SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2010/039/09:14:06 981 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 77 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 07 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 07803
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 114)
---------------------------------------
Vector Time (GMT): 2010/046/13:11:12
000
Vector Time (MET): 007/03:57:05
019
Weight (LBS) : 210582
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1317167
53 A = 6715340
58 meter
Y = -4284344
26 meter E =
0013082
Z = 5005224
16 I = 51
87029
XDOT = 6172
188412 Wp = 355
19012
YDOT = -4176
396854 meter/sec RA = 134
13628 deg
ZDOT = -1938
221953 TA = 113
54078
MA = 113
40330
Ha = 188
430 n
mi
Hp = 181
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4321415
79 X = -1293450
75
Y = -14056247
58 feet Y = -4298948
23 meter
Z = 16421339
12 Z = 4998883
30
XDOT = 20249
961980 XDOT = 6227
869553
YDOT = -13702
089415 feet/sec YDOT = -4107
029257 meter/sec
ZDOT = -6358
995908 ZDOT = -1908
102804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22870
54 X = 6970
94
Y = -14733771
85 feet Y = -4490853
66 meter
Z = 16395991
98 Z = 4997498
36
XDOT = 22398
476943 XDOT = 6827
055772
YDOT = -6954
108199 feet/sec YDOT = -2119
612179 meter/sec
ZDOT = -6239
590841 ZDOT = -1901
827288
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 36394U 10004A 10046
59378278
00020000 00000-0 20000-3 0 9009
2 36394 51
6463 134
8794 0011406 329
3314 30
7182 15
76095963 1154
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10046
59378278 = yrday
fracday
Element set: 900
Inclination: 51
6463 deg
RA of node: 134
8794 deg
Eccentricity:
0011406
Arg of perigee: 329
3314 deg
Mean anomaly: 30
7182 deg
Mean motion: 15
76095963 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 115
Checksum: 300
Coasting Arc #2 (Orbit 130)
---------------------------------------
Vector Time (GMT): 2010/047/13:15:55
357
Vector Time (MET): 008/04:01:48
376
Weight (LBS) : 210582
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5264147
35 A = 6720162
36 meter
Y = 1845521
71 meter E =
0011181
Z = 3734082
17 I = 51
90610
XDOT = 816
792636 Wp = 37
22734
YDOT = -6352
068262 meter/sec RA = 129
02817 deg
ZDOT = 4292
993750 TA = 7
74963
MA = 7
73237
Ha = 188
694 n
mi
Hp = 180
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17270824
65 X = -5302542
34
Y = 6054861
26 feet Y = 1786410
34 meter
Z = 12250925
77 Z = 3708416
13
XDOT = 2679
765866 XDOT = 866
943813
YDOT = -20840
118970 feet/sec YDOT = -6342
648993 meter/sec
ZDOT = 14084
625164 ZDOT = 4297
083770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18327111
42 X = -5586103
56
Y = 1242686
56 feet Y = 378770
86 meter
Z = 12149099
90 Z = 3703045
65
XDOT = 8117
506192 XDOT = 2474
215887
YDOT = -18070
014975 feet/sec YDOT = -5507
740564 meter/sec
ZDOT = 14100
608975 ZDOT = 4297
865616
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 36394U 10004A 10047
60827208
00020000 00000-0 20000-3 0 9015
2 36394 51
6455 129
6541 0011338 334
1266 25
9330 15
76120890 1318
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10047
60827208 = yrday
fracday
Element set: 901
Inclination: 51
6455 deg
RA of node: 129
6541 deg
Eccentricity:
0011338
Arg of perigee: 334
1266 deg
Mean anomaly: 25
9330 deg
Mean motion: 15
76120890 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 131
Checksum: 270
Coasting Arc #3 (Orbit 145)
---------------------------------------
Vector Time (GMT): 2010/048/13:20:33
570
Vector Time (MET): 009/04:06:26
589
Weight (LBS) : 210582
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2417282
85 A = 6724800
32 meter
Y = 6023434
08 meter E =
0016736
Z = -1719399
09 I = 51
93947
XDOT = -5128
774776 Wp = 1
63713
YDOT = -424
127266 meter/sec RA = 123
83775 deg
ZDOT = 5742
389358 TA = 339
38271
MA = 339
45016
Ha = 188
794 n
mi
Hp = 180
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7930718
03 X = -2476140
02
Y = 19761922
83 feet Y = 5996059
49 meter
Z = -5641073
12 Z = -1731285
32
XDOT = -16826
688896 XDOT = -5151
543218
YDOT = -1391
493656 feet/sec YDOT = -481
636528 meter/sec
ZDOT = 18839
860099 ZDOT = 5717
418903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12207365
60 X = -3720805
04
Y = 17432100
61 feet Y = 5313304
27 meter
Z = -5688029
70 Z = -1733711
45
XDOT = -14898
989545 XDOT = -4541
212013
YDOT = -4337
265016 feet/sec YDOT = -1321
998377 meter/sec
ZDOT = 18740
701404 ZDOT = 5712
165788
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 36394U 10004A 10048
55932681
00020000 00000-0 20000-3 0 9023
2 36394 51
6449 124
7553 0011535 338
3773 21
6903 15
76133558 1468
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10048
55932681 = yrday
fracday
Element set: 902
Inclination: 51
6449 deg
RA of node: 124
7553 deg
Eccentricity:
0011535
Arg of perigee: 338
3773 deg
Mean anomaly: 21
6903 deg
Mean motion: 15
76133558 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 146
Checksum: 298
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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