Date: April 17th 2010

SHUTTLE TRAJECTORY DATA

Lift off time (UTC) : 2010/095/10:21:24 956 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 82 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 05 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


107/11:51:25 413 -0 2 -0 2 0 2
012/01:30:00 457 0 0 -0 1 188 9
000/00:00:00 914 0 1 0 0 182 4

107/14:07:30 709 -1 2 0 0 3 0
012/03:46:05 753 1 7 -0 0 189 3
000/00:00:11 505 -2 1 -3 0 182 4

107/14:35:30 707 -2 1 -3 0 3 0
012/04:14:05 750 1 3 0 0 188 7
000/00:00:11 501 -1 7 -0 0 181 9

108/17:31:24 950 17 8 -19 0 19 0
013/07:09:59 994 3 0 0 0 187 9
000/00:00:13 120 -5 9 -0 0 171 1

Coasting Arc #1 (Orbit 165)
---------------------------------------

Vector Time (GMT): 2010/105/20:57:27
000
Vector Time (MET): 010/10:36:02
044
Weight (LBS)     : 216425
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2112263
78                 A    =         6718366
18  meter
 Y    =        3787712
15  meter          E    =           
0015570
 Z    =       -5144446
31                 I    =           51
56935
 XDOT =      -7236
276129                 Wp   =          115
09334
 YDOT =      -2251
807085  meter/sec      RA   =          189
40318  deg
 ZDOT =       1309
808149                 TA   =          167
48266
                                          MA   =          167
44394
                                          Ha   =            189
437  n
mi
                                          Hp   =            182
291

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6929999
28                 X    =        -2129470
43
 Y    =       12426877
14  feet           Y    =         3763995
23  meter
 Z    =      -16878104
69                 Z    =        -5154749
75
 XDOT =     -23741
063416                 XDOT =       -7216
921123
 YDOT =      -7387
818520  feet/sec       YDOT =       -2332
619180  meter/sec
 ZDOT =       4297
270830                 ZDOT =        1274
700754

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11066645
01                 X    =         3373113
40
 Y    =       -8865771
59  feet           Y    =        -2702287
18  meter
 Z    =      -16918925
67                 Z    =        -5156888
54
 XDOT =      18482
006051                 XDOT =        5633
315444
 YDOT =      15114
654816  feet/sec       YDOT =        4606
946788  meter/sec
 ZDOT =       4157
620393                 ZDOT =        1267
242696


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 36507U  10012   10105
88697748  
00020000  00000-0  20000-3 0  9008
2 36507  51
6453 190
3789 0004103 178
1992 181
9188 15
74796850  1660


Satellite: SHUTTLE
Catalog Number: 36507
Epoch time:      10105
88697748   =   yrday
fracday
Element set:     900
Inclination:       51
6453  deg
RA of node:       190
3789  deg
Eccentricity:     
0004103     
Arg of perigee:   178
1992  deg
Mean anomaly:     181
9188  deg
Mean motion:   15
74796850  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             166
Checksum:              326


Coasting Arc #2 (Orbit 181)
---------------------------------------

Vector Time (GMT): 2010/106/20:57:40
793
Vector Time (MET): 011/10:36:15
836
Weight (LBS)     : 216399
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6329141
24                 A    =         6728798
26  meter
 Y    =        1681105
87  meter          E    =           
0011787
 Z    =       -1520556
91                 I    =           51
63526
 XDOT =      -2552
319081                 Wp   =          155
69550
 YDOT =       4400
741309  meter/sec      RA   =          184
28369  deg
 ZDOT =      -5784
686897                 TA   =           41
07060
                                          MA   =           40
98192
                                          Ha   =            189
311  n
mi
                                          Hp   =            182
405

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20764899
08                 X    =         6317259
13
 Y    =        5515439
20  feet           Y    =         1751815
66  meter
 Z    =       -4988703
77                 Z    =        -1489838
27
 XDOT =      -8373
750265                 XDOT =       -2573
237809
 YDOT =      14438
127655  feet/sec       YDOT =        4372
082803  meter/sec
 ZDOT =     -18978
631551                 ZDOT =       -5797
137086

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17334298
70                 X    =        -5283494
24
 Y    =      -12740778
28  feet           Y    =        -3883389
22  meter
 Z    =       -4866510
67                 Z    =        -1483312
45
 XDOT =      12042
267302                 XDOT =        3670
483074
 YDOT =      -9149
812290  feet/sec       YDOT =       -2788
862786  meter/sec
 ZDOT =     -19027
973425                 ZDOT =       -5799
726300


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 36507U  10012   10106
90227472  
00020000  00000-0  20000-3 0  9016
2 36507  51
6456 185
1593 0004023 182
1583 177
9564 15
74851347  1824


Satellite: SHUTTLE
Catalog Number: 36507
Epoch time:      10106
90227472   =   yrday
fracday
Element set:     901
Inclination:       51
6456  deg
RA of node:       185
1593  deg
Eccentricity:     
0004023     
Arg of perigee:   182
1583  deg
Mean anomaly:     177
9564  deg
Mean motion:   15
74851347  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             182
Checksum:              288


Coasting Arc #3 (Orbit 191)
---------------------------------------

Vector Time (GMT): 2010/107/11:51:25
870
Vector Time (MET): 012/01:30:00
914
Weight (LBS)     : 216393
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3210275
39                 A    =         6719934
83  meter
 Y    =       -3625907
65  meter          E    =           
0006401
 Z    =        4653047
51                 I    =           51
62658
 XDOT =       6768
811570                 Wp   =           95
93009
 YDOT =       2362
892570  meter/sec      RA   =          181
05584  deg
 ZDOT =      -2826
047037                 TA   =           21
97305
                                          MA   =           21
94562
                                          Ha   =            188
942  n
mi
                                          Hp   =            182
401

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10532399
57                 X    =         3227978
31
 Y    =      -11896022
46  feet           Y    =        -3589909
52  meter
 Z    =       15265903
92                 Z    =         4668686
23
 XDOT =      22207
387042                 XDOT =        6755
614851
 YDOT =       7752
272210  feet/sec       YDOT =        2438
511702  meter/sec
 ZDOT =      -9271
807863                 ZDOT =       -2793
195642

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5072068
56                 X    =         1545966
50
 Y    =      -14994080
63  feet           Y    =        -4570195
78  meter
 Z    =       15327957
47                 Z    =         4671961
44
 XDOT =      22438
094161                 XDOT =        6839
131100
 YDOT =      -1763
377274  feet/sec       YDOT =        -537
477393  meter/sec
 ZDOT =      -9141
102582                 ZDOT =       -2786
208067


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 36507U  10012   10107
53681622  
00020000  00000-0  20000-3 0  9028
2 36507  51
6468 181
8963 0004298 189
0942 171
0144 15
74957439  1929


Satellite: SHUTTLE
Catalog Number: 36507
Epoch time:      10107
53681622   =   yrday
fracday
Element set:     902
Inclination:       51
6468  deg
RA of node:       181
8963  deg
Eccentricity:     
0004298     
Arg of perigee:   189
0942  deg
Mean anomaly:     171
0144  deg
Mean motion:   15
74957439  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             192
Checksum:              305


Coasting Arc #4 (Orbit 192)
---------------------------------------

Vector Time (GMT): 2010/107/14:07:36
461
Vector Time (MET): 012/03:46:11
505
Weight (LBS)     : 216317
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2821349
97                 A    =         6719500
91  meter
 Y    =        3774625
38  meter          E    =           
0013624
 Z    =       -4802315
98                 I    =           51
62683
 XDOT =      -6983
899819                 Wp   =          130
38848
 YDOT =      -2043
624270  meter/sec      RA   =          180
57213  deg
 ZDOT =       2492
694631                 TA   =          164
04919
                                          MA   =          164
00624
                                          Ha   =            189
253  n
mi
                                          Hp   =            182
395

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9256397
53                 X    =        -2840019
66
 Y    =       12383941
53  feet           Y    =         3742971
06  meter
 Z    =      -15755629
85                 Z    =        -4816067
60
 XDOT =     -22913
057149                 XDOT =       -6972
637833
 YDOT =      -6704
804036  feet/sec       YDOT =       -2121
659464  meter/sec
 ZDOT =       8178
131991                 ZDOT =        2458
793632

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5325791
21                 X    =         1623301
16
 Y    =       14455347
31  feet           Y    =         4405989
86  meter
 Z    =      -15810175
75                 Z    =        -4818941
57
 XDOT =     -17148
679744                 XDOT =       -5226
917586
 YDOT =      15129
663251  feet/sec       YDOT =        4611
521359  meter/sec
 ZDOT =       8043
263230                 ZDOT =        2451
586633


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 36507U  10012   10107
60027144  
00020000  00000-0  20000-3 0  9030
2 36507  51
6461 181
5707 0005223 190
0535 170
0525 15
74910940  1933


Satellite: SHUTTLE
Catalog Number: 36507
Epoch time:      10107
60027144   =   yrday
fracday
Element set:     903
Inclination:       51
6461  deg
RA of node:       181
5707  deg
Eccentricity:     
0005223     
Arg of perigee:   190
0535  deg
Mean anomaly:     170
0525  deg
Mean motion:   15
74910940  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             193
Checksum:              251


Coasting Arc #5 (Orbit 193)
---------------------------------------

Vector Time (GMT): 2010/107/14:35:36
457
Vector Time (MET): 012/04:14:11
501
Weight (LBS)     : 216242
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4758158
25                 A    =         6722107
35  meter
 Y    =       -2972696
05  meter          E    =           
0012392
 Z    =        3701587
84                 I    =           51
64048
 XDOT =       5445
869969                 Wp   =          130
59595
 YDOT =      -3348
992042  meter/sec      RA   =          180
51765  deg
 ZDOT =       4293
507425                 TA   =          274
01706
                                          MA   =          274
15870
                                          Ha   =            188
699  n
mi
                                          Hp   =            181
897

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15610755
40                 X    =        -4742545
31
 Y    =       -9752939
81  feet           Y    =        -3025817
38  meter
 Z    =       12144317
05                 Z    =         3678510
21
 XDOT =      17867
027457                 XDOT =        5462
056834
 YDOT =     -10987
506699  feet/sec       YDOT =       -3288
002652  meter/sec
 ZDOT =      14086
310451                 ZDOT =        4320
003139

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15683694
71                 X    =        -4780390
15
 Y    =        9749876
77  feet           Y    =         2971762
44  meter
 Z    =       12052451
15                 Z    =         3673587
11
 XDOT =      -1275
679322                 XDOT =        -388
827057
 YDOT =     -19665
781418  feet/sec       YDOT =       -5994
130176  meter/sec
 ZDOT =      14191
544486                 ZDOT =        4325
582759


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 36507U  10012   10107
66370086  
00020000  00000-0  20000-3 0  9043
2 36507  51
6452 181
2444 0007260 199
0546 161
0347 15
75477375  1946


Satellite: SHUTTLE
Catalog Number: 36507
Epoch time:      10107
66370086   =   yrday
fracday
Element set:     904
Inclination:       51
6452  deg
RA of node:       181
2444  deg
Eccentricity:     
0007260     
Arg of perigee:   199
0546  deg
Mean anomaly:     161
0347  deg
Mean motion:   15
75477375  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             194
Checksum:              287


Coasting Arc #6 (Orbit 208)
---------------------------------------

Vector Time (GMT): 2010/108/14:40:28
506
Vector Time (MET): 013/04:19:03
550
Weight (LBS)     : 216242
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6161025
79                 A    =         6726244
88  meter
 Y    =        1970555
61  meter          E    =           
0001994
 Z    =       -1848306
23                 I    =           51
68654
 XDOT =      -3050
624147                 Wp   =          126
86079
 YDOT =      -4234
649164  meter/sec      RA   =          175
31187  deg
 ZDOT =       5657
034815                 TA   =          212
64228
                                          MA   =          212
65461
                                          Ha   =            188
435  n
mi
                                          Hp   =            181
913

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20213339
21                 X    =        -6173624
15
 Y    =        6465077
45  feet           Y    =         1901588
97  meter
 Z    =       -6063996
83                 Z    =        -1878267
39
 XDOT =     -10008
609406                 XDOT =       -3030
525989
 YDOT =     -13893
205920  feet/sec       YDOT =       -4268
650869  meter/sec
 ZDOT =      18559
825508                 ZDOT =        5642
263386

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2318957
10                 X    =         -706818
12
 Y    =       21060398
28  feet           Y    =         6419209
40  meter
 Z    =       -6183075
93                 Z    =        -1884601
54
 XDOT =     -15274
211993                 XDOT =       -4655
579816
 YDOT =       3746
961539  feet/sec       YDOT =        1142
073877  meter/sec
 ZDOT =      18500
937772                 ZDOT =        5639
085833


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 36507U  10012   10108
61513782  
00020000  00000-0  20000-3 0  9052
2 36507  51
6460 176
3483 0007323 202
9328 157
1510 15
75539959  2097


Satellite: SHUTTLE
Catalog Number: 36507
Epoch time:      10108
61513782   =   yrday
fracday
Element set:     905
Inclination:       51
6460  deg
RA of node:       176
3483  deg
Eccentricity:     
0007323     
Arg of perigee:   202
9328  deg
Mean anomaly:     157
1510  deg
Mean motion:   15
75539959  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             209
Checksum:              287


Coasting Arc #7 (Orbit 210)
---------------------------------------

Vector Time (GMT): 2010/108/17:31:31
510
Vector Time (MET): 013/07:10:06
554
Weight (LBS)     : 215839
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2345713
51                 A    =         6707706
00  meter
 Y    =        4052670
67  meter          E    =           
0027439
 Z    =       -4827887
55                 I    =           51
65794
 XDOT =      -7185
299449                 Wp   =          125
89904
 YDOT =      -1260
774076  meter/sec      RA   =          174
69841  deg
 ZDOT =       2426
577508                 TA   =          167
86386
                                          MA   =          167
79763
                                          Ha   =            187
897  n
mi
                                          Hp   =            171
097

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7695910
47                 X    =        -2367403
59
 Y    =       13296163
62  feet           Y    =         4026318
40  meter
 Z    =      -15839526
08                 Z    =        -4839335
70
 XDOT =     -23573
817091                 XDOT =       -7182
455225
 YDOT =      -4136
397886  feet/sec       YDOT =       -1341
108547  meter/sec
 ZDOT =       7961
212298                 ZDOT =        2391
677792

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15037977
89                 X    =         4583575
66
 Y    =        2904192
43  feet           Y    =          885197
85  meter
 Z    =      -15884913
56                 Z    =        -4841721
65
 XDOT =       3920
800059                 XDOT =        1195
059858
 YDOT =      22594
530940  feet/sec       YDOT =        6886
813031  meter/sec
 ZDOT =       7822
380457                 ZDOT =        2384
261563


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 36507U  10012   10108
74199651  
00020000  00000-0  20000-3 0  9062
2 36507  51
6431 175
6946 0016389 138
8337 221
4068 15
79028921  2112


Satellite: SHUTTLE
Catalog Number: 36507
Epoch time:      10108
74199651   =   yrday
fracday
Element set:     906
Inclination:       51
6431  deg
RA of node:       175
6946  deg
Eccentricity:     
0016389     
Arg of perigee:   138
8337  deg
Mean anomaly:     221
4068  deg
Mean motion:   15
79028921  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             211
Checksum:              302

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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