Date: February 19th 2010

SHUTTLE TRAJECTORY DATA

Lift off time (UTC) : 2010/039/09:14:06 981 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 77 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 07 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 07803

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


049/07:10:38 104 -0 1 0 6 0 6
009/21:56:31 123 0 6 -0 0 188 8
000/00:00:02 246 -0 2 0 0 180 6

049/08:10:37 680 0 3 0 4 0 4
009/22:56:30 699 -0 2 -0 0 190 4
000/00:00:01 399 -0 1 0 0 180 8

051/00:10:07 265 -0 1 -0 1 0 2
011/14:56:00 284 -0 1 0 0 190 7
000/00:00:00 568 0 1 0 0 180 2

051/02:09:12 568 0 2 -0 0 3 0
011/16:55:05 587 2 6 -0 0 190 3
000/00:00:11 174 -1 4 -3 0 180 4

051/02:37:12 566 -0 6 -3 0 3 0
011/17:23:05 585 2 9 0 0 189 2
000/00:00:11 170 -0 6 0 0 180 3

052/08:05:17 154 -14 3 -33 0 33 0
012/22:51:10 173 -18 2 -0 0 189 0
000/00:00:20 345 23 5 0 4 161 2

Coasting Arc #1 (Orbit 150)
---------------------------------------

Vector Time (GMT): 2010/048/20:39:22
000
Vector Time (MET): 009/11:25:15
019
Weight (LBS)     : 210189
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3420263
16                 A    =         6713871
88  meter
 Y    =        2347441
64  meter          E    =           
0015455
 Z    =       -5288242
41                 I    =           51
90777
 XDOT =      -4208
837679                 Wp   =           46
13680
 YDOT =       6442
388452  meter/sec      RA   =          122
29079  deg
 ZDOT =        148
365845                 TA   =          225
20377
                                          MA   =          225
32955
                                          Ha   =            188
891  n
mi
                                          Hp   =            180
220

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11221335
82                 X    =         3419434
81
 Y    =        7701580
17  feet           Y    =         2385703
61  meter
 Z    =      -17349876
67                 Z    =        -5271629
15
 XDOT =     -13808
522569                 XDOT =       -4281
321903
 YDOT =      21136
445051  feet/sec       YDOT =        6394
893308  meter/sec
 ZDOT =        486
764584                 ZDOT =         127
743250

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6310014
70                 X    =         1923292
48
 Y    =      -12153356
87  feet           Y    =        -3704343
17  meter
 Z    =      -17283823
84                 Z    =        -5268109
51
 XDOT =      21733
408193                 XDOT =        6624
342817
 YDOT =      10758
113737  feet/sec       YDOT =        3279
073067  meter/sec
 ZDOT =        405
134778                 ZDOT =         123
485080


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 36394U 10004A   10048
87631641  
00020000  00000-0  20000-3 0  9008
2 36394  51
6445 123
1243 0011690 340
2070  19
8639 15
76188562  1513


Satellite: SHUTTLE
Catalog Number: 36394
Epoch time:      10048
87631641   =   yrday
fracday
Element set:     900
Inclination:       51
6445  deg
RA of node:       123
1243  deg
Eccentricity:     
0011690     
Arg of perigee:   340
2070  deg
Mean anomaly:      19
8639  deg
Mean motion:   15
76188562  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             151
Checksum:              278


Coasting Arc #2 (Orbit 157)
---------------------------------------

Vector Time (GMT): 2010/049/07:10:39
227
Vector Time (MET): 009/21:56:32
246
Weight (LBS)     : 210174
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4780042
12                 A    =         6717034
44  meter
 Y    =       -1042581
49  meter          E    =           
0015137
 Z    =       -4614202
65                 I    =           51
92413
 XDOT =      -1351
098972                 Wp   =           22
96775
 YDOT =       6970
478512  meter/sec      RA   =          120
06065  deg
 ZDOT =      -2964
254766                 TA   =          217
67736
                                          MA   =          217
78347
                                          Ha   =            188
763  n
mi
                                          Hp   =            180
580

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15682552
88                 X    =         4813765
47
 Y    =       -3420542
93  feet           Y    =         -988912
58  meter
 Z    =      -15138460
15                 Z    =        -4590899
57
 XDOT =      -4432
739409                 XDOT =       -1414
583630
 YDOT =      22869
023989  feet/sec       YDOT =        6955
006758  meter/sec
 ZDOT =      -9725
245296                 ZDOT =       -2970
972836

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -767328
19                 X    =         -233881
63
 Y    =       16119720
22  feet           Y    =         4913290
72  meter
 Z    =      -15045975
61                 Z    =        -4586013
37
 XDOT =     -19788
065976                 XDOT =       -6031
402509
 YDOT =     -10076
041330  feet/sec       YDOT =       -3071
177397  meter/sec
 ZDOT =      -9751
651868                 ZDOT =       -2972
303489


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 36394U 10004A   10049
32012177  
00020000  00000-0  20000-3 0  9017
2 36394  51
6441 120
8341 0011110 339
2504  20
8208 15
76109838  1589


Satellite: SHUTTLE
Catalog Number: 36394
Epoch time:      10049
32012177   =   yrday
fracday
Element set:     901
Inclination:       51
6441  deg
RA of node:       120
8341  deg
Eccentricity:     
0011110     
Arg of perigee:   339
2504  deg
Mean anomaly:      20
8208  deg
Mean motion:   15
76109838  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             158
Checksum:              253


Coasting Arc #3 (Orbit 158)
---------------------------------------

Vector Time (GMT): 2010/049/08:10:38
380
Vector Time (MET): 009/22:56:31
399
Weight (LBS)     : 210165
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1657499
13                 A    =         6718506
96  meter
 Y    =       -4511119
79  meter          E    =           
0015998
 Z    =        4697905
09                 I    =           51
92425
 XDOT =       5290
346637                 Wp   =           15
51218
 YDOT =      -4855
854855  meter/sec      RA   =          119
80350  deg
 ZDOT =      -2779
015691                 TA   =          101
86641
                                          MA   =          101
68696
                                          Ha   =            190
399  n
mi
                                          Hp   =            180
824

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5437989
27                 X    =        -1629727
30
 Y    =      -14800261
76  feet           Y    =        -4529508
78  meter
 Z    =       15413074
45                 Z    =         4689920
73
 XDOT =      17356
780306                 XDOT =        5357
779538
 YDOT =     -15931
282332  feet/sec       YDOT =       -4796
287860  meter/sec
 ZDOT =      -9117
505548                 ZDOT =       -2753
151522

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14792760
46                 X    =         4508833
39
 Y    =       -5547546
27  feet           Y    =        -1690892
10  meter
 Z    =       15381199
82                 Z    =         4688189
71
 XDOT =      15549
406718                 XDOT =        4739
459168
 YDOT =      16310
777014  feet/sec       YDOT =        4971
524834  meter/sec
 ZDOT =      -9014
998081                 ZDOT =       -2747
771415


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 36394U 10004A   10049
38355280  
00020000  00000-0  20000-3 0  9029
2 36394  51
6449 120
5074 0012109 347
1064  12
9788 15
75443676  1591


Satellite: SHUTTLE
Catalog Number: 36394
Epoch time:      10049
38355280   =   yrday
fracday
Element set:     902
Inclination:       51
6449  deg
RA of node:       120
5074  deg
Eccentricity:     
0012109     
Arg of perigee:   347
1064  deg
Mean anomaly:      12
9788  deg
Mean motion:   15
75443676  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             159
Checksum:              297


Coasting Arc #4 (Orbit 174)
---------------------------------------

Vector Time (GMT): 2010/050/08:15:18
594
Vector Time (MET): 010/23:01:11
613
Weight (LBS)     : 210165
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4687444
60                 A    =         6720428
23  meter
 Y    =        2466054
36  meter          E    =           
0012459
 Z    =        4123100
39                 I    =           51
94650
 XDOT =       -188
441439                 Wp   =           40
90085
 YDOT =      -6706
854803  meter/sec      RA   =          114
70785  deg
 ZDOT =       3799
992460                 TA   =           10
36794
                                          MA   =           10
34227
                                          Ha   =            190
482  n
mi
                                          Hp   =            180
406

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15378755
26                 X    =        -4734714
88
 Y    =        8090729
52  feet           Y    =         2413345
60  meter
 Z    =       13527232
26                 Z    =         4100214
12
 XDOT =       -618
246190                 XDOT =        -131
851514
 YDOT =     -22004
116808  feet/sec       YDOT =       -6708
646441  meter/sec
 ZDOT =      12467
166863                 ZDOT =        3799
214699

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8686477
31                 X    =        -2647638
28
 Y    =      -15131389
98  feet           Y    =        -4612047
67  meter
 Z    =       13436449
66                 Z    =         4095429
86
 XDOT =      20856
849965                 XDOT =        6357
167869
 YDOT =       -913
840355  feet/sec       YDOT =        -278
538540  meter/sec
 ZDOT =      12463
831189                 ZDOT =        3798
975746


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 36394U 10004A   10050
39841593  
00020000  00000-0  20000-3 0  9030
2 36394  51
6457 115
2843 0012183 350
3472   9
7456 15
75556134  1754


Satellite: SHUTTLE
Catalog Number: 36394
Epoch time:      10050
39841593   =   yrday
fracday
Element set:     903
Inclination:       51
6457  deg
RA of node:       115
2843  deg
Eccentricity:     
0012183     
Arg of perigee:   350
3472  deg
Mean anomaly:       9
7456  deg
Mean motion:   15
75556134  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             175
Checksum:              291


Coasting Arc #5 (Orbit 184)
---------------------------------------

Vector Time (GMT): 2010/051/00:10:07
549
Vector Time (MET): 011/14:56:00
568
Weight (LBS)     : 210161
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4207350
80                 A    =         6723863
21  meter
 Y    =       -4306655
54  meter          E    =           
0011507
 Z    =       -3009700
27                 I    =           51
96680
 XDOT =       2045
335394                 Wp   =           13
38321
 YDOT =       5487
508635  meter/sec      RA   =          111
31353  deg
 ZDOT =      -4985
810176                 TA   =          201
20538
                                          MA   =          201
25311
                                          Ha   =            190
675  n
mi
                                          Hp   =            180
164

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13803644
34                 X    =         4269840
56
 Y    =      -14129447
31  feet           Y    =        -4259233
00  meter
 Z    =       -9874344
71                 Z    =        -2989109
26
 XDOT =       6710
417960                 XDOT =        2008
009680
 YDOT =      18003
637253  feet/sec       YDOT =        5510
183506  meter/sec
 ZDOT =     -16357
644935                 ZDOT =       -4975
964817

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18914842
16                 X    =        -5765243
89
 Y    =        5832291
16  feet           Y    =         1777682
35  meter
 Z    =       -9792736
49                 Z    =        -2984826
08
 XDOT =       3004
889926                 XDOT =         915
890449
 YDOT =     -17693
993538  feet/sec       YDOT =       -5393
129230  meter/sec
 ZDOT =     -16318
354384                 ZDOT =       -4973
834416


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 36394U 10004A   10051
03269150  
00020000  00000-0  20000-3 0  9046
2 36394  51
6464 112
0249 0012884 352
9254   7
1726 15
75561651  1854


Satellite: SHUTTLE
Catalog Number: 36394
Epoch time:      10051
03269150   =   yrday
fracday
Element set:     904
Inclination:       51
6464  deg
RA of node:       112
0249  deg
Eccentricity:     
0012884     
Arg of perigee:   352
9254  deg
Mean anomaly:       7
1726  deg
Mean motion:   15
75561651  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             185
Checksum:              277


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

Vector Time (GMT): 2010/051/02:09:18
155
Vector Time (MET): 011/16:55:11
174
Weight (LBS)     : 210088
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         322664
81                 A    =         6723493
62  meter
 Y    =        5953808
27  meter          E    =           
0013398
 Z    =       -3092923
46                 I    =           51
96440
 XDOT =      -5203
861559                 Wp   =            8
17528
 YDOT =       2834
077920  meter/sec      RA   =          110
83867  deg
 ZDOT =       4928
200651                 TA   =          316
04869
                                          MA   =          316
15517
                                          Ha   =            190
334  n
mi
                                          Hp   =            180
416

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1058611
59                 X    =          271055
13
 Y    =       19533491
71  feet           Y    =         5957129
56  meter
 Z    =      -10147386
67                 Z    =        -3091481
45
 XDOT =     -17073
036611                 XDOT =       -5259
121838
 YDOT =       9298
155904  feet/sec       YDOT =        2775
546619  meter/sec
 ZDOT =      16168
637307                 ZDOT =        4902
786238

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1616753
98                 X    =         -492786
61
 Y    =      -19498321
67  feet           Y    =        -5943088
44  meter
 Z    =      -10141448
22                 Z    =        -3091113
42
 XDOT =      15502
810182                 XDOT =        4725
256544
 YDOT =      -9616
086305  feet/sec       YDOT =       -2930
983106  meter/sec
 ZDOT =      16067
822679                 ZDOT =        4897
472352


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 36394U 10004A   10051
09611665  
00020000  00000-0  20000-3 0  9055
2 36394  51
6440 111
6965 0012387 348
3043  11
7832 15
75585862  1861


Satellite: SHUTTLE
Catalog Number: 36394
Epoch time:      10051
09611665   =   yrday
fracday
Element set:     905
Inclination:       51
6440  deg
RA of node:       111
6965  deg
Eccentricity:     
0012387     
Arg of perigee:   348
3043  deg
Mean anomaly:      11
7832  deg
Mean motion:   15
75585862  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             186
Checksum:              293


Coasting Arc #7 (Orbit 186)
---------------------------------------

Vector Time (GMT): 2010/051/02:37:18
150
Vector Time (MET): 011/17:23:11
170
Weight (LBS)     : 210015
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4358237
23                 A    =         6714937
98  meter
 Y    =         226062
26  meter          E    =           
0008657
 Z    =        5101942
31                 I    =           51
94031
 XDOT =       1471
308197                 Wp   =          356
03632
 YDOT =      -7394
435832  meter/sec      RA   =          110
77636  deg
 ZDOT =       1593
087046                 TA   =           78
78990
                                          MA   =           78
69261
                                          Ha   =            189
209  n
mi
                                          Hp   =            180
260

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14298678
56                 X    =        -4385226
28
 Y    =         741674
07  feet           Y    =          177150
19  meter
 Z    =       16738655
87                 Z    =         5080704
63
 XDOT =       4827
126631                 XDOT =        1546
187851
 YDOT =     -24259
960079  feet/sec       YDOT =       -7377
555500  meter/sec
 ZDOT =       5226
663536                 ZDOT =        1600
416631

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14129828
03                 X    =         4306771
58
 Y    =       -2857628
01  feet           Y    =         -871005
02  meter
 Z    =       16654333
12                 Z    =         5076240
73
 XDOT =      -1373
654643                 XDOT =        -418
689935
 YDOT =      23671
592877  feet/sec       YDOT =        7215
101509  meter/sec
 ZDOT =       5255
504199                 ZDOT =        1601
877680


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 36394U 10004A   10051
15952133  
00020000  00000-0  20000-3 0  9061
2 36394  51
6436 111
3695 0012412 338
3010  21
7627 15
76107191  1875


Satellite: SHUTTLE
Catalog Number: 36394
Epoch time:      10051
15952133   =   yrday
fracday
Element set:     906
Inclination:       51
6436  deg
RA of node:       111
3695  deg
Eccentricity:     
0012412     
Arg of perigee:   338
3010  deg
Mean anomaly:      21
7627  deg
Mean motion:   15
76107191  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             187
Checksum:              263


Coasting Arc #8 (Orbit 202)
---------------------------------------

Vector Time (GMT): 2010/052/02:41:47
120
Vector Time (MET): 012/17:27:40
139
Weight (LBS)     : 210015
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2491735
79                 A    =         6725676
57  meter
 Y    =        6159773
65  meter          E    =           
0020905
 Z    =         947200
18                 I    =           51
98572
 XDOT =      -4128
029012                 Wp   =           20
48822
 YDOT =      -2592
364673  meter/sec      RA   =          105
62644  deg
 ZDOT =       5979
042463                 TA   =          349
83050
                                          MA   =          349
87273
                                          Ha   =            189
190  n
mi
                                          Hp   =            179
953

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8174986
18                 X    =        -2565066
44
 Y    =       20209231
15  feet           Y    =         6131485
19  meter
 Z    =        3107612
14                 Z    =          934917
30
 XDOT =     -13543
402269                 XDOT =       -4127
763756
 YDOT =      -8505
133440  feet/sec       YDOT =       -2638
548722  meter/sec
 ZDOT =      19616
281046                 ZDOT =        5958
989336

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4338714
19                 X    =         1322440
08
 Y    =      -21370972
74  feet           Y    =        -6513872
49  meter
 Z    =        3059045
51                 Z    =          932397
07
 XDOT =      13430
601591                 XDOT =        4093
647365
 YDOT =       5532
741066  feet/sec       YDOT =        1686
379477  meter/sec
 ZDOT =      19536
560867                 ZDOT =        5954
743752


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 36394U 10004A   10052
17396346  
00020000  00000-0  20000-3 0  9073
2 36394  51
6428 106
1426 0012381 341
7452  18
3267 15
76159582  2035


Satellite: SHUTTLE
Catalog Number: 36394
Epoch time:      10052
17396346   =   yrday
fracday
Element set:     907
Inclination:       51
6428  deg
RA of node:       106
1426  deg
Eccentricity:     
0012381     
Arg of perigee:   341
7452  deg
Mean anomaly:      18
3267  deg
Mean motion:   15
76159582  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             203
Checksum:              285


Coasting Arc #9 (Orbit 205)
---------------------------------------

Vector Time (GMT): 2010/052/08:05:27
326
Vector Time (MET): 012/22:51:20
345
Weight (LBS)     : 209330
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3300104
87                 A    =         6706079
75  meter
 Y    =       -5362054
35  meter          E    =           
0033014
 Z    =       -2371724
79                 I    =           51
98379
 XDOT =       3236
738252                 Wp   =           20
77450
 YDOT =       4389
685744  meter/sec      RA   =          104
48440  deg
 ZDOT =      -5413
291153                 TA   =          185
80510
                                          MA   =          185
84346
                                          Ha   =            188
982  n
mi
                                          Hp   =            161
200

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10827115
72                 X    =         3371370
64
 Y    =      -17592041
84  feet           Y    =        -5324733
18  meter
 Z    =       -7781249
31                 Z    =        -2355519
93
 XDOT =      10619
219988                 XDOT =        3213
682809
 YDOT =      14401
856116  feet/sec       YDOT =        4425
770313  meter/sec
 ZDOT =     -17760
141579                 ZDOT =       -5397
623227

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17912654
68                 X    =         5459777
15
 Y    =       10336233
26  feet           Y    =         3150483
90  meter
 Z    =       -7717078
20                 Z    =        -2352165
43
 XDOT =     -13317
184146                 XDOT =       -4059
077728
 YDOT =       9847
355747  feet/sec       YDOT =        3001
474032  meter/sec
 ZDOT =     -17697
774878                 ZDOT =       -5394
281783


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 36394U 10004A   10052
36408747  
00020000  00000-0  20000-3 0  9084
2 36394  51
6459 105
1610 0035716  12
3904 347
8134 15
82353967  2069


Satellite: SHUTTLE
Catalog Number: 36394
Epoch time:      10052
36408747   =   yrday
fracday
Element set:     908
Inclination:       51
6459  deg
RA of node:       105
1610  deg
Eccentricity:     
0035716     
Arg of perigee:    12
3904  deg
Mean anomaly:     347
8134  deg
Mean motion:   15
82353967  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             206
Checksum:              290


Coasting Arc #10 (Orbit 221)
---------------------------------------

Vector Time (GMT): 2010/053/08:06:30
656
Vector Time (MET): 013/22:52:23
675
Weight (LBS)     : 209330
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -999793
59                 A    =         6705697
57  meter
 Y    =       -6141776
58  meter          E    =           
0038791
 Z    =        2527362
97                 I    =           51
98914
 XDOT =       4698
110844                 Wp   =           37
23469
 YDOT =      -2983
078278  meter/sec      RA   =           99
26288  deg
 ZDOT =      -5318
229267                 TA   =          114
23611
                                          MA   =          113
83030
                                          Ha   =            189
105  n
mi
                                          Hp   =            160
898

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3280162
70                 X    =         -943283
17
 Y    =      -20150185
63  feet           Y    =        -6152646
47  meter
 Z    =        8291873
28                 Z    =         2522643
20
 XDOT =      15413
749488                 XDOT =        4756
970336
 YDOT =      -9787
002226  feet/sec       YDOT =       -2930
185133  meter/sec
 ZDOT =     -17448
258751                 ZDOT =       -5295
263201

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19949580
09                 X    =         6080632
01
 Y    =       -4372350
98  feet           Y    =        -1332692
58  meter
 Z    =        8272932
47                 Z    =         2521589
82
 XDOT =      10262
335436                 XDOT =        3127
959841
 YDOT =      13531
216406  feet/sec       YDOT =        4124
314761  meter/sec
 ZDOT =     -17357
146430                 ZDOT =       -5290
458232


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 36394U 10004A   10053
37455726  
00020000  00000-0  20000-3 0  9096
2 36394  51
6460  99
9080 0035700  16
3235 343
9074 15
82366401  2221


Satellite: SHUTTLE
Catalog Number: 36394
Epoch time:      10053
37455726   =   yrday
fracday
Element set:     909
Inclination:       51
6460  deg
RA of node:        99
9080  deg
Eccentricity:     
0035700     
Arg of perigee:    16
3235  deg
Mean anomaly:     343
9074  deg
Mean motion:   15
82366401  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             222
Checksum:              284


Coasting Arc #11 (Orbit 237)
---------------------------------------

Vector Time (GMT): 2010/054/08:07:42
952
Vector Time (MET): 014/22:53:35
971
Weight (LBS)     : 209330
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4026990
90                 A    =         6696252
38  meter
 Y    =       -1072650
41  meter          E    =           
0038048
 Z    =        5232209
14                 I    =           51
96256
 XDOT =       1086
289653                 Wp   =           22
95121
 YDOT =      -7615
726685  meter/sec      RA   =           94
09867  deg
 ZDOT =       -689
194105                 TA   =           73
76316
                                          MA   =           73
34489
                                          Ha   =            189
211  n
mi
                                          Hp   =            160
492

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13211912
41                 X    =        -4040107
40
 Y    =       -3519194
26  feet           Y    =        -1117779
04  meter
 Z    =       17166040
49                 Z    =         5212614
45
 XDOT =       3563
942431                 XDOT =        1174
760504
 YDOT =     -24985
979938  feet/sec       YDOT =       -7603
078033  meter/sec
 ZDOT =      -2261
135516                 ZDOT =        -683
702307

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2518040
70                 X    =          767498
81
 Y    =      -13537569
85  feet           Y    =        -4126251
29  meter
 Z    =       17088182
40                 Z    =         5208477
99
 XDOT =      24195
818210                 XDOT =        7374
885390
 YDOT =       1523
672056  feet/sec       YDOT =         464
415243  meter/sec
 ZDOT =      -2239
557094                 ZDOT =        -682
617002


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 36394U 10004A   10054
38499942  
00020000  00000-0  20000-3 0  9108
2 36394  51
6468  94
6542 0035772  20
0174 340
2387 15
82457818  2384


Satellite: SHUTTLE
Catalog Number: 36394
Epoch time:      10054
38499942   =   yrday
fracday
Element set:     910
Inclination:       51
6468  deg
RA of node:        94
6542  deg
Eccentricity:     
0035772     
Arg of perigee:    20
0174  deg
Mean anomaly:     340
2387  deg
Mean motion:   15
82457818  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             238
Checksum:              309


Coasting Arc #12 (Orbit 253)
---------------------------------------

Vector Time (GMT): 2010/055/08:08:37
984
Vector Time (MET): 015/22:54:31
004
Weight (LBS)     : 209330
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2580020
78                 A    =         6703043
61  meter
 Y    =        5118623
89  meter          E    =           
0042231
 Z    =        3419842
45                 I    =           51
98654
 XDOT =      -3714
611723                 Wp   =           39
73904
 YDOT =      -4968
569885  meter/sec      RA   =           88
95247  deg
 ZDOT =       4635
183708                 TA   =             
82582
                                          MA   =             
81887
                                          Ha   =            189
262  n
mi
                                          Hp   =            160
180

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8464635
10                 X    =        -2653707
96
 Y    =       16793385
45  feet           Y    =         5089345
58  meter
 Z    =       11219955
53                 Z    =         3407130
12
 XDOT =     -12187
046336                 XDOT =       -3681
264122
 YDOT =     -16301
082299  feet/sec       YDOT =       -5009
943581  meter/sec
 ZDOT =      15207
295629                 ZDOT =        4617
219373

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17532088
54                 X    =        -5343780
59
 Y    =       -6886280
30  feet           Y    =        -2098938
23  meter
 Z    =       11169613
23                 Z    =         3404498
11
 XDOT =      14550
608805                 XDOT =        4435
025564
 YDOT =     -12499
540967  feet/sec       YDOT =       -3809
860087  meter/sec
 ZDOT =      15135
791920                 ZDOT =        4613
389377


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 36394U 10004A   10055
39541599  
00020000  00000-0  20000-3 0  9117
2 36394  51
6467  89
4014 0035730  24
1553 336
1280 15
82475460  2546


Satellite: SHUTTLE
Catalog Number: 36394
Epoch time:      10055
39541599   =   yrday
fracday
Element set:     911
Inclination:       51
6467  deg
RA of node:        89
4014  deg
Eccentricity:     
0035730     
Arg of perigee:    24
1553  deg
Mean anomaly:     336
1280  deg
Mean motion:   15
82475460  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             254
Checksum:              290

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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