[list_settings.list_name] Current STS TLEs @ 18:30 UTC

 
Date: July 19th 2011

SHUTTLE TRAJECTORY DATA

Lift off time (UTC) : 2011/189/15:29:03 960 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 99 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 52 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


200/07:50:09 702 2 8 0 0 3 0
010/16:21:05 742 0 6 0 0 214 1
000/00:00:11 483 0 9 3 0 205 2

200/08:18:22 735 -7 5 -10 0 10 0
010/16:49:18 774 -4 0 -0 0 210 3
000/00:00:37 549 -5 3 -0 0 202 0

201/05:06:23 060 5 6 -10 0 10 0
011/13:37:19 099 4 8 -0 0 209 0
000/00:00:38 199 6 8 -0 0 198 6

Coasting Arc #1 (Orbit 156)
---------------------------------------

Vector Time (GMT): 2011/199/13:09:30
000
Vector Time (MET): 009/21:40:26
040
Weight (LBS)     : 216000
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5913802
54                 A    =         6769429
04  meter
 Y    =        1896775
13  meter          E    =           
0011816
 Z    =        2696679
06                 I    =           51
66388
 XDOT =      -3735
808595                 Wp   =           49
99903
 YDOT =      -4250
090585  meter/sec      RA   =            2
29894  deg
 ZDOT =      -5180
748627                 TA   =           99
48582
                                          MA   =           99
35225
                                          Ha   =            213
770  n
mi
                                          Hp   =            205
564

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19402239
30                 X    =        -5947672
80
 Y    =        6223015
51  feet           Y    =         1830453
79  meter
 Z    =        8847372
25                 Z    =         2667868
34
 XDOT =     -12256
589878                 XDOT =       -3662
839032
 YDOT =     -13943
866748  feet/sec       YDOT =       -4291
458255  meter/sec
 ZDOT =     -16997
206782                 ZDOT =       -5198
719885

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17746904
29                 X    =         5409256
43
 Y    =       10113333
05  feet           Y    =         3082543
91  meter
 Z    =        8730217
11                 Z    =         2660970
17
 XDOT =      -1305
501095                 XDOT =        -397
916734
 YDOT =      17090
763950  feet/sec       YDOT =        5209
264852  meter/sec
 ZDOT =     -17069
931700                 ZDOT =       -5202
915182


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 37736U 11031A   11199
58567921  
00020000  00000-0  20000-3 0  9005
2 37736  51
6381   2
6490 0011208 338
2110  21
8567 15
59954333  1572


Satellite: SHUTTLE
Catalog Number: 37736
Epoch time:      11199
58567921   =   yrday
fracday
Element set:     900
Inclination:       51
6381  deg
RA of node:         2
6490  deg
Eccentricity:     
0011208     
Arg of perigee:   338
2110  deg
Mean anomaly:      21
8567  deg
Mean motion:   15
59954333  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             157
Checksum:              293


Coasting Arc #2 (Orbit 168)
---------------------------------------

Vector Time (GMT): 2011/200/07:50:15
444
Vector Time (MET): 010/16:21:11
483
Weight (LBS)     : 215925
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6271383
69                 A    =         6770495
40  meter
 Y    =       -1482340
16  meter          E    =           
0006905
 Z    =       -2089665
51                 I    =           51
64719
 XDOT =       2897
849210                 Wp   =          352
89971
 YDOT =      -4454
999241  meter/sec      RA   =          358
43148  deg
 ZDOT =      -5527
971998                 TA   =          210
26276
                                          MA   =          210
30266
                                          Ha   =            214
130  n
mi
                                          Hp   =            205
179

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20575405
80                 X    =        -6244190
76
 Y    =       -4863320
75  feet           Y    =        -1552318
41  meter
 Z    =       -6855857
97                 Z    =        -2120065
33
 XDOT =       9507
379298                 XDOT =        2974
303847
 YDOT =     -14616
139241  feet/sec       YDOT =       -4422
165855  meter/sec
 ZDOT =     -18136
391071                 ZDOT =       -5513
709139

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16114069
80                 X    =        -4911568
48
 Y    =       13624569
39  feet           Y    =         4152768
75  meter
 Z    =       -6979245
26                 Z    =        -2127273
96
 XDOT =      -5048
051850                 XDOT =       -1538
646204
 YDOT =     -15245
349386  feet/sec       YDOT =       -4646
782493  meter/sec
 ZDOT =     -18078
167950                 ZDOT =       -5510
225591


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 37736U 11031A   11200
35440465  
00020000  00000-0  20000-3 0  9017
2 37736  51
6410 358
7883 0012654 336
7693  23
2889 15
59960683  1692


Satellite: SHUTTLE
Catalog Number: 37736
Epoch time:      11200
35440465   =   yrday
fracday
Element set:     901
Inclination:       51
6410  deg
RA of node:       358
7883  deg
Eccentricity:     
0012654     
Arg of perigee:   336
7693  deg
Mean anomaly:      23
2889  deg
Mean motion:   15
59960683  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             169
Checksum:              315


Coasting Arc #3 (Orbit 168)
---------------------------------------

Vector Time (GMT): 2011/200/08:18:41
509
Vector Time (MET): 010/16:49:37
549
Weight (LBS)     : 215632
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4608219
05                 A    =         6760852
01  meter
 Y    =       -3156339
47  meter          E    =           
0008241
 Z    =       -3810984
21                 I    =           51
63155
 XDOT =       5611
182173                 Wp   =           53
74605
 YDOT =       3149
146062  meter/sec      RA   =          358
28649  deg
 ZDOT =       4187
883869                 TA   =          260
29409
                                          MA   =          260
38719
                                          Ha   =            210
271  n
mi
                                          Hp   =            202
012

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15118828
91                 X    =         4661684
06
 Y    =      -10355444
46  feet           Y    =        -3104508
35  meter
 Z    =      -12503229
04                 Z    =        -3788468
29
 XDOT =      18409
390332                 XDOT =        5555
207203
 YDOT =      10331
844037  feet/sec       YDOT =        3211
580451  meter/sec
 ZDOT =      13739
776473                 ZDOT =        4215
006707

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1585537
83                 X    =         -483271
93
 Y    =      -18318953
16  feet           Y    =        -5583616
92  meter
 Z    =      -12411566
35                 Z    =        -3783045
42
 XDOT =      16649
483342                 XDOT =        5074
762523
 YDOT =     -10799
821682  feet/sec       YDOT =       -3291
785649  meter/sec
 ZDOT =      13849
744947                 ZDOT =        4221
402260


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 37736U 11031A   11200
35440592  
00020000  00000-0  20000-3 0  9029
2 37736  51
6403 358
7870 0006293   7
2415 352
8831 15
61848171  1692


Satellite: SHUTTLE
Catalog Number: 37736
Epoch time:      11200
35440592   =   yrday
fracday
Element set:     902
Inclination:       51
6403  deg
RA of node:       358
7870  deg
Eccentricity:     
0006293     
Arg of perigee:     7
2415  deg
Mean anomaly:     352
8831  deg
Mean motion:   15
61848171  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             169
Checksum:              287


Coasting Arc #4 (Orbit 182)
---------------------------------------

Vector Time (GMT): 2011/201/05:06:42
159
Vector Time (MET): 011/13:37:38
199
Weight (LBS)     : 215383
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5636407
73                 A    =         6758806
49  meter
 Y    =        2675389
07  meter          E    =           
0014545
 Z    =        2604822
95                 I    =           51
61754
 XDOT =      -4200
702427                 Wp   =           47
24240
 YDOT =      -3723
877202  meter/sec      RA   =          353
91913  deg
 ZDOT =      -5236
656193                 TA   =          103
31923
                                          MA   =          103
15700
                                          Ha   =            209
002  n
mi
                                          Hp   =            198
588

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18492151
34                 X    =        -5678559
08
 Y    =        8777523
18  feet           Y    =         2612123
47  meter
 Z    =        8546007
04                 Z    =         2577339
53
 XDOT =     -13781
832111                 XDOT =       -4133
310812
 YDOT =     -12217
444887  feet/sec       YDOT =       -3770
474871  meter/sec
 ZDOT =     -17180
630553                 ZDOT =       -5256
899405

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15976010
36                 X    =        -4869487
96
 Y    =       12871290
76  feet           Y    =         3923169
42  meter
 Z    =        8434202
86                 Z    =         2570745
03
 XDOT =     -15217
870176                 XDOT =       -4638
406830
 YDOT =      -7515
440992  feet/sec       YDOT =       -2290
706414  meter/sec
 ZDOT =     -17262
614861                 ZDOT =       -5261
645010


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 37736U 11031A   11201
25013107  
00020000  00000-0  20000-3 0  9038
2 37736  51
6414 354
2699 0013249 348
9055  11
1809 15
63704575  1835


Satellite: SHUTTLE
Catalog Number: 37736
Epoch time:      11201
25013107   =   yrday
fracday
Element set:     903
Inclination:       51
6414  deg
RA of node:       354
2699  deg
Eccentricity:     
0013249     
Arg of perigee:   348
9055  deg
Mean anomaly:      11
1809  deg
Mean motion:   15
63704575  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             183
Checksum:              279


Coasting Arc #5 (Orbit 198)
---------------------------------------

Vector Time (GMT): 2011/202/05:08:18
431
Vector Time (MET): 012/13:39:14
470
Weight (LBS)     : 215383
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6140507
72                 A    =         6758516
20  meter
 Y    =         923442
26  meter          E    =           
0019854
 Z    =        2634107
20                 I    =           51
58740
 XDOT =      -2966
319706                 Wp   =           35
15950
 YDOT =       4805
670071  meter/sec      RA   =          348
89646  deg
 ZDOT =       5226
632844                 TA   =          354
73417
                                          MA   =          354
75502
                                          Ha   =            209
070  n
mi
                                          Hp   =            198
202

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20146022
71                 X    =         6116929
39
 Y    =        3029666
22  feet           Y    =          991977
16  meter
 Z    =        8642083
98                 Z    =         2663880
17
 XDOT =      -9732
020034                 XDOT =       -3045
226866
 YDOT =      15766
634092  feet/sec       YDOT =        4772
057344  meter/sec
 ZDOT =      17147
745550                 ZDOT =        5212
031308

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20196672
41                 X    =         6155945
75
 Y    =       -2243175
76  feet           Y    =         -683719
97  meter
 Z    =        8762951
01                 Z    =         2670947
47
 XDOT =      -5609
449423                 XDOT =       -1709
760184
 YDOT =      16294
687481  feet/sec       YDOT =        4966
620744  meter/sec
 ZDOT =      17088
131542                 ZDOT =        5208
462494


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 37736U 11031A   11202
27264280  
00020000  00000-0  20000-3 0  9042
2 37736  51
6419 349
0980 0013455 352
7013   7
3947 15
63724878  1996


Satellite: SHUTTLE
Catalog Number: 37736
Epoch time:      11202
27264280   =   yrday
fracday
Element set:     904
Inclination:       51
6419  deg
RA of node:       349
0980  deg
Eccentricity:     
0013455     
Arg of perigee:   352
7013  deg
Mean anomaly:       7
3947  deg
Mean motion:   15
63724878  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             199
Checksum:              304


Coasting Arc #6 (Orbit 213)
---------------------------------------

Vector Time (GMT): 2011/203/05:09:47
315
Vector Time (MET): 013/13:40:43
354
Weight (LBS)     : 215383
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1307450
44                 A    =         6749405
50  meter
 Y    =       -3998061
66  meter          E    =           
0019481
 Z    =       -5290476
01                 I    =           51
52768
 XDOT =       7342
274202                 Wp   =           45
26800
 YDOT =      -2228
932717  meter/sec      RA   =          343
80677  deg
 ZDOT =       -116
916959                 TA   =          223
53996
                                          MA   =          223
69390
                                          Ha   =            209
180  n
mi
                                          Hp   =            197
889

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4289535
58                 X    =        -1236946
27
 Y    =      -13117000
19  feet           Y    =        -4012287
77  meter
 Z    =      -17357204
74                 Z    =        -5296656
57
 XDOT =      24088
826121                 XDOT =        7367
220819
 YDOT =      -7312
771380  feet/sec       YDOT =       -2146
687442  meter/sec
 ZDOT =       -383
585825                 ZDOT =         -81
188141

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7692634
88                 X    =        -2344715
11
 Y    =      -11419984
66  feet           Y    =        -3480811
33  meter
 Z    =      -17382050
65                 Z    =        -5298049
04
 XDOT =      20244
343475                 XDOT =        6170
475891
 YDOT =     -13208
368088  feet/sec       YDOT =       -4025
910593  meter/sec
 ZDOT =       -238
332424                 ZDOT =         -72
643723


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 37736U 11031A   11203
23123496  
00020000  00000-0  20000-3 0  9053
2 37736  51
6420 344
2499 0013487 355
7239   4
3801 15
63778018  2147


Satellite: SHUTTLE
Catalog Number: 37736
Epoch time:      11203
23123496   =   yrday
fracday
Element set:     905
Inclination:       51
6420  deg
RA of node:       344
2499  deg
Eccentricity:     
0013487     
Arg of perigee:   355
7239  deg
Mean anomaly:       4
3801  deg
Mean motion:   15
63778018  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             214
Checksum:              286


Coasting Arc #7 (Orbit 229)
---------------------------------------

Vector Time (GMT): 2011/204/05:11:31
235
Vector Time (MET): 014/13:42:27
274
Weight (LBS)     : 215383
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4632176
47                 A    =         6758361
81  meter
 Y    =        4112998
72  meter          E    =           
0017047
 Z    =        2706445
81                 I    =           51
52852
 XDOT =      -5157
418542                 Wp   =           50
57742
 YDOT =      -2391
413518  meter/sec      RA   =          338
71188  deg
 ZDOT =      -5160
532786                 TA   =           98
66776
                                          MA   =           98
47461
                                          Ha   =            209
391  n
mi
                                          Hp   =            197
729

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15197429
35                 X    =        -4690971
85
 Y    =       13494090
30  feet           Y    =         4060869
94  meter
 Z    =        8879415
39                 Z    =         2683800
42
 XDOT =     -16920
664507                 XDOT =       -5105
225268
 YDOT =      -7845
844874  feet/sec       YDOT =       -2448
794656  meter/sec
 ZDOT =     -16930
881843                 ZDOT =       -5185
460727

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10428914
97                 X    =        -3178733
28
 Y    =       17490555
08  feet           Y    =         5331121
19  meter
 Z    =        8787181
84                 Z    =         2678333
03
 XDOT =     -17132
159137                 XDOT =       -5221
882105
 YDOT =      -1604
585547  feet/sec       YDOT =        -489
077675  meter/sec
 ZDOT =     -17031
968880                 ZDOT =       -5191
344115


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 37736U 11031A   11204
25372407  
00020000  00000-0  20000-3 0  9065
2 37736  51
6419 339
0783 0013530 359
8236    
2915 15
63775304  2308


Satellite: SHUTTLE
Catalog Number: 37736
Epoch time:      11204
25372407   =   yrday
fracday
Element set:     906
Inclination:       51
6419  deg
RA of node:       339
0783  deg
Eccentricity:     
0013530     
Arg of perigee:   359
8236  deg
Mean anomaly:        
2915  deg
Mean motion:   15
63775304  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             230
Checksum:              279

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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