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 50)
---------------------------------------
Vector Time (GMT): 2010/042/11:28:12
000
Vector Time (MET): 003/02:14:05
019
Weight (LBS) : 245190
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6041803
02 A = 6723193
70 meter
Y = 272472
85 meter E =
0010636
Z = 2920255
41 I = 51
79362
XDOT = 2194
454786 Wp = 29
15905
YDOT = -5398
367068 meter/sec RA = 155
08084 deg
ZDOT = 5045
321815 TA = 4
43815
MA = 4
42873
Ha = 187
905 n
mi
Hp = 182
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19822188
40 X = -6058587
63
Y = 893939
79 feet Y = 204781
46 meter
Z = 9580890
44 Z = 2890864
47
XDOT = 7199
654810 XDOT = 2230
179252
YDOT = -17711
178046 feet/sec YDOT = -5373
615207 meter/sec
ZDOT = 16552
893093 ZDOT = 5056
068743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14137669
35 X = -4309161
62
Y = -14002354
30 feet Y = -4267917
59 meter
Z = 9464254
98 Z = 2884704
92
XDOT = 16811
333836 XDOT = 5124
094553
YDOT = -5760
207266 feet/sec YDOT = -1755
711175 meter/sec
ZDOT = 16595
329578 ZDOT = 5058
256456
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 10042
53549026
00020000 00000-0 20000-3 0 9000
2 36394 51
6455 155
7720 0011001 312
2728 47
7502 15
75884966 518
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10042
53549026 = yrday
fracday
Element set: 900
Inclination: 51
6455 deg
RA of node: 155
7720 deg
Eccentricity:
0011001
Arg of perigee: 312
2728 deg
Mean anomaly: 47
7502 deg
Mean motion: 15
75884966 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 51
Checksum: 275
Coasting Arc #2 (Orbit 65)
---------------------------------------
Vector Time (GMT): 2010/043/11:32:45
372
Vector Time (MET): 004/02:18:38
391
Weight (LBS) : 244725
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3856785
04 A = 6723532
16 meter
Y = 4752011
55 meter E =
0011120
Z = -2766145
90 I = 51
82205
XDOT = -5528
450230 Wp = 341
38751
YDOT = -1484
992618 meter/sec RA = 149
88025 deg
ZDOT = 5161
789001 TA = 347
01623
MA = 347
04483
Ha = 188
121 n
mi
Hp = 182
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12653494
24 X = -3896226
01
Y = 15590589
07 feet Y = 4708640
15 meter
Z = -9075281
84 Z = -2784977
31
XDOT = -18137
960072 XDOT = -5536
499339
YDOT = -4872
023026 feet/sec YDOT = -1546
891575 meter/sec
ZDOT = 16935
003285 ZDOT = 5134
913070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19939841
25 X = -6077663
61
Y = 2054594
73 feet Y = 626240
47 meter
Z = -9149835
83 Z = -2788869
96
XDOT = -9251
850061 XDOT = -2819
963899
YDOT = -14914
668243 feet/sec YDOT = -4545
990881 meter/sec
ZDOT = 16828
267630 ZDOT = 5129
255974
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 10043
48670836
00020000 00000-0 20000-3 0 9010
2 36394 51
6460 150
8750 0011245 316
7041 43
3239 15
75845993 662
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10043
48670836 = yrday
fracday
Element set: 901
Inclination: 51
6460 deg
RA of node: 150
8750 deg
Eccentricity:
0011245
Arg of perigee: 316
7041 deg
Mean anomaly: 43
3239 deg
Mean motion: 15
75845993 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 66
Checksum: 289
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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