[list_settings.list_name] Current STS TLEs @ 00:30 UTC

 
Date: June 1st 2011

SHUTTLE TRAJECTORY DATA

Lift off time (UTC) : 2011/136/12:56:27 958 Area (sq ft) : 5166 0 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 107 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 52 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : -0 26320

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


151/07:35:04 867 -1 4 0 3 3 9
014/18:38:36 909 -1 6 -2 5 186 8
000/00:06:09 818 3 3 -3 0 180 7

Coasting Arc #1 (Orbit 221)
---------------------------------------

Vector Time (GMT): 2011/150/12:46:05
000
Vector Time (MET): 013/23:49:37
042
Weight (LBS)     : 213190
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3977564
19                 A    =         6713850
50  meter
 Y    =        1359198
58  meter          E    =           
0014419
 Z    =       -5247199
01                 I    =           51
30535
 XDOT =      -2546
652092                 Wp   =           75
68104
 YDOT =      -7260
601955  meter/sec      RA   =          250
35347  deg
 ZDOT =         53
354445                 TA   =          194
80686
                                          MA   =          194
84913
                                          Ha   =            186
817  n
mi
                                          Hp   =            180
546

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13049751
28                 X    =        -3966951
86
 Y    =        4459312
92  feet           Y    =         1314854
89  meter
 Z    =      -17215219
86                 Z    =        -5266496
44
 XDOT =      -8355
157783                 XDOT =       -2465
672452
 YDOT =     -23820
872557  feet/sec       YDOT =       -7288
579284  meter/sec
 ZDOT =        175
047391                 ZDOT =          41
178969

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1768652
96                 X    =          539085
42
 Y    =       13577775
29  feet           Y    =         4138505
91  meter
 Z    =      -17293384
86                 Z    =        -5271023
70
 XDOT =     -24023
333779                 XDOT =       -7322
312136
 YDOT =       3274
725936  feet/sec       YDOT =         998
136465  meter/sec
 ZDOT =        126
061236                 ZDOT =          38
423465


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 37577U  11020   11150
54780281  
00020000  00000-0  20000-3 0  9005
2 37577  51
6504 251
1487 0003841 343
1219  16
9817 15
76194875  2220


Satellite: SHUTTLE
Catalog Number: 37577
Epoch time:      11150
54780281   =   yrday
fracday
Element set:     900
Inclination:       51
6504  deg
RA of node:       251
1487  deg
Eccentricity:     
0003841     
Arg of perigee:   343
1219  deg
Mean anomaly:      16
9817  deg
Mean motion:   15
76194875  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             222
Checksum:              293


Coasting Arc #2 (Orbit 234)
---------------------------------------

Vector Time (GMT): 2011/151/07:38:09
776
Vector Time (MET): 014/18:41:41
818
Weight (LBS)     : 212998
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1562735
51                 A    =         6717841
62  meter
 Y    =       -4940127
38  meter          E    =           
0008030
 Z    =        4268121
91                 I    =           51
32911
 XDOT =       5081
353158                 Wp   =           79
78989
 YDOT =       4627
315334  meter/sec      RA   =          246
31118  deg
 ZDOT =       3491
229482                 TA   =          334
73337
                                          MA   =          334
77262
                                          Ha   =            186
841  n
mi
                                          Hp   =            180
701

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5127085
02                 X    =         1597032
31
 Y    =      -16207766
98  feet           Y    =        -4922490
77  meter
 Z    =       14003024
63                 Z    =         4275796
75
 XDOT =      16671
106160                 XDOT =        5012
361882
 YDOT =      15181
480755  feet/sec       YDOT =        4683
655257  meter/sec
 ZDOT =      11454
164967                 ZDOT =        3515
747744

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4413288
94                 X    =         1345170
47
 Y    =      -16389781
18  feet           Y    =        -4995605
30  meter
 Z    =       14034292
43                 Z    =         4277652
33
 XDOT =      15980
925631                 XDOT =        4870
986132
 YDOT =      14207
666831  feet/sec       YDOT =        4330
496850  meter/sec
 ZDOT =      11553
225012                 ZDOT =        3521
422984


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 37577U  11020   11151
37201115  
00020000  00000-0  20000-3 0  9012
2 37577  51
6516 246
9033 0004725 342
3366  17
7633 15
76233068  2355


Satellite: SHUTTLE
Catalog Number: 37577
Epoch time:      11151
37201115   =   yrday
fracday
Element set:     901
Inclination:       51
6516  deg
RA of node:       246
9033  deg
Eccentricity:     
0004725     
Arg of perigee:   342
3366  deg
Mean anomaly:      17
7633  deg
Mean motion:   15
76233068  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             235
Checksum:              275


Coasting Arc #3 (Orbit 249)
---------------------------------------

Vector Time (GMT): 2011/152/07:42:56
916
Vector Time (MET): 015/18:46:28
958
Weight (LBS)     : 212998
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3749781
95                 A    =         6725546
61  meter
 Y    =       -5520626
76  meter          E    =           
0013850
 Z    =        -767662
16                 I    =           51
36981
 XDOT =       3624
846373                 Wp   =           24
23416
 YDOT =      -3283
437239  meter/sec      RA   =          241
08879  deg
 ZDOT =       5956
898501                 TA   =          327
35429
                                          MA   =          327
43983
                                          Ha   =            186
995  n
mi
                                          Hp   =            180
499

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12302434
20                 X    =        -3684148
09
 Y    =      -18112292
51  feet           Y    =        -5562120
71  meter
 Z    =       -2518576
64                 Z    =         -785719
84
 XDOT =      11892
540593                 XDOT =        3632
292910
 YDOT =     -10772
431888  feet/sec       YDOT =       -3242
930524  meter/sec
 ZDOT =      19543
630251                 ZDOT =        5974
525999

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13640088
34                 X    =        -4157498
93
 Y    =      -17116675
94  feet           Y    =        -5217162
83  meter
 Z    =       -2591457
19                 Z    =         -789876
15
 XDOT =       9666
106251                 XDOT =        2946
229185
 YDOT =     -10648
236089  feet/sec       YDOT =       -3245
582360  meter/sec
 ZDOT =      19615
124243                 ZDOT =        5978
689869


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 37577U  11020   11152
32301250  
00020000  00000-0  20000-3 0  9020
2 37577  51
6527 242
0051 0004678 348
0438  12
0615 15
76236582  2503


Satellite: SHUTTLE
Catalog Number: 37577
Epoch time:      11152
32301250   =   yrday
fracday
Element set:     902
Inclination:       51
6527  deg
RA of node:       242
0051  deg
Eccentricity:     
0004678     
Arg of perigee:   348
0438  deg
Mean anomaly:      12
0615  deg
Mean motion:   15
76236582  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             250
Checksum:              261


Coasting Arc #4 (Orbit 265)
---------------------------------------

Vector Time (GMT): 2011/153/07:48:03
714
Vector Time (MET): 016/18:51:35
756
Weight (LBS)     : 212998
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4563075
40                 A    =         6714984
10  meter
 Y    =         289826
53  meter          E    =           
0011835
 Z    =       -4927592
61                 I    =           51
35078
 XDOT =      -2675
403718                 Wp   =           84
01295
 YDOT =      -6911
178214  meter/sec      RA   =          235
88988  deg
 ZDOT =       2076
481575                 TA   =          206
16712
                                          MA   =          206
22698
                                          Ha   =            187
030  n
mi
                                          Hp   =            180
159

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14970719
82                 X    =        -4542035
05
 Y    =         950874
44  feet           Y    =          239004
95  meter
 Z    =      -16166642
44                 Z    =        -4949709
05
 XDOT =      -8777
571252                 XDOT =       -2608
143206
 YDOT =     -22674
469206  feet/sec       YDOT =       -6940
669626  meter/sec
 ZDOT =       6812
603591                 ZDOT =        2063
647075

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14662629
09                 X    =        -4469169
35
 Y    =        2670254
86  feet           Y    =          813893
68  meter
 Z    =      -16256198
48                 Z    =        -4954889
30
 XDOT =     -11196
063473                 XDOT =       -3412
560147
 YDOT =     -20427
970077  feet/sec       YDOT =       -6226
445279  meter/sec
 ZDOT =       6760
915187                 ZDOT =        2060
726949


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 37577U  11020   11153
33738744  
00020000  00000-0  20000-3 0  9035
2 37577  51
6527 236
7807 0004711 352
1495   7
9595 15
76287564  2662


Satellite: SHUTTLE
Catalog Number: 37577
Epoch time:      11153
33738744   =   yrday
fracday
Element set:     903
Inclination:       51
6527  deg
RA of node:       236
7807  deg
Eccentricity:     
0004711     
Arg of perigee:   352
1495  deg
Mean anomaly:       7
9595  deg
Mean motion:   15
76287564  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             266
Checksum:              325

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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