Date: March 25th 2008

SHUTTLE TRAJECTORY DATA

Lift off time (UTC) : 2008/071/06:28:13 948 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 10 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : -0 34056

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


085/01:11:25 158 0 0 0 0 0 0
013/18:43:11 211 0 0 0 0 185 7
000/00:00:00 000 0 0 0 0 180 9

085/01:39:16 793 0 6 1 5 1 5
013/19:11:02 846 -1 1 -0 0 186 4
000/00:00:05 691 -0 8 -0 0 181 0

085/17:53:21 674 -2 5 4 0 4 0
014/11:25:07 727 -0 7 0 0 188 3
000/00:00:15 453 3 1 -0 0 181 7

Coasting Arc #1 (Orbit 209)
---------------------------------------

Vector Time (GMT): 2008/084/10:19:06
000
Vector Time (MET): 013/03:50:52
052
Weight (LBS)     : 218128
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3932041
77                 A    =         6713991
19  meter
 Y    =       -1833403
19  meter          E    =           
0004476
 Z    =        5122473
51                 I    =           51
94568
 XDOT =       1502
185733                 Wp   =           37
03691
 YDOT =      -7409
364034  meter/sec      RA   =           92
55774  deg
 ZDOT =      -1494
657509                 TA   =           67
24585
                                          MA   =           67
19855
                                          Ha   =            186
163  n
mi
                                          Hp   =            180
481

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12900399
51                 X    =        -3936178
94
 Y    =       -6015102
32  feet           Y    =        -1877298
17  meter
 Z    =       16806015
45                 Z    =         5103361
79
 XDOT =       4928
430883                 XDOT =        1592
003979
 YDOT =     -24308
937118  feet/sec       YDOT =       -7392
102186  meter/sec
 ZDOT =      -4903
731985                 ZDOT =       -1487
140554

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9480059
45                 X    =        -2889522
12
 Y    =      -10732910
99  feet           Y    =        -3271391
27  meter
 Z    =       16732513
65                 Z    =         5100070
16
 XDOT =      13529
713779                 XDOT =        4123
856760
 YDOT =     -19573
046834  feet/sec       YDOT =       -5965
864675  meter/sec
 ZDOT =      -4875
744247                 ZDOT =       -1486
126846


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 32699U 08009A   08084
47498794  
00020000  00000-0  70000-3 0  9002
2 32699  51
6387  93
0951 0001388 308
1540  51
9499 15
76409581  2105


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08084
47498794   =   yrday
fracday
Element set:     900
Inclination:       51
6387  deg
RA of node:        93
0951  deg
Eccentricity:     
0001388     
Arg of perigee:   308
1540  deg
Mean anomaly:      51
9499  deg
Mean motion:   15
76409581  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             210
Checksum:              327


Coasting Arc #2 (Orbit 219)
---------------------------------------

Vector Time (GMT): 2008/085/01:11:25
158
Vector Time (MET): 013/18:43:11
211
Weight (LBS)     : 218054
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1561738
46                 A    =         6723443
15  meter
 Y    =        6192923
57  meter          E    =           
0012545
 Z    =        2079335
66                 I    =           51
97561
 XDOT =      -4395
567685                 Wp   =           60
86418
 YDOT =      -2988
810062  meter/sec      RA   =           89
40485  deg
 ZDOT =       5581
132348                 TA   =          322
27622
                                          MA   =          322
36412
                                          Ha   =            185
675  n
mi
                                          Hp   =            180
884

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5123813
86                 X    =        -1640820
37
 Y    =       20317990
70  feet           Y    =         6175057
20  meter
 Z    =        6821967
40                 Z    =         2071555
74
 XDOT =     -14421
153823                 XDOT =       -4389
007403
 YDOT =      -9805
807291  feet/sec       YDOT =       -3037
817265  meter/sec
 ZDOT =      18310
801666                 ZDOT =        5559
794909

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2091253
73                 X    =         -637414
14
 Y    =      -20858993
83  feet           Y    =        -6357821
32  meter
 Z    =        6792826
21                 Z    =         2070453
43
 XDOT =      15480
244257                 XDOT =        4718
378450
 YDOT =       4404
725064  feet/sec       YDOT =        1342
560199  meter/sec
 ZDOT =      18228
635053                 ZDOT =        5556
087964


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 32699U 08009A   08085
10891649  
00020000  00000-0  70000-3 0  9010
2 32699  51
6363  89
8233 0002524 297
2780  62
8128 15
76428146  2201


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08085
10891649   =   yrday
fracday
Element set:     901
Inclination:       51
6363  deg
RA of node:        89
8233  deg
Eccentricity:     
0002524     
Arg of perigee:   297
2780  deg
Mean anomaly:      62
8128  deg
Mean motion:   15
76428146  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             220
Checksum:              311


Coasting Arc #3 (Orbit 219)
---------------------------------------

Vector Time (GMT): 2008/085/01:39:19
639
Vector Time (MET): 013/19:11:05
691
Weight (LBS)     : 218010
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3068819
44                 A    =         6719773
11  meter
 Y    =       -4570377
00  meter          E    =           
0010131
 Z    =        3846583
48                 I    =           51
96022
 XDOT =       3183
911810                 Wp   =           78
82090
 YDOT =      -5650
293774  meter/sec      RA   =           89
26058  deg
 ZDOT =      -4162
251559                 TA   =           54
52329
                                          MA   =           54
42879
                                          Ha   =            186
434  n
mi
                                          Hp   =            181
029

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10068305
24                 X    =        -3036285
16
 Y    =      -14994675
20  feet           Y    =        -4604436
04  meter
 Z    =       12620024
54                 Z    =         3831754
73
 XDOT =      10445
904890                 XDOT =        3266
937799
 YDOT =     -18537
709232  feet/sec       YDOT =       -5614
305917  meter/sec
 ZDOT =     -13655
680968                 ZDOT =       -4146
581565

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15838607
80                 X    =         4827607
66
 Y    =        8763253
17  feet           Y    =         2671039
57  meter
 Z    =       12562641
88                 Z    =         3829093
24
 XDOT =       -329
697119                 XDOT =        -100
491682
 YDOT =      20139
292741  feet/sec       YDOT =        6138
456427  meter/sec
 ZDOT =     -13596
219496                 ZDOT =       -4144
127702


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 32699U 08009A   08085
10892610  
00020000  00000-0  70000-3 0  9020
2 32699  51
6362  89
8231 0001367 281
9591  78
1420 15
76120703  2205


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08085
10892610   =   yrday
fracday
Element set:     902
Inclination:       51
6362  deg
RA of node:        89
8231  deg
Eccentricity:     
0001367     
Arg of perigee:   281
9591  deg
Mean anomaly:      78
1420  deg
Mean motion:   15
76120703  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             220
Checksum:              285


Coasting Arc #4 (Orbit 230)
---------------------------------------

Vector Time (GMT): 2008/085/17:53:29
401
Vector Time (MET): 014/11:25:15
453
Weight (LBS)     : 217909
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -545956
19                 A    =         6727512
73  meter
 Y    =        6567419
91  meter          E    =           
0015923
 Z    =        1306763
11                 I    =           51
98203
 XDOT =      -4725
911643                 Wp   =           45
90889
 YDOT =      -1570
045017  meter/sec      RA   =           85
83398  deg
 ZDOT =       5883
114661                 TA   =          328
38476
                                          MA   =          328
48032
                                          Ha   =            188
329  n
mi
                                          Hp   =            181
742

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1791194
86                 X    =         -625538
65
 Y    =       21546653
26  feet           Y    =         6560884
46  meter
 Z    =        4287280
54                 Z    =         1303916
70
 XDOT =     -15504
959458                 XDOT =       -4736
623512
 YDOT =      -5151
066329  feet/sec       YDOT =       -1622
834511  meter/sec
 ZDOT =      19301
557287                 ZDOT =        5860
130219

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21579578
96                 X    =         6577455
67
 Y    =        1369547
59  feet           Y    =          417438
11  meter
 Z    =        4277093
79                 Z    =         1303658
19
 XDOT =      -4727
251599                 XDOT =       -1440
866287
 YDOT =      14143
832569  feet/sec       YDOT =        4311
040167  meter/sec
 ZDOT =      19213
233528                 ZDOT =        5856
193579


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 32699U 08009A   08085
80639326  
00020000  00000-0  70000-3 0  9031
2 32699  51
6398  86
2351 0003997 351
7916   8
3181 15
75393679  2310


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08085
80639326   =   yrday
fracday
Element set:     903
Inclination:       51
6398  deg
RA of node:        86
2351  deg
Eccentricity:     
0003997     
Arg of perigee:   351
7916  deg
Mean anomaly:       8
3181  deg
Mean motion:   15
75393679  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             231
Checksum:              331


Coasting Arc #5 (Orbit 245)
---------------------------------------

Vector Time (GMT): 2008/086/17:53:47
215
Vector Time (MET): 015/11:25:33
268
Weight (LBS)     : 217909
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4211243
02                 A    =         6717603
00  meter
 Y    =        1720105
35  meter          E    =           
0011835
 Z    =       -4952868
55                 I    =           51
94635
 XDOT =       -492
741869                 Wp   =           87
30250
 YDOT =       7372
776113  meter/sec      RA   =           80
67990  deg
 ZDOT =       2146
485843                 TA   =          203
41869
                                          MA   =          203
47264
                                          Ha   =            188
367  n
mi
                                          Hp   =            181
722

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13816414
12                 X    =         4215799
71
 Y    =        5643390
25  feet           Y    =         1767118
18  meter
 Z    =      -16249568
74                 Z    =        -4932399
34
 XDOT =      -1616
607183                 XDOT =        -585
393122
 YDOT =      24188
898007  feet/sec       YDOT =        7366
761570  meter/sec
 ZDOT =       7042
276389                 ZDOT =        2143
866249

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5094275
07                 X    =         1552735
04
 Y    =      -14118810
84  feet           Y    =        -4303413
55  meter
 Z    =      -16170874
40                 Z    =        -4928882
52
 XDOT =      23205
648637                 XDOT =        7073
081705
 YDOT =        336
280877  feet/sec       YDOT =         102
498411  meter/sec
 ZDOT =       7033
036422                 ZDOT =        2143
669502


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 32699U 08009A   08086
75788819  
00020000  00000-0  70000-3 0  9049
2 32699  51
6407  81
3385 0003995 354
8430   5
2692 15
75411235  2465


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08086
75788819   =   yrday
fracday
Element set:     904
Inclination:       51
6407  deg
RA of node:        81
3385  deg
Eccentricity:     
0003995     
Arg of perigee:   354
8430  deg
Mean anomaly:       5
2692  deg
Mean motion:   15
75411235  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             246
Checksum:              324


Coasting Arc #6 (Orbit 261)
---------------------------------------

Vector Time (GMT): 2008/087/17:59:00
228
Vector Time (MET): 016/11:30:46
281
Weight (LBS)     : 217909
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1772820
76                 A    =         6721637
46  meter
 Y    =       -5220168
16  meter          E    =           
0008328
 Z    =       -3855209
55                 I    =           51
95501
 XDOT =       4544
274141                 Wp   =           46
21558
 YDOT =       4612
801459  meter/sec      RA   =           75
58050  deg
 ZDOT =      -4156
208914                 TA   =          180
47743
                                          MA   =          180
47823
                                          Ha   =            188
341  n
mi
                                          Hp   =            181
534

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5816341
07                 X    =         1849660
57
 Y    =      -17126535
96  feet           Y    =        -5199959
18  meter
 Z    =      -12648325
29                 Z    =        -3846410
02
 XDOT =      14909
035897                 XDOT =        4512
661339
 YDOT =      15133
863053  feet/sec       YDOT =        4663
328514  meter/sec
 ZDOT =     -13635
856017                 ZDOT =       -4134
209975

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17538713
18                 X    =        -5345799
78
 Y    =       -4514422
68  feet           Y    =        -1375996
03  meter
 Z    =      -12615138
45                 Z    =        -3845094
20
 XDOT =      13571
437601                 XDOT =        4136
574181
 YDOT =     -14857
754575  feet/sec       YDOT =       -4528
643595  meter/sec
 ZDOT =     -13550
980712                 ZDOT =       -4130
338921


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 32699U 08009A   08087
77280240  
00020000  00000-0  70000-3 0  9058
2 32699  51
6414  76
1155 0004023 357
9222   2
1925 15
75449088  2626


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08087
77280240   =   yrday
fracday
Element set:     905
Inclination:       51
6414  deg
RA of node:        76
1155  deg
Eccentricity:     
0004023     
Arg of perigee:   357
9222  deg
Mean anomaly:       2
1925  deg
Mean motion:   15
75449088  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             262
Checksum:              294


Coasting Arc #7 (Orbit 277)
---------------------------------------

Vector Time (GMT): 2008/088/17:59:18
908
Vector Time (MET): 017/11:31:04
961
Weight (LBS)     : 217909
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4134222
34                 A    =         6723762
31  meter
 Y    =       -4258416
65  meter          E    =           
0013568
 Z    =        3151796
27                 I    =           51
95340
 XDOT =       2048
435464                 Wp   =           77
05289
 YDOT =      -5607
493730  meter/sec      RA   =           70
40427  deg
 ZDOT =      -4868
977894                 TA   =           66
39444
                                          MA   =           66
25203
                                          Ha   =            188
465  n
mi
                                          Hp   =            181
356

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13563721
59                 X    =        -4101714
57
 Y    =      -13971183
23  feet           Y    =        -4304363
58  meter
 Z    =       10340538
94                 Z    =         3131791
54
 XDOT =       6720
588793                 XDOT =        2134
501040
 YDOT =     -18397
289141  feet/sec       YDOT =       -5584
158105  meter/sec
 ZDOT =     -15974
336921                 ZDOT =       -4858
817045

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12574705
27                 X    =        -3832770
17
 Y    =       14920980
04  feet           Y    =         4547914
72  meter
 Z    =       10263351
88                 Z    =         3128269
65
 XDOT =     -17886
230718                 XDOT =       -5451
723123
 YDOT =      -4065
768200  feet/sec       YDOT =       -1239
246147  meter/sec
 ZDOT =     -15935
961883                 ZDOT =       -4857
281182


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 32699U 08009A   08088
78769785  
00020000  00000-0  70000-3 0  9067
2 32699  51
6411  70
8923 0004015   3
3834 356
7357 15
75467742  2780


Satellite: SHUTTLE
Catalog Number: 32699
Epoch time:      08088
78769785   =   yrday
fracday
Element set:     906
Inclination:       51
6411  deg
RA of node:        70
8923  deg
Eccentricity:     
0004015     
Arg of perigee:     3
3834  deg
Mean anomaly:     356
7357  deg
Mean motion:   15
75467742  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             278
Checksum:              337

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 may contain past, current and future orbital data 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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