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