[list_settings.list_name] Current STS TLEs @ 06:30 UTC
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
There are no maneuvers
Coasting Arc #1 (Orbit 188)
---------------------------------------
Vector Time (GMT): 2011/201/13:47:30
000
Vector Time (MET): 011/22:18:26
040
Weight (LBS) : 235971
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6188636
73 A = 6759888
26 meter
Y = 1107909
15 meter E =
0016142
Z = 2454442
66 I = 51
60777
XDOT = -2957
673445 Wp = 37
78014
YDOT = 4679
621253 meter/sec RA = 352
13032 deg
ZDOT = 5339
155205 TA = 349
86491
MA = 349
89742
Ha = 207
962 n
mi
Hp = 200
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20303926
28 X = 6163864
87
Y = 3634872
54 feet Y = 1176975
59 meter
Z = 8052633
39 Z = 2484446
48
XDOT = -9703
653035 XDOT = -3035
718295
YDOT = 15353
088100 feet/sec YDOT = 4646
110034 meter/sec
ZDOT = 17516
913403 ZDOT = 5324
597784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14270989
24 X = -4349797
52
Y = -14826469
26 feet Y = -4519107
83 meter
Z = 8174429
68 Z = 2491566
17
XDOT = 15869
728234 XDOT = 4837
093166
YDOT = -5639
460392 feet/sec YDOT = -1718
907527 meter/sec
ZDOT = 17457
484437 ZDOT = 5321
041257
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
63359910
00020000 00000-0 20000-3 0 9002
2 37736 51
6418 352
3287 0009792 340
2714 19
8063 15
63387558 1897
Satellite: SHUTTLE
Catalog Number: 37736
Epoch time: 11201
63359910 = yrday
fracday
Element set: 900
Inclination: 51
6418 deg
RA of node: 352
3287 deg
Eccentricity:
0009792
Arg of perigee: 340
2714 deg
Mean anomaly: 19
8063 deg
Mean motion: 15
63387558 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 189
Checksum: 305
Coasting Arc #2 (Orbit 203)
---------------------------------------
Vector Time (GMT): 2011/202/13:49:23
897
Vector Time (MET): 012/22:20:19
937
Weight (LBS) : 235971
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1301901
46 A = 6750567
95 meter
Y = -4007171
48 meter E =
0015874
Z = -5285175
85 I = 51
54645
XDOT = 7410
736233 Wp = 49
69455
YDOT = -1968
261556 meter/sec RA = 347
04735 deg
ZDOT = -323
751125 TA = 217
16249
MA = 217
27247
Ha = 208
238 n
mi
Hp = 199
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4271330
24 X = -1231321
62
Y = -13146888
07 feet Y = -4021335
15 meter
Z = -17339815
77 Z = -5291329
24
XDOT = 24313
439084 XDOT = 7433
767636
YDOT = -6457
551036 feet/sec YDOT = -1885
261392 meter/sec
ZDOT = -1062
175606 ZDOT = -287
694408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4003045
20 X = -1220128
18
Y = 13198565
38 feet Y = 4022922
73 meter
Z = -17364551
25 Z = -5292715
22
XDOT = -22743
691706 XDOT = -6932
277232
YDOT = -8143
246029 feet/sec YDOT = -2482
061390 meter/sec
ZDOT = -915
603375 ZDOT = -279
075909
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
59242903
00020000 00000-0 20000-3 0 9012
2 37736 51
6418 347
4833 0009983 344
2201 15
8644 15
63383039 2045
Satellite: SHUTTLE
Catalog Number: 37736
Epoch time: 11202
59242903 = yrday
fracday
Element set: 901
Inclination: 51
6418 deg
RA of node: 347
4833 deg
Eccentricity:
0009983
Arg of perigee: 344
2201 deg
Mean anomaly: 15
8644 deg
Mean motion: 15
63383039 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 204
Checksum: 283
Coasting Arc #3 (Orbit 219)
---------------------------------------
Vector Time (GMT): 2011/203/13:50:54
831
Vector Time (MET): 013/22:21:50
870
Weight (LBS) : 235971
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4514273
24 A = 6758717
09 meter
Y = 4008946
05 meter E =
0013739
Z = 3038744
63 I = 51
54419
XDOT = -5410
271587 Wp = 53
04666
YDOT = -2345
929918 meter/sec RA = 341
95398 deg
ZDOT = -4918
959642 TA = 91
91554
MA = 91
75818
Ha = 208
427 n
mi
Hp = 199
890
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14810607
76 X = -4573528
07
Y = 13152710
15 feet Y = 3958133
16 meter
Z = 9969634
62 Z = 3016670
88
XDOT = -17750
234867 XDOT = -5359
741663
YDOT = -7696
620466 feet/sec YDOT = -2406
147971 meter/sec
ZDOT = -16138
319035 ZDOT = -4945
119922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19639705
77 X = 5986182
32
Y = -2900765
32 feet Y = -884153
27 meter
Z = 9879727
67 Z = 3011340
99
XDOT = 10375
304939 XDOT = 3162
392945
YDOT = 14654
866063 feet/sec YDOT = 4466
803176 meter/sec
ZDOT = -16244
415890 ZDOT = -4951
297963
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
61517193
00020000 00000-0 20000-3 0 9023
2 37736 51
6419 342
3133 0009909 348
1656 11
9267 15
63369760 2209
Satellite: SHUTTLE
Catalog Number: 37736
Epoch time: 11203
61517193 = yrday
fracday
Element set: 902
Inclination: 51
6419 deg
RA of node: 342
3133 deg
Eccentricity:
0009909
Arg of perigee: 348
1656 deg
Mean anomaly: 11
9267 deg
Mean motion: 15
63369760 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 220
Checksum: 288
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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