SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2010/134/18:20:08 955 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 80 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 80 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 56)
---------------------------------------
Vector Time (GMT): 2010/138/05:04:43
000
Vector Time (MET): 003/10:44:34
045
Weight (LBS) : 233701
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2892867
81 A = 6725280
61 meter
Y = 4643519
10 meter E =
0008354
Z = 3901747
39 I = 51
77963
XDOT = -6506
963755 Wp = 39
71988
YDOT = 628
317889 meter/sec RA = 23
90905 deg
ZDOT = 4078
209656 TA = 7
93248
MA = 7
91928
Ha = 190
996 n
mi
Hp = 184
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9491036
13 X = 2821774
09
Y = 15234642
72 feet Y = 4675470
85 meter
Z = 12801008
49 Z = 3915628
91
XDOT = -21348
306282 XDOT = -6533
317377
YDOT = 2061
410397 feet/sec YDOT = 555
405266 meter/sec
ZDOT = 13379
952938 ZDOT = 4046
534778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5265599
51 X = -1604954
73
Y = 17118093
51 feet Y = 5217594
90 meter
Z = 12856292
63 Z = 3918597
99
XDOT = -14412
927934 XDOT = -4393
060434
YDOT = -14383
788365 feet/sec YDOT = -4384
178694 meter/sec
ZDOT = 13253
783869 ZDOT = 4039
753323
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 36572U 10019A 10138
26663812
00020000 00000-0 20000-3 0 9000
2 36572 51
6440 24
1304 0010062 326
5541 33
4985 15
74074355 579
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10138
26663812 = yrday
fracday
Element set: 900
Inclination: 51
6440 deg
RA of node: 24
1304 deg
Eccentricity:
0010062
Arg of perigee: 326
5541 deg
Mean anomaly: 33
4985 deg
Mean motion: 15
74074355 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 57
Checksum: 260
Coasting Arc #2 (Orbit 71)
---------------------------------------
Vector Time (GMT): 2010/139/05:05:38
922
Vector Time (MET): 004/10:45:29
967
Weight (LBS) : 233604
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5822365
72 A = 6727428
53 meter
Y = -751359
93 meter E =
0009403
Z = -3274933
95 I = 51
75817
XDOT = 3320
652962 Wp = 357
93690
YDOT = 5076
663402 meter/sec RA = 18
72793 deg
ZDOT = 4747
711092 TA = 323
72637
MA = 323
79008
Ha = 191
358 n
mi
Hp = 184
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19102249
73 X = 5846243
87
Y = -2465091
63 feet Y = -686116
90 meter
Z = -10744533
95 Z = -3246590
96
XDOT = 10894
530715 XDOT = 3240
574461
YDOT = 16655
719822 feet/sec YDOT = 5113
348652 meter/sec
ZDOT = 15576
479961 ZDOT = 4763
648888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14744802
35 X = 4494215
76
Y = 12489066
88 feet Y = 3806667
58 meter
Z = -10631634
09 Z = -3240522
07
XDOT = -4103
420065 XDOT = -1250
722436
YDOT = 18133
664330 feet/sec YDOT = 5527
140888 meter/sec
ZDOT = 15639
954716 ZDOT = 4767
058197
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 36572U 10019A 10139
21894059
00020000 00000-0 20000-3 0 9016
2 36572 51
6438 19
2397 0010103 331
1302 28
9301 15
74060685 725
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10139
21894059 = yrday
fracday
Element set: 901
Inclination: 51
6438 deg
RA of node: 19
2397 deg
Eccentricity:
0010103
Arg of perigee: 331
1302 deg
Mean anomaly: 28
9301 deg
Mean motion: 15
74060685 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 72
Checksum: 262
Coasting Arc #3 (Orbit 87)
---------------------------------------
Vector Time (GMT): 2010/140/05:06:05
776
Vector Time (MET): 005/10:45:56
821
Weight (LBS) : 233604
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3049473
08 A = 6723908
41 meter
Y = -4211539
00 meter E =
0012781
Z = -4273946
96 I = 51
71800
XDOT = 6709
978148 Wp = 16
77437
YDOT = -1250
695918 meter/sec RA = 13
64652 deg
ZDOT = -3545
781378 TA = 217
21737
MA = 217
30603
Ha = 191
348 n
mi
Hp = 183
933
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10004832
94 X = -2981390
18
Y = -13817385
17 feet Y = -4245258
98 meter
Z = -14022135
69 Z = -4288596
30
XDOT = 22014
364001 XDOT = 6740
689723
YDOT = -4103
333065 feet/sec YDOT = -1175
488923 meter/sec
ZDOT = -11633
141003 ZDOT = -3513
109798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3192523
19 X = 973081
07
Y = -16708829
18 feet Y = -5092851
13 meter
Z = -14080480
37 Z = -4291730
42
XDOT = 16959
490256 XDOT = 5169
252630
YDOT = 12959
766750 feet/sec YDOT = 3950
136905 meter/sec
ZDOT = -11502
998460 ZDOT = -3506
113930
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 36572U 10019A 10140
23471445
00020000 00000-0 20000-3 0 9021
2 36572 51
6439 14
0222 0010131 334
8019 25
2648 15
74097574 880
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10140
23471445 = yrday
fracday
Element set: 902
Inclination: 51
6439 deg
RA of node: 14
0222 deg
Eccentricity:
0010131
Arg of perigee: 334
8019 deg
Mean anomaly: 25
2648 deg
Mean motion: 15
74097574 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 88
Checksum: 262
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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