Mean motion:   15
79038296  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             252
Checksum:              308


Coasting Arc #11 (Orbit 266)
---------------------------------------

Vector Time (GMT): 2009/213/17:39:09
664
Vector Time (MET): 016/19:35:59
716
Weight (LBS)     : 225766
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4044873
55                 A    =         6713342
50  meter
 Y    =        4255244
75  meter          E    =           
0012374
 Z    =       -3254279
38                 I    =           51
96335
 XDOT =      -2113
885402                 Wp   =           46
66583
 YDOT =       5656
249131  meter/sec      RA   =           72
15061  deg
 ZDOT =       4788
172278                 TA   =          275
34347
                                          MA   =          275
48464
                                          Ha   =            185
135  n
mi
                                          Hp   =            174
006

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13270582
52                 X    =         4012798
55
 Y    =       13960776
75  feet           Y    =         4300297
98  meter
 Z    =      -10676769
63                 Z    =        -3234707
00
 XDOT =      -6935
319561                 XDOT =       -2200
237208
 YDOT =      18557
247804  feet/sec       YDOT =        5632
126992  meter/sec
 ZDOT =      15709
226633                 ZDOT =        4777
694135

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18894011
61                 X    =        -5758894
74
 Y    =       -3958516
85  feet           Y    =        -1206555
94  meter
 Z    =      -10599600
33                 Z    =        -3230758
18
 XDOT =      -5003
992626                 XDOT =       -1525
216952
 YDOT =     -17897
102587  feet/sec       YDOT =       -5455
036869  meter/sec
 ZDOT =      15668
270719                 ZDOT =        4775
688915


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 35633U 09038A   09213
74218523  
00020000  00000-0  20000-3 0  9107
2 35633  51
6407  72
8246 0009047  29
2519 330
9152 15
79024043  2675


Satellite: SHUTTLE
Catalog Number: 35633
Epoch time:      09213
74218523   =   yrday
fracday
Element set:     910
Inclination:       51
6407  deg
RA of node:        72
8246  deg
Eccentricity:     
0009047     
Arg of perigee:    29
2519  deg
Mean anomaly:     330
9152  deg
Mean motion:   15
79024043  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             267
Checksum:              274


Coasting Arc #12 (Orbit 282)
---------------------------------------

Vector Time (GMT): 2009/214/17:42:18
199
Vector Time (MET): 017/19:39:08
251
Weight (LBS)     : 225766
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3460936
35                 A    =         6705877
03  meter
 Y    =       -2370737
40  meter          E    =           
0021669
 Z    =       -5249374
83                 I    =           51
92836
 XDOT =       3518
488495                 Wp   =           65
01367
 YDOT =       6801
508067  meter/sec      RA   =           67
01984  deg
 ZDOT =       -745
395298                 TA   =          197
87912
                                          MA   =          197
95547
                                          Ha   =            185
097  n
mi
                                          Hp   =            173
856

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11354778
06                 X    =         3512689
21
 Y    =       -7778009
84  feet           Y    =        -2331745
17  meter
 Z    =      -17222358
38                 Z    =        -5232436
47
 XDOT =      11543
597423                 XDOT =        3445
792302
 YDOT =      22314
659014  feet/sec       YDOT =        6840
447494  meter/sec
 ZDOT =      -2445
522632                 ZDOT =        -728
478502

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4636322
22                 X    =        -1413151
01
 Y    =       13046826
54  feet           Y    =         3976672
73  meter
 Z    =      -17155841
09                 Z    =        -5229100
36
 XDOT =     -21565
737701                 XDOT =       -6573
236851
 YDOT =     -10819
873933  feet/sec       YDOT =       -3297
897575  meter/sec
 ZDOT =      -2378
684074                 ZDOT =        -725
022906


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 35633U 09038A   09214
75477040  
00020000  00000-0  20000-3 0  9111
2 35633  51
6410  67
5863 0009085  32
8597 327
3132 15
79067712  2839


Satellite: SHUTTLE
Catalog Number: 35633
Epoch time:      09214
75477040   =   yrday
fracday
Element set:     911
Inclination:       51
6410  deg
RA of node:        67
5863  deg
Eccentricity:     
0009085     
Arg of perigee:    32
8597  deg
Mean anomaly:     327
3132  deg
Mean motion:   15
79067712  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             283
Checksum:              292

SPACE SHUTTLE ORBITAL DATA:

The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:

NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission

By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command

   David Cottle
   Director Of Engineering
   IDB Communications

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