Date: February 8th 2010

SHUTTLE TRAJECTORY DATA

Lift off time (UTC) : 2010/039/09:14:08 000 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 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


039/09:25:21 852 0 0 0 0 0 0
000/00:11:13 852 0 0 0 0 123 8
000/00:00:00 000 0 0 0 0 31 4

039/09:52:40 625 30 0 143 3 143 3
000/00:38:32 625 84 7 -0 1 123 6
000/00:01:36 051 -111 7 -1 4 109 9

039/12:05:40 001 -23 3 109 2 109 2
000/02:51:32 001 -64 3 0 0 185 3
000/00:01:12 889 85 1 -0 0 110 1

040/02:25:22 965 3 5 92 0 93 3
000/17:11:14 965 59 5 -1 7 186 8
000/00:05:52 321 -71 8 -15 8 161 4

040/11:28:54 433 0 0 0 0 0 0
001/02:14:46 433 0 0 0 0 186 8
000/00:00:00 000 0 0 0 0 162 9

041/00:57:05 844 15 7 23 5 23 5
001/15:42:57 844 8 0 -0 0 187 2
000/00:00:17 543 -15 7 0 0 176 0

041/02:28:34 983 6 0 9 0 9 0
001/17:14:26 983 3 0 -0 0 187 4
000/00:00:13 966 -6 0 -0 2 181 3

041/03:45:28 864 2 7 2 5 3 1
001/18:31:20 864 0 5 -0 1 187 8
000/00:00:13 728 -1 6 2 0 182 4

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

Vector Time (GMT): 2010/039/09:24:36
680
Vector Time (MET): 000/00:10:28
680
Weight (LBS)     : 256427
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3772582
57                 A    =         6518583
01  meter
 Y    =       -2924310
93  meter          E    =           
0127561
 Z    =        4390698
74                 I    =           51
68262
 XDOT =       6268
293087                 Wp   =          352
38395
 YDOT =      -3517
886256  meter/sec      RA   =          171
15300  deg
 ZDOT =       3178
749836                 TA   =           67
25651
                                          MA   =           65
91344
                                          Ha   =            123
811  n
mi
                                          Hp   =             31
427

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12377239
40                 X    =        -3760930
79
 Y    =       -9594195
98  feet           Y    =        -2966433
24  meter
 Z    =       14405179
58                 Z    =         4372400
08
 XDOT =      20565
266033                 XDOT =        6291
723375
 YDOT =     -11541
621575  feet/sec       YDOT =       -3447
659629  meter/sec
 ZDOT =      10428
969279                 ZDOT =        3209
257314

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7583753
12                 X    =         2311527
95
 Y    =      -13777550
03  feet           Y    =        -4199397
25  meter
 Z    =       14332468
53                 Z    =         4368536
41
 XDOT =      13525
116039                 XDOT =        4122
455369
 YDOT =      17953
420977  feet/sec       YDOT =        5472
202714  meter/sec
 ZDOT =      10549
860836                 ZDOT =        3215
597583


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 00130U          10039
44229781  
00020000  00000-0  20000-3 0  9003
2 00130  51
6433 171
8651 0026054 168
8984 191
2825 16
95278905    20


Satellite: SHUTTLE
Catalog Number: 00130
Epoch time:      10039
44229781   =   yrday
fracday
Element set:     900
Inclination:       51
6433  deg
RA of node:       171
8651  deg
Eccentricity:     
0026054     
Arg of perigee:   168
8984  deg
Mean anomaly:     191
2825  deg
Mean motion:   16
95278905  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:               2
Checksum:              265


Coasting Arc #2 (Orbit 1)
---------------------------------------

Vector Time (GMT): 2010/039/09:25:21
852
Vector Time (MET): 000/00:11:13
852
Weight (LBS)     : 256427
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3483962
18                 A    =         6517955
10  meter
 Y    =       -3078796
82  meter          E    =           
0127543
 Z    =        4527672
36                 I    =           51
68061
 XDOT =       6507
070578                 Wp   =          351
92491
 YDOT =      -3320
324878  meter/sec      RA   =          171
14835  deg
 ZDOT =       2884
331656                 TA   =           70
85262
                                          MA   =           69
47630
                                          Ha   =            123
774  n
mi
                                          Hp   =             31
410

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11430322
10                 X    =        -3471269
74
 Y    =      -10101039
42  feet           Y    =        -3117685
79  meter
 Z    =       14854568
10                 Z    =         4510778
31
 XDOT =      21348
656751                 XDOT =        6529
704154
 YDOT =     -10893
454325  feet/sec       YDOT =       -3247
432541  meter/sec
 ZDOT =       9463
030367                 ZDOT =        2915
997164

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8185892
14                 X    =         2495059
92
 Y    =      -12948541
78  feet           Y    =        -3946715
53  meter
 Z    =       14787423
37                 Z    =         4507206
64
 XDOT =      13128
953582                 XDOT =        4001
705052
 YDOT =      18741
828050  feet/sec       YDOT =        5712
509189  meter/sec
 ZDOT =       9588
523952                 ZDOT =        2922
582101


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 00130U          10039
44230842  
00020000  00000-0  20000-3 0  9014
2 00130  51
6433 171
8651 0025071 168
8655 191
3137 16
94997127    23


Satellite: SHUTTLE
Catalog Number: 00130
Epoch time:      10039
44230842   =   yrday
fracday
Element set:     901
Inclination:       51
6433  deg
RA of node:       171
8651  deg
Eccentricity:     
0025071     
Arg of perigee:   168
8655  deg
Mean anomaly:     191
3137  deg
Mean motion:   16
94997127  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:               2
Checksum:              249


Coasting Arc #3 (Orbit 1)
---------------------------------------

Vector Time (GMT): 2010/039/09:53:28
651
Vector Time (MET): 000/00:39:20
651
Weight (LBS)     : 252810
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6487654
32                 A    =         6600353
33  meter
 Y    =       -1225170
80  meter          E    =           
0010438
 Z    =         249202
45                 I    =           51
71489
 XDOT =       1116
974055                 Wp   =          342
88466
 YDOT =       4687
512596  meter/sec      RA   =          171
01310  deg
 ZDOT =      -6086
739745                 TA   =          194
36111
                                          MA   =          194
39079
                                          Ha   =            123
618  n
mi
                                          Hp   =            109
934

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21284955
11                 X    =         6499661
66
 Y    =       -4019589
22  feet           Y    =        -1152554
88  meter
 Z    =         817593
33                 Z    =          280747
92
 XDOT =       3664
613040                 XDOT =        1094
042099
 YDOT =      15378
978332  feet/sec       YDOT =        4699
875320  meter/sec
 ZDOT =     -19969
618586                 ZDOT =       -6081
369086

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9728565
18                 X    =         2965266
67
 Y    =       19347899
57  feet           Y    =         5897239
79  meter
 Z    =         942693
98                 Z    =          287333
12
 XDOT =     -12329
789224                 XDOT =       -3758
119755
 YDOT =       7164
243205  feet/sec       YDOT =        2183
661329  meter/sec
 ZDOT =     -19948
126220                 ZDOT =       -6080
188872


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 00130U          10039
44348535  
00020000  00000-0  20000-3 0  9024
2 00130  51
6434 171
8762 0022791 325
7743  34
1975 16
21494072    20


Satellite: SHUTTLE
Catalog Number: 00130
Epoch time:      10039
44348535   =   yrday
fracday
Element set:     902
Inclination:       51
6434  deg
RA of node:       171
8762  deg
Eccentricity:     
0022791     
Arg of perigee:   325
7743  deg
Mean anomaly:      34
1975  deg
Mean motion:   16
21494072  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:               2
Checksum:              246


Coasting Arc #4 (Orbit 2)
---------------------------------------

Vector Time (GMT): 2010/039/12:06:16
445
Vector Time (MET): 000/02:52:08
445
Weight (LBS)     : 250090
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6429103
98                 A    =         6657711
73  meter
 Y    =        1364396
37  meter          E    =           
0113591
 Z    =        -361290
24                 I    =           51
72091
 XDOT =      -1342
470188                 Wp   =          352
67965
 YDOT =      -4678
611181  meter/sec      RA   =          170
50471  deg
 ZDOT =       6128
000453                 TA   =            3
31085
                                          MA   =            3
23631
                                          Ha   =            185
261  n
mi
                                          Hp   =            110
105

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21092860
82                 X    =        -6442128
03
 Y    =        4476366
03  feet           Y    =         1292429
51  meter
 Z    =       -1185335
42                 Z    =         -392553
73
 XDOT =      -4404
429750                 XDOT =       -1319
821432
 YDOT =     -15349
774215  feet/sec       YDOT =       -4693
497122  meter/sec
 ZDOT =      20104
988364                 ZDOT =        6121
533672

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18902452
25                 X    =        -5761467
45
 Y    =      -10360243
61  feet           Y    =        -3157802
25  meter
 Z    =       -1309313
44                 Z    =         -399078
74
 XDOT =       5828
279193                 XDOT =        1776
459498
 YDOT =     -13206
091754  feet/sec       YDOT =       -4025
216767  meter/sec
 ZDOT =      20079
147476                 ZDOT =        6120
124151


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 00130U          10039
50511312  
00020000  00000-0  20000-3 0  9037
2 00130  51
6470 171
5371 0106382 347
5295  12
3253 16
00537988    35


Satellite: SHUTTLE
Catalog Number: 00130
Epoch time:      10039
50511312   =   yrday
fracday
Element set:     903
Inclination:       51
6470  deg
RA of node:       171
5371  deg
Eccentricity:     
0106382     
Arg of perigee:   347
5295  deg
Mean anomaly:      12
3253  deg
Mean motion:   16
00537988  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:               3
Checksum:              224


Coasting Arc #5 (Orbit 12)
---------------------------------------

Vector Time (GMT): 2010/040/02:28:19
125
Vector Time (MET): 000/17:14:11
125
Weight (LBS)     : 247708
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6241373
04                 A    =         6704301
91  meter
 Y    =         548188
89  meter          E    =           
0034667
 Z    =       -2411790
31                 I    =           51
72789
 XDOT =      -2531
037634                 Wp   =          320
90672
 YDOT =       4907
868897  meter/sec      RA   =          167
33943  deg
 ZDOT =      -5366
286444                 TA   =          246
32477
                                          MA   =          246
68897
                                          Ha   =            186
797  n
mi
                                          Hp   =            161
387

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20476945
68                 X    =         6246494
99
 Y    =        1798519
99  feet           Y    =          618012
37  meter
 Z    =       -7912697
88                 Z    =        -2381457
98
 XDOT =      -8303
929247                 XDOT =       -2559
662356
 YDOT =      16101
932078  feet/sec       YDOT =        4879
405521  meter/sec
 ZDOT =     -17605
926652                 ZDOT =       -5378
651243

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20312070
74                 X    =        -6191119
16
 Y    =       -3442406
27  feet           Y    =        -1049245
43  meter
 Z    =       -7792328
78                 Z    =        -2375101
81
 XDOT =       9217
243829                 XDOT =        2809
415919
 YDOT =     -13908
958343  feet/sec       YDOT =       -4239
450503  meter/sec
 ZDOT =     -17654
791569                 ZDOT =       -5381
180470


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 00130U          10040
12976965  
00020000  00000-0  20000-3 0  9047
2 00130  51
6441 168
2086 0040253 319
7071  40
1116 15
82970344   130


Satellite: SHUTTLE
Catalog Number: 00130
Epoch time:      10040
12976965   =   yrday
fracday
Element set:     904
Inclination:       51
6441  deg
RA of node:       168
2086  deg
Eccentricity:     
0040253     
Arg of perigee:   319
7071  deg
Mean anomaly:      40
1116  deg
Mean motion:   15
82970344  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              13
Checksum:              229


Coasting Arc #6 (Orbit 18)
---------------------------------------

Vector Time (GMT): 2010/040/11:28:54
433
Vector Time (MET): 001/02:14:46
433
Weight (LBS)     : 247622
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6585134
04                 A    =         6708003
82  meter
 Y    =       -1110411
36  meter          E    =           
0027612
 Z    =        -747009
60                 I    =           51
74471
 XDOT =        121
265924                 Wp   =          317
61563
 YDOT =       4841
460502  meter/sec      RA   =          165
36855  deg
 ZDOT =      -5979
923122                 TA   =          230
52286
                                          MA   =          230
76741
                                          Ha   =            186
780  n
mi
                                          Hp   =            162
911

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21604770
46                 X    =         6600690
18
 Y    =       -3643081
88  feet           Y    =        -1036685
48  meter
 Z    =       -2450818
91                 Z    =         -714982
09
 XDOT =        397
854081                 XDOT =          96
167491
 YDOT =      15884
056766  feet/sec       YDOT =        4842
676484  meter/sec
 ZDOT =     -19619
170348                 ZDOT =       -5979
394790

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16909847
67                 X    =         5154121
57
 Y    =       13953556
85  feet           Y    =         4253044
13  meter
 Z    =       -2323783
26                 Z    =         -708289
14
 XDOT =     -10651
077777                 XDOT =       -3246
448507
 YDOT =       9555
583675  feet/sec       YDOT =        2912
541904  meter/sec
 ZDOT =     -19616
882549                 ZDOT =       -5979
225801


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 00130U          10040
50855563  
00020000  00000-0  20000-3 0  9050
2 00130  51
6420 166
2322 0038271 318
2028  41
6218 15
82450265   191


Satellite: SHUTTLE
Catalog Number: 00130
Epoch time:      10040
50855563   =   yrday
fracday
Element set:     905
Inclination:       51
6420  deg
RA of node:       166
2322  deg
Eccentricity:     
0038271     
Arg of perigee:   318
2028  deg
Mean anomaly:      41
6218  deg
Mean motion:   15
82450265  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              19
Checksum:              223


Coasting Arc #7 (Orbit 27)
---------------------------------------

Vector Time (GMT): 2010/041/00:57:14
615
Vector Time (MET): 001/15:43:06
615
Weight (LBS)     : 247045
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4804597
90                 A    =         6717267
01  meter
 Y    =       -3807074
26  meter          E    =           
0011980
 Z    =        2764075
57                 I    =           51
75179
 XDOT =       5068
128451                 Wp   =          355
36668
 YDOT =       2651
368165  meter/sec      RA   =          162
42780  deg
 ZDOT =      -5147
565933                 TA   =          153
07236
                                          MA   =          153
01014
                                          Ha   =            187
223  n
mi
                                          Hp   =            176
047

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15763116
48                 X    =         4833385
18
 Y    =      -12490401
10  feet           Y    =        -3753185
53  meter
 Z    =        9068489
41                 Z    =         2787485
46
 XDOT =      16627
718015                 XDOT =        5063
108971
 YDOT =       8698
714451  feet/sec       YDOT =        2708
015098  meter/sec
 ZDOT =     -16888
339676                 ZDOT =       -5122
957735

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19628967
98                 X    =        -5982909
44
 Y    =        4183170
02  feet           Y    =         1275030
22  meter
 Z    =        9161231
67                 Z    =         2792343
41
 XDOT =     -10794
572273                 XDOT =       -3290
185629
 YDOT =     -13808
036985  feet/sec       YDOT =       -4208
689673  meter/sec
 ZDOT =     -16790
586552                 ZDOT =       -5117
770781


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 00130U          10041
07703840  
00020000  00000-0  20000-3 0  9064
2 00130  51
6433 163
2822 0020288 314
8324  45
1192 15
78053803   289


Satellite: SHUTTLE
Catalog Number: 00130
Epoch time:      10041
07703840   =   yrday
fracday
Element set:     906
Inclination:       51
6433  deg
RA of node:       163
2822  deg
Eccentricity:     
0020288     
Arg of perigee:   314
8324  deg
Mean anomaly:      45
1192  deg
Mean motion:   15
78053803  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              28
Checksum:              225


Coasting Arc #8 (Orbit 28)
---------------------------------------

Vector Time (GMT): 2010/041/02:28:41
966
Vector Time (MET): 001/17:14:33
966
Weight (LBS)     : 246826
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4863138
05                 A    =         6722275
78  meter
 Y    =       -3791801
82  meter          E    =           
0006272
 Z    =        2681603
01                 I    =           51
75483
 XDOT =       4984
132465                 Wp   =           27
65210
 YDOT =       2702
875220  meter/sec      RA   =          162
10098  deg
 ZDOT =      -5206
649317                 TA   =          121
83298
                                          MA   =          121
77190
                                          Ha   =            187
404  n
mi
                                          Hp   =            181
253

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15955177
32                 X    =         4892150
82
 Y    =      -12440294
69  feet           Y    =        -3737257
21  meter
 Z    =        8797910
14                 Z    =         2705297
82
 XDOT =      16352
140632                 XDOT =        4978
830270
 YDOT =       8867
700854  feet/sec       YDOT =        2758
581278  meter/sec
 ZDOT =     -17082
182800                 ZDOT =       -5182
449853

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16639013
71                 X    =        -5071571
38
 Y    =       11437273
81  feet           Y    =         3486081
06  meter
 Z    =        8891784
34                 Z    =         2710215
87
 XDOT =     -15040
985716                 XDOT =       -4584
492446
 YDOT =      -8650
129829  feet/sec       YDOT =       -2636
559572  meter/sec
 ZDOT =     -16986
048736                 ZDOT =       -5177
347655


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 00130U          10041
14041289  
00020000  00000-0  20000-3 0  9075
2 00130  51
6438 162
9557 0013359 308
1555  51
8405 15
76358644   299


Satellite: SHUTTLE
Catalog Number: 00130
Epoch time:      10041
14041289   =   yrday
fracday
Element set:     907
Inclination:       51
6438  deg
RA of node:       162
9557  deg
Eccentricity:     
0013359     
Arg of perigee:   308
1555  deg
Mean anomaly:      51
8405  deg
Mean motion:   15
76358644  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              29
Checksum:              256


Coasting Arc #9 (Orbit 29)
---------------------------------------

Vector Time (GMT): 2010/041/03:45:35
728
Vector Time (MET): 001/18:31:27
728
Weight (LBS)     : 246736
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -984430
75                 A    =         6714601
14  meter
 Y    =       -4051851
63  meter          E    =           
0010198
 Z    =        5268699
28                 I    =           51
72735
 XDOT =       7379
163143                 Wp   =          322
08936
 YDOT =      -2179
125294  meter/sec      RA   =          161
84669  deg
 ZDOT =       -289
482003                 TA   =          130
69989
                                          MA   =          130
61125
                                          Ha   =            187
766  n
mi
                                          Hp   =            182
362

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3229759
68                 X    =         -964642
74
 Y    =      -13293476
48  feet           Y    =        -4062749
66  meter
 Z    =       17285758
80                 Z    =         5263964
97
 XDOT =      24209
852830                 XDOT =        7404
388287
 YDOT =      -7149
361202  feet/sec       YDOT =       -2096
466068  meter/sec
 ZDOT =       -949
744103                 ZDOT =        -253
573824

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6813733
08                 X    =         2076825
84
 Y    =       11890146
17  feet           Y    =         3624116
55  meter
 Z    =       17266811
72                 Z    =         5262924
21
 XDOT =     -20498
999624                 XDOT =       -6248
095085
 YDOT =      12955
746777  feet/sec       YDOT =        3948
911618  meter/sec
 ZDOT =       -807
340717                 ZDOT =        -246
077451


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 00130U          10041
20382096  
00020000  00000-0  20000-3 0  9087
2 00130  51
6449 162
6291 0011508 310
8162  49
2003 15
75938855   305


Satellite: SHUTTLE
Catalog Number: 00130
Epoch time:      10041
20382096   =   yrday
fracday
Element set:     908
Inclination:       51
6449  deg
RA of node:       162
6291  deg
Eccentricity:     
0011508     
Arg of perigee:   310
8162  deg
Mean anomaly:      49
2003  deg
Mean motion:   15
75938855  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              30
Checksum:              234

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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