Date: May 20th 2009

SHUTTLE TRAJECTORY DATA

Lift off time (UTC) : 2009/131/18:01:55 956 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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


139/12:54:58 057 1 0 -0 6 1 0
007/18:53:02 101 -0 0 0 2 305 3
000/00:00:04 202 0 2 -0 8 301 6

139/13:30:33 555 0 7 -6 0 6 0
007/19:28:37 599 5 8 -0 0 305 2
000/00:00:25 198 1 4 0 1 297 8

139/15:02:57 013 85 6 -233 7 234 4
007/21:01:01 057 204 0 -0 1 305 3
000/00:02:26 114 77 6 18 7 160 2

Coasting Arc #1 (Orbit 104)
---------------------------------------

Vector Time (GMT): 2009/138/12:44:40
000
Vector Time (MET): 006/18:42:44
044
Weight (LBS)     : 241466
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6247820
29                 A    =         6945905
89  meter
 Y    =       -1287304
64  meter          E    =           
0012240
 Z    =        2726752
21                 I    =           28
16271
 XDOT =        637
687057                 Wp   =           57
12927
 YDOT =       7293
354506  meter/sec      RA   =          295
37582  deg
 ZDOT =       1981
763971                 TA   =          359
25558
                                          MA   =          359
25741
                                          Ha   =            305
134  n
mi
                                          Hp   =            302
013

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20498098
07                 X    =         6248504
60
 Y    =       -4223440
44  feet           Y    =        -1217434
21  meter
 Z    =        8946037
45                 Z    =         2757105
99
 XDOT =       2092
149138                 XDOT =         546
457004
 YDOT =      23928
328431  feet/sec       YDOT =        7299
975279  meter/sec
 ZDOT =       6501
850297                 ZDOT =        1984
640733

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4194399
59                 X    =         1278453
00
 Y    =      -20451866
58  feet           Y    =        -6233728
93  meter
 Z    =        9064724
21                 Z    =         2762927
94
 XDOT =      21303
407443                 XDOT =        6493
278589
 YDOT =       7256
417057  feet/sec       YDOT =        2211
755919  meter/sec
 ZDOT =       6513
521336                 ZDOT =        1985
321303


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 34933U 09025A   09138
58705438  
00020000  00000-0  70000-3 0  9003
2 34933  28
4692 295
4749 0003609 326
7484  33
3034 15
00794985  1057


Satellite: SHUTTLE
Catalog Number: 34933
Epoch time:      09138
58705438   =   yrday
fracday
Element set:     900
Inclination:       28
4692  deg
RA of node:       295
4749  deg
Eccentricity:     
0003609     
Arg of perigee:   326
7484  deg
Mean anomaly:      33
3034  deg
Mean motion:   15
00794985  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             105
Checksum:              311


Coasting Arc #2 (Orbit 119)
---------------------------------------

Vector Time (GMT): 2009/139/12:49:14
028
Vector Time (MET): 007/18:47:18
072
Weight (LBS)     : 241466
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5897595
85                 A    =         6944600
15  meter
 Y    =        1633707
35  meter          E    =           
0010733
 Z    =        3267637
06                 I    =           28
13854
 XDOT =      -2114
003372                 Wp   =           70
94784
 YDOT =       7281
089621  meter/sec      RA   =          288
73413  deg
 ZDOT =        179
974826                 TA   =           16
18495
                                          MA   =           16
15069
                                          Ha   =            305
358  n
mi
                                          Hp   =            301
745

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19349067
74                 X    =         5863015
33
 Y    =        5359932
26  feet           Y    =         1699464
17  meter
 Z    =       10720594
04                 Z    =         3296204
06
 XDOT =      -6935
706601                 XDOT =       -2196
138923
 YDOT =      23888
089309  feet/sec       YDOT =        7256
990347  meter/sec
 ZDOT =        590
468588                 ZDOT =         169
505776

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11952310
43                 X    =         3643064
22
 Y    =      -16057601
55  feet           Y    =        -4894356
95  meter
 Z    =       10832457
74                 Z    =         3301733
12
 XDOT =      18609
566813                 XDOT =        5672
195964
 YDOT =      14212
278382  feet/sec       YDOT =        4331
902451  meter/sec
 ZDOT =        549
925199                 ZDOT =         167
617201


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 34933U 09025A   09139
58457032  
00020000  00000-0  70000-3 0  9019
2 34933  28
4692 288
9643 0003552 337
2720  22
7867 15
00798577  1208


Satellite: SHUTTLE
Catalog Number: 34933
Epoch time:      09139
58457032   =   yrday
fracday
Element set:     901
Inclination:       28
4692  deg
RA of node:       288
9643  deg
Eccentricity:     
0003552     
Arg of perigee:   337
2720  deg
Mean anomaly:      22
7867  deg
Mean motion:   15
00798577  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             120
Checksum:              308


Coasting Arc #3 (Orbit 119)
---------------------------------------

Vector Time (GMT): 2009/139/12:55:00
158
Vector Time (MET): 007/18:53:04
202
Weight (LBS)     : 241433
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4766552
53                 A    =         6944794
25  meter
 Y    =        3978876
39  meter          E    =           
0010479
 Z    =        3096987
45                 I    =           28
14201
 XDOT =      -4342
932652                 Wp   =           78
66765
 YDOT =       6107
924394  meter/sec      RA   =          288
68248  deg
 ZDOT =      -1154
077232                 TA   =           30
18770
                                          MA   =           30
12736
                                          Ha   =            305
348  n
mi
                                          Hp   =            301
577

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15638295
71                 X    =         4706661
00
 Y    =       13054056
39  feet           Y    =         4031843
71  meter
 Z    =       10160719
98                 Z    =         3119998
43
 XDOT =     -14248
466706                 XDOT =       -4405
303341
 YDOT =      20039
122029  feet/sec       YDOT =        6059
010520  meter/sec
 ZDOT =      -3786
342626                 ZDOT =       -1175
326624

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17538954
58                 X    =         5345873
36
 Y    =      -10271679
32  feet           Y    =        -3130807
86  meter
 Z    =       10250979
85                 Z    =         3124498
66
 XDOT =      13327
151858                 XDOT =        4062
115886
 YDOT =      18865
833448  feet/sec       YDOT =        5750
306035  meter/sec
 ZDOT =      -3869
131961                 ZDOT =       -1179
311422


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 34933U 09025A   09139
58456783  
00020000  00000-0  70000-3 0  9022
2 34933  28
4694 288
9638 0004050 336
3939  23
6619 15
00882554  1204


Satellite: SHUTTLE
Catalog Number: 34933
Epoch time:      09139
58456783   =   yrday
fracday
Element set:     902
Inclination:       28
4694  deg
RA of node:       288
9638  deg
Eccentricity:     
0004050     
Arg of perigee:   336
3939  deg
Mean anomaly:      23
6619  deg
Mean motion:   15
00882554  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             120
Checksum:              317


Coasting Arc #4 (Orbit 119)
---------------------------------------

Vector Time (GMT): 2009/139/13:30:46
154
Vector Time (MET): 007/19:28:50
198
Weight (LBS)     : 241237
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6177143
54                 A    =         6941720
35  meter
 Y    =        1226146
57  meter          E    =           
0003438
 Z    =       -2923658
16                 I    =           28
14562
 XDOT =       -698
658845                 Wp   =           12
17864
 YDOT =      -7369
954094  meter/sec      RA   =          288
57006  deg
 ZDOT =      -1609
922917                 TA   =          231
03096
                                          MA   =          231
06159
                                          Ha   =            305
240  n
mi
                                          Hp   =            297
776

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20266218
98                 X    =        -6176192
63
 Y    =        4022790
58  feet           Y    =         1157075
63  meter
 Z    =       -9592054
32                 Z    =        -2953664
74
 XDOT =      -2292
187812                 XDOT =        -608
374030
 YDOT =     -24179
639416  feet/sec       YDOT =       -7377
262002  meter/sec
 ZDOT =      -5281
899335                 ZDOT =       -1613
098174

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         193875
36                 X    =           59093
21
 Y    =       20605829
44  feet           Y    =         6280656
81  meter
 Z    =       -9709386
55                 Z    =        -2959421
02
 XDOT =     -22675
878652                 XDOT =       -6911
607813
 YDOT =      -2288
857820  feet/sec       YDOT =        -697
643864  meter/sec
 ZDOT =      -5294
745201                 ZDOT =       -1613
838337


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 34933U 09025A   09139
58456065  
00020000  00000-0  70000-3 0  9036
2 34933  28
4702 288
9655 0006527  24
3535 335
7517 15
02011196  1202


Satellite: SHUTTLE
Catalog Number: 34933
Epoch time:      09139
58456065   =   yrday
fracday
Element set:     903
Inclination:       28
4702  deg
RA of node:       288
9655  deg
Eccentricity:     
0006527     
Arg of perigee:    24
3535  deg
Mean anomaly:     335
7517  deg
Mean motion:   15
02011196  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             120
Checksum:              289


Coasting Arc #5 (Orbit 120)
---------------------------------------

Vector Time (GMT): 2009/139/15:04:10
070
Vector Time (MET): 007/21:02:14
114
Weight (LBS)     : 235723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5993723
79                 A    =         6814843
61  meter
 Y    =        2269482
39  meter          E    =           
0189083
 Z    =       -2669319
42                 I    =           28
14942
 XDOT =      -1723
798326                 Wp   =           47
43700
 YDOT =      -7013
023482  meter/sec      RA   =          288
14594  deg
 ZDOT =      -2045
099239                 TA   =          187
14745
                                          MA   =          187
42088
                                          Ha   =            305
345  n
mi
                                          Hp   =            160
201

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19664448
12                 X    =        -6005688
81
 Y    =        7445808
37  feet           Y    =         2202390
33  meter
 Z    =       -8757609
66                 Z    =        -2698466
26
 XDOT =      -5655
506320                 XDOT =       -1635
314539
 YDOT =     -23008
607224  feet/sec       YDOT =       -7031
805143  meter/sec
 ZDOT =      -6709
643174                 ZDOT =       -2053
259048

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11574108
90                 X    =         3527788
39
 Y    =       17497499
12  feet           Y    =         5333237
73  meter
 Z    =       -8871518
30                 Z    =        -2704038
78
 XDOT =     -19935
878823                 XDOT =       -6076
455865
 YDOT =       9691
881010  feet/sec       YDOT =        2954
085332  meter/sec
 ZDOT =      -6741
971009                 ZDOT =       -2054
952764


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 34933U 09025A   09139
65061899  
00020000  00000-0  70000-3 0  9042
2 34933  28
4706 288
5216 0193672  47
5173 314
1784 15
44394776  1210


Satellite: SHUTTLE
Catalog Number: 34933
Epoch time:      09139
65061899   =   yrday
fracday
Element set:     904
Inclination:       28
4706  deg
RA of node:       288
5216  deg
Eccentricity:     
0193672     
Arg of perigee:    47
5173  deg
Mean anomaly:     314
1784  deg
Mean motion:   15
44394776  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             121
Checksum:              323


Coasting Arc #6 (Orbit 136)
---------------------------------------

Vector Time (GMT): 2009/140/15:08:23
848
Vector Time (MET): 008/21:06:27
892
Weight (LBS)     : 235723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5711077
99                 A    =         6814599
40  meter
 Y    =       -2040285
05  meter          E    =           
0205632
 Z    =        2787706
19                 I    =           28
13481
 XDOT =       1815
534849                 Wp   =           59
67685
 YDOT =       7397
200186  meter/sec      RA   =          281
06592  deg
 ZDOT =       1711
987435                 TA   =            2
66307
                                          MA   =            2
55525
                                          Ha   =            305
273  n
mi
                                          Hp   =            159
996

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18737132
52                 X    =         5719925
92
 Y    =       -6693848
60  feet           Y    =        -1976371
16  meter
 Z    =        9146017
67                 Z    =         2815472
47
 XDOT =       5956
479164                 XDOT =        1724
366496
 YDOT =      24269
029480  feet/sec       YDOT =        7416
992696  meter/sec
 ZDOT =       5616
756677                 ZDOT =        1720
586496

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11227650
49                 X    =        -3422187
87
 Y    =      -16365535
70  feet           Y    =        -4988215
28  meter
 Z    =        9254538
85                 Z    =         2820783
44
 XDOT =      20769
490262                 XDOT =        6330
540632
 YDOT =     -11085
605937  feet/sec       YDOT =       -3378
892690  meter/sec
 ZDOT =       5650
825505                 ZDOT =        1722
371614


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 34933U 09025A   09140
68460985  
00020000  00000-0  70000-3 0  9057
2 34933  28
4704 281
3025 0193558  59
3033 302
6651 15
44284561  1378


Satellite: SHUTTLE
Catalog Number: 34933
Epoch time:      09140
68460985   =   yrday
fracday
Element set:     905
Inclination:       28
4704  deg
RA of node:       281
3025  deg
Eccentricity:     
0193558     
Arg of perigee:    59
3033  deg
Mean anomaly:     302
6651  deg
Mean motion:   15
44284561  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             137
Checksum:              296


Coasting Arc #7 (Orbit 151)
---------------------------------------

Vector Time (GMT): 2009/141/15:12:25
630
Vector Time (MET): 009/21:10:29
674
Weight (LBS)     : 235723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5873758
86                 A    =         6813972
63  meter
 Y    =        2094969
04  meter          E    =           
0190957
 Z    =       -3054479
12                 I    =           28
12687
 XDOT =      -1891
547230                 Wp   =           70
37148
 YDOT =      -7148
760138  meter/sec      RA   =          273
98242  deg
 ZDOT =      -1274
088225                 TA   =          178
54611
                                          MA   =          178
48978
                                          Ha   =            305
580  n
mi
                                          Hp   =            159
670

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19270862
42                 X    =        -5881910
17
 Y    =        6873258
01  feet           Y    =         2029239
92  meter
 Z    =      -10021256
94                 Z    =        -3083034
10
 XDOT =      -6205
863614                 XDOT =       -1805
278575
 YDOT =     -23453
937462  feet/sec       YDOT =       -7169
430065  meter/sec
 ZDOT =      -4180
079477                 ZDOT =       -1283
068608

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12114824
62                 X    =         3692598
54
 Y    =       16419180
88  feet           Y    =         5004566
33  meter
 Z    =      -10132863
78                 Z    =        -3088496
88
 XDOT =     -19482
878405                 XDOT =       -5938
381338
 YDOT =      11790
621042  feet/sec       YDOT =        3593
781294  meter/sec
 ZDOT =      -4215
624255                 ZDOT =       -1284
922273


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 34933U 09025A   09141
65395459  
00020000  00000-0  70000-3 0  9069
2 34933  28
4707 274
5330 0193611  70
3120 291
8427 15
44392530  1527


Satellite: SHUTTLE
Catalog Number: 34933
Epoch time:      09141
65395459   =   yrday
fracday
Element set:     906
Inclination:       28
4707  deg
RA of node:       274
5330  deg
Eccentricity:     
0193611     
Arg of perigee:    70
3120  deg
Mean anomaly:     291
8427  deg
Mean motion:   15
44392530  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             152
Checksum:              287


Coasting Arc #8 (Orbit 167)
---------------------------------------

Vector Time (GMT): 2009/142/15:16:48
564
Vector Time (MET): 010/21:14:52
608
Weight (LBS)     : 235723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5636050
72                 A    =         6813818
57  meter
 Y    =       -1846496
78  meter          E    =           
0205524
 Z    =        3061311
70                 I    =           28
12314
 XDOT =       1984
513944                 Wp   =           81
71101
 YDOT =       7503
158458  meter/sec      RA   =          266
89628  deg
 ZDOT =        841
978663                 TA   =          354
96066
                                          MA   =          355
16440
                                          Ha   =            305
424  n
mi
                                          Hp   =            159
616

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18490980
05                 X    =         5641408
01
 Y    =       -6058060
30  feet           Y    =        -1783441
55  meter
 Z    =       10043673
57                 Z    =         3088705
12
 XDOT =       6510
872520                 XDOT =        1896
374585
 YDOT =      24616
661606  feet/sec       YDOT =        7524
857545  meter/sec
 ZDOT =       2762
397187                 ZDOT =         851
406401

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11680680
19                 X    =        -3560271
32
 Y    =      -15492439
97  feet           Y    =        -4722095
70  meter
 Z    =       10150755
18                 Z    =         3093950
18
 XDOT =      20075
334029                 XDOT =        6118
961812
 YDOT =     -13237
566364  feet/sec       YDOT =       -4034
810228  meter/sec
 ZDOT =       2799
709279                 ZDOT =         853
351388


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 34933U 09025A   09142
68790796  
00020000  00000-0  70000-3 0  9077
2 34933  28
4700 267
3148 0193563  82
0799 280
1887 15
44304322  1685


Satellite: SHUTTLE
Catalog Number: 34933
Epoch time:      09142
68790796   =   yrday
fracday
Element set:     907
Inclination:       28
4700  deg
RA of node:       267
3148  deg
Eccentricity:     
0193563     
Arg of perigee:    82
0799  deg
Mean anomaly:     280
1887  deg
Mean motion:   15
44304322  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             168
Checksum:              323


Coasting Arc #9 (Orbit 182)
---------------------------------------

Vector Time (GMT): 2009/143/15:20:49
325
Vector Time (MET): 011/21:18:53
369
Weight (LBS)     : 235723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5859868
89                 A    =         6813444
25  meter
 Y    =        1808389
37  meter          E    =           
0191938
 Z    =       -3254067
99                 I    =           28
12717
 XDOT =      -2037
591997                 Wp   =           93
17384
 YDOT =      -7212
801393  meter/sec      RA   =          259
80901  deg
 ZDOT =       -389
846368                 TA   =          170
68182
                                          MA   =          170
32057
                                          Ha   =            305
627  n
mi
                                          Hp   =            159
485

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19225291
65                 X    =        -5863847
04
 Y    =        5933035
98  feet           Y    =         1742839
11  meter
 Z    =      -10676076
08                 Z    =        -3282545
32
 XDOT =      -6685
013113                 XDOT =       -1954
891947
 YDOT =     -23664
046565  feet/sec       YDOT =       -7235
124480  meter/sec
 ZDOT =      -1279
023516                 ZDOT =        -399
545372

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12354743
18                 X    =         3765725
72
 Y    =       15804539
45  feet           Y    =         4817223
62  meter
 Z    =      -10787409
76                 Z    =        -3288002
50
 XDOT =     -18594
736387                 XDOT =       -5667
675651
 YDOT =      13749
134418  feet/sec       YDOT =        4190
736171  meter/sec
 ZDOT =      -1317
377848                 ZDOT =        -401
536768


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 34933U 09025A   09143
65721491  
00020000  00000-0  70000-3 0  9082
2 34933  28
4708 260
5449 0193602  93
0807 269
2133 15
44401021  1831


Satellite: SHUTTLE
Catalog Number: 34933
Epoch time:      09143
65721491   =   yrday
fracday
Element set:     908
Inclination:       28
4708  deg
RA of node:       260
5449  deg
Eccentricity:     
0193602     
Arg of perigee:    93
0807  deg
Mean anomaly:     269
2133  deg
Mean motion:   15
44401021  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             183
Checksum:              284


Coasting Arc #10 (Orbit 198)
---------------------------------------

Vector Time (GMT): 2009/144/15:25:12
246
Vector Time (MET): 012/21:23:16
290
Weight (LBS)     : 235723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5658706
60                 A    =         6813502
33  meter
 Y    =       -1628656
45  meter          E    =           
0204949
 Z    =        3148036
63                 I    =           28
13502
 XDOT =       2164
613754                 Wp   =          103
68809
 YDOT =       7496
600510  meter/sec      RA   =          252
72443  deg
 ZDOT =        -85
175888                 TA   =          347
38691
                                          MA   =          347
89215
                                          Ha   =            305
371  n
mi
                                          Hp   =            159
627

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18565310
36                 X    =         5661205
04
 Y    =       -5343361
06  feet           Y    =        -1565364
06  meter
 Z    =       10328204
18                 Z    =         3175532
97
 XDOT =       7101
751162                 XDOT =        2081
038399
 YDOT =      24595
146029  feet/sec       YDOT =        7520
339204  meter/sec
 ZDOT =       -279
448452                 ZDOT =         -74
861704

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12122122
30                 X    =        -3694822
88
 Y    =      -14968097
75  feet           Y    =        -4562276
19  meter
 Z    =       10435720
31                 Z    =         3180807
55
 XDOT =      18801
949870                 XDOT =        5730
834320
 YDOT =     -15229
023797  feet/sec       YDOT =       -4641
806453  meter/sec
 ZDOT =       -238
671873                 ZDOT =         -72
747187


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 34933U 09025A   09144
69112191  
00020000  00000-0  70000-3 0  9099
2 34933  28
4695 253
3275 0193559 104
8246 257
4045 15
44329795  1997


Satellite: SHUTTLE
Catalog Number: 34933
Epoch time:      09144
69112191   =   yrday
fracday
Element set:     909
Inclination:       28
4695  deg
RA of node:       253
3275  deg
Eccentricity:     
0193559     
Arg of perigee:   104
8246  deg
Mean anomaly:     257
4045  deg
Mean motion:   15
44329795  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             199
Checksum:              327

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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