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Date:
February 22nd 2010
<B> SHUTTLE TRAJECTORY DATA</B>
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 191)
Vector Time (GMT): 2010/051/11:10:46.000 Vector Time (MET): 012/01:56:39.019 Weight (LBS) : 209039.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2384032.83 A = 6716752.69 meter
Y = 4237759.19 meter E = .0010200
Z = -4636772.59 I = 51.95081
XDOT = -4353.229867 Wp = 45.97723
YDOT = 5638.761038 meter/sec RA = 108.91550 deg
ZDOT = 2926.152583 TA = 252.81575
MA = 252.92744
Ha = 188.979 n.mi
Hp = 180.054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7821630.02 X = 2358968.41
Y = 13903409.42 feet Y = 4264292.14 meter
Z = -15212508.51 Z = -4625252.01
XDOT = -14282.250221 XDOT = -4430.206344
YDOT = 18499.872173 feet/sec YDOT = 5589.625300 meter/sec
ZDOT = 9600.238134 ZDOT = 2904.817725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3641807.68 X = -1110022.98
Y = 15576077.63 feet Y = 4747588.46 meter
Z = -15166612.91 Z = -4622783.62
XDOT = -21954.413239 XDOT = -6691.705155
YDOT = 4097.602082 feet/sec YDOT = 1248.949114 meter/sec
ZDOT = 9515.717450 ZDOT = 2900.390679
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 10051.47660669 .00020000 00000-0 20000-3 0 9000
2 36394 51.6438 109.7392 0011065 345.6248 14.4600 15.76146754 1923
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10051.47660669 = yrday.fracday
Element set: 900
Inclination: 51.6438 deg
RA of node: 109.7392 deg
Eccentricity: .0011065
Arg of perigee: 345.6248 deg
Mean anomaly: 14.4600 deg
Mean motion: 15.76146754 rev/day Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 192
Checksum: 290
Coasting Arc #2 (Orbit 207)
Vector Time (GMT): 2010/052/11:15:24.504 Vector Time (MET): 013/02:01:17.523 Weight (LBS) : 209039.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4219303.52 A = 6718013.49 meter
Y = -2930639.42 meter E = .0015330
Z = -4342706.64 I = 51.96339
XDOT = 1127.115067 Wp = 23.99785
YDOT = 6774.054430 meter/sec RA = 103.81620 deg
ZDOT = -3466.892248 TA = 211.05311
MA = 211.14381
Ha = 189.097 n.mi
Hp = 179.943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13842859.32 X = 4272873.14
Y = -9614958.74 feet Y = -2883132.98 meter
Z = -14247725.20 Z = -4322079.35
XDOT = 3697.884077 XDOT = 1068.085384
YDOT = 22224.588024 feet/sec YDOT = 6786.334701 meter/sec
ZDOT = -11374.318399 ZDOT = -3461.560138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16829694.65 X = 5129690.93
Y = 1777149.16 feet Y = 541675.07 meter
Z = -14165909.01 Z = -4317769.07
XDOT = -11492.084292 XDOT = -3502.787292
YDOT = 18086.735753 feet/sec YDOT = 5512.837057 meter/sec
ZDOT = -11352.917567 ZDOT = -3460.369274
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 10052.49106230 .00020000 00000-0 20000-3 0 9013
2 36394 51.6437 104.5130 0011086 349.4364 10.6565 15.76131913 2086
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10052.49106230 = yrday.fracday
Element set: 901
Inclination: 51.6437 deg
RA of node: 104.5130 deg
Eccentricity: .0011086
Arg of perigee: 349.4364 deg
Mean anomaly: 10.6565 deg
Mean motion: 15.76131913 rev/day Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 208
Checksum: 256
Coasting Arc #3 (Orbit 223)
Vector Time (GMT): 2010/053/11:20:06.741 Vector Time (MET): 014/02:05:59.760 Weight (LBS) : 209039.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 412231.72 A = 6725671.39 meter
Y = -6670931.79 meter E = .0010064
Z = 760863.64 I = 51.99668
XDOT = 4803.292823 Wp = 71.87381
YDOT = -395.379647 meter/sec RA = 98.63941 deg
ZDOT = -6001.439263 TA = 99.87323
MA = 99.75961
Ha = 189.217 n.mi
Hp = 179.444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1352466.27 X = 483138.46
Y = -21886259.14 feet Y = -6665922.97 meter
Z = 2496271.77 Z = 763038.34
XDOT = 15758.834720 XDOT = 4836.512522
YDOT = -1297.177320 feet/sec YDOT = -341.453107 meter/sec
ZDOT = -19689.761361 ZDOT = -5978.024475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14667384.62 X = 4470618.83
Y = -16299177.96 feet Y = -4967989.44 meter
Z = 2504696.20 Z = 763431.40
XDOT = 12044.781778 XDOT = 3671.249486
YDOT = 7793.571140 feet/sec YDOT = 2375.480483 meter/sec
ZDOT = -19596.783059 ZDOT = -5973.099476
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 10053.50550282 .00020000 00000-0 20000-3 0 9027
2 36394 51.6445 99.2870 0011318 353.9357 6.1668 15.76198300 2241
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10053.50550282 = yrday.fracday
Element set: 902
Inclination: 51.6445 deg
RA of node: 99.2870 deg
Eccentricity: .0011318
Arg of perigee: 353.9357 deg
Mean anomaly: 6.1668 deg
Mean motion: 15.76198300 rev/day Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 224
Checksum: 285
Coasting Arc #4 (Orbit 239)
Vector Time (GMT): 2010/054/11:24:41.551 Vector Time (MET): 015/02:10:34.570 Weight (LBS) : 209039.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3803932.59 A = 6714903.29 meter
Y = -2302077.61 meter E = .0014996
Z = 5032461.12 I = 51.96371
XDOT = 1897.394789 Wp = 15.63099
YDOT = -7231.830972 meter/sec RA = 93.48748 deg
ZDOT = -1858.563198 TA = 92.29080
MA = 92.11908
Ha = 189.354 n.mi
Hp = 179.218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12480093.80 X = -3802340.67
Y = -7552748.07 feet Y = -2344628.32 meter
Z = 16510699.22 Z = 5013985.73
XDOT = 6225.048519 XDOT = 1987.190817
YDOT = -23726.479568 feet/sec YDOT = -7210.100002 meter/sec
ZDOT = -6097.648289 ZDOT = -1849.127897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5652713.96 X = -1722947.21
Y = -13537489.50 feet Y = -4126226.80 meter
Z = 16437248.44 Z = 5010073.33
XDOT = 18119.019713 XDOT = 5522.677209
YDOT = -14985.964381 feet/sec YDOT = -4567.721943 meter/sec
ZDOT = -6060.394082 ZDOT = -1847.208116
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 10054.51992696 .00020000 00000-0 20000-3 0 9039
2 36394 51.6442 94.0612 0011277 357.5052 2.6054 15.76225556 2403
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10054.51992696 = yrday.fracday
Element set: 903
Inclination: 51.6442 deg
RA of node: 94.0612 deg
Eccentricity: .0011277
Arg of perigee: 357.5052 deg
Mean anomaly: 2.6054 deg
Mean motion: 15.76225556 rev/day Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 240
Checksum: 279
Coasting Arc #5 (Orbit 255)
Vector Time (GMT): 2010/055/11:29:16.873 Vector Time (MET): 016/02:15:09.892 Weight (LBS) : 209039.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2734061.36 A = 6720037.97 meter
Y = 4904224.15 meter E = .0016076
Z = 3672632.56 I = 51.98135
XDOT = -3566.170990 Wp = 50.41178
YDOT = -5262.383786 meter/sec RA = 88.38371 deg
ZDOT = 4369.759951 TA = 353.60188
MA = 353.62239
Ha = 189.583 n.mi
Hp = 178.878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8970017.60 X = -2806566.39
Y = 16089974.25 feet Y = 4873229.00 meter
Z = 12049319.44 Z = 3659174.80
XDOT = -11700.036056 XDOT = -3528.257911
YDOT = -17265.038669 feet/sec YDOT = -5302.071135 meter/sec
ZDOT = 14336.482779 ZDOT = 4352.527825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16523743.89 X = -5036437.14
Y = 8221693.58 feet Y = 2505972.20 meter
Z = 11996008.86 Z = 3656383.50
XDOT = 563.196885 XDOT = 171.662410
YDOT = -19698.023212 feet/sec YDOT = -6003.957475 meter/sec
ZDOT = 14267.878292 ZDOT = 4348.849304
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 10055.53433669 .00020000 00000-0 20000-3 0 9043
2 36394 51.6440 88.8347 0011337 2.9662 357.1568 15.76215928 2569
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10055.53433669 = yrday.fracday
Element set: 904
Inclination: 51.6440 deg
RA of node: 88.8347 deg
Eccentricity: .0011337
Arg of perigee: 2.9662 deg
Mean anomaly: 357.1568 deg
Mean motion: 15.76215928 rev/day Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 256
Checksum: 309
Coasting Arc #6 (Orbit 270)
Vector Time (GMT): 2010/056/11:33:53.726 Vector Time (MET): 017/02:19:46.745 Weight (LBS) : 209039.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2132259.83 A = 6724361.33 meter
Y = 6112566.39 meter E = .0018132
Z = -1782866.07 I = 51.99518
XDOT = -4133.226700 Wp = 18.76686
YDOT = 3101.289087 meter/sec RA = 83.19693 deg
ZDOT = 5722.260019 TA = 321.54121
MA = 321.67030
Ha = 189.559 n.mi
Hp = 178.612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6995603.12 X = 2072375.26
Y = 20054351.66 feet Y = 6136087.73 meter
Z = -5849298.12 Z = -1772653.22
XDOT = -13560.455051 XDOT = -4195.413017
YDOT = 10174.832963 feet/sec YDOT = 3054.697442 meter/sec
ZDOT = 18773.818959 ZDOT = 5702.030325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4692127.76 X = -1430160.54
Y = 20726178.11 feet Y = 6317339.09 meter
Z = -5808549.75 Z = -1770445.97
XDOT = -15475.766250 XDOT = -4717.013553
YDOT = 1705.118314 feet/sec YDOT = 519.720062 meter/sec
ZDOT = 18693.548331 ZDOT = 5697.793531
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 10056.48532878 .00020000 00000-0 20000-3 0 9051
2 36394 51.6449 83.9356 0011329 6.2889 353.8416 15.76267582 2718
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10056.48532878 = yrday.fracday
Element set: 905
Inclination: 51.6449 deg
RA of node: 83.9356 deg
Eccentricity: .0011329
Arg of perigee: 6.2889 deg
Mean anomaly: 353.8416 deg
Mean motion: 15.76267582 rev/day Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 271
Checksum: 326
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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