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
------------------------------------------------------------------------
041/00:56:42.981 14.3 21.0 21.0
001/15:42:36.000 6.9 -0.0 187.1
000/00:00:15.922 -13.8 0.0 176.6
041/01:30:43.425 0.2 -0.2 0.2
001/16:16:36.445 -0.0 0.0 187.1
000/00:00:00.889 -0.0 -0.0 176.6
041/02:28:31.490 5.5 8.1 8.2
001/17:14:24.509 3.9 -1.2 187.2
000/00:00:13.019 -4.8 0.2 181.3
041/03:45:25.641 2.4 2.5 3.1
001/18:31:18.660 -0.4 0.8 187.7
000/00:00:13.320 -1.8 1.5 182.3
Coasting Arc #1 (Orbit 19)
---------------------------------------
Vector Time (GMT): 2010/040/12:31:30.000
Vector Time (MET): 001/03:17:23.019
Weight (LBS) : 247423.6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2395419.26 A = 6698360.15 meter
Y = -3570482.40 meter E = .0031361
Z = 5149557.70 I = 51.71114
XDOT = 7018.141574 Wp = 318.85394
YDOT = -2905.078772 meter/sec RA = 165.14585 deg
ZDOT = 1277.909129 TA = 119.10013
MA = 118.78577
Ha = 186.666 n.mi
Hp = 164.819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7858987.09 X = -2380309.98
Y = -11714181.10 feet Y = -3597198.81 meter
Z = 16894874.35 Z = 5137957.53
XDOT = 23025.398866 XDOT = 7043.913464
YDOT = -9531.098332 feet/sec YDOT = -2826.413735 meter/sec
ZDOT = 4192.615254 ZDOT = 1312.064816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -194859.54 X = -59393.19
Y = -14160001.63 feet Y = -4315968.50 meter
Z = 16848705.58 Z = 5135485.46
XDOT = 23415.635026 XDOT = 7137.085556
YDOT = 4719.805350 feet/sec YDOT = 1438.596671 meter/sec
ZDOT = 4328.024997 ZDOT = 1319.182019
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 10040.57147101 .00020000 00000-0 20000-3 0 9000
2 36394 51.6455 165.9047 0035529 317.0959 42.7437 15.81857978 201
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10040.57147101 = yrday.fracday
Element set: 900
Inclination: 51.6455 deg
RA of node: 165.9047 deg
Eccentricity: .0035529
Arg of perigee: 317.0959 deg
Mean anomaly: 42.7437 deg
Mean motion: 15.81857978 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 20
Checksum: 298
Coasting Arc #2 (Orbit 27)
---------------------------------------
Vector Time (GMT): 2010/041/00:56:50.942
Vector Time (MET): 001/15:42:43.961
Weight (LBS) : 246909.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4708644.35 A = 6717419.98 meter
Y = -3855494.36 meter E = .0011610
Z = 2859801.98 I = 51.75245
XDOT = 5185.049318 Wp = 357.05024
YDOT = 2557.522677 meter/sec RA = 162.43059 deg
ZDOT = -5078.713828 TA = 150.16069
MA = 150.09444
Ha = 187.139 n.mi
Hp = 176.561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15448308.23 X = 4737536.82
Y = -12649259.73 feet Y = -3802651.26 meter
Z = 9382552.42 Z = 2882745.91
XDOT = 17011.316660 XDOT = 5180.721204
YDOT = 8390.822431 feet/sec YDOT = 2615.510536 meter/sec
ZDOT = -16662.446942 ZDOT = -5053.535917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19423934.97 X = -5920415.38
Y = 4432933.51 feet Y = 1351158.13 meter
Z = 9473443.91 Z = 2887505.70
XDOT = -11229.617361 XDOT = -3422.787372
YDOT = -13737.618949 feet/sec YDOT = -4187.226256 meter/sec
ZDOT = -16562.436912 ZDOT = -5048.230771
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 10041.07698522 .00020000 00000-0 20000-3 0 9015
2 36394 51.6447 163.2845 0019472 314.2417 45.7150 15.77917004 281
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10041.07698522 = yrday.fracday
Element set: 901
Inclination: 51.6447 deg
RA of node: 163.2845 deg
Eccentricity: .0019472
Arg of perigee: 314.2417 deg
Mean anomaly: 45.7150 deg
Mean motion: 15.77917004 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 28
Checksum: 283
Coasting Arc #3 (Orbit 27)
---------------------------------------
Vector Time (GMT): 2010/041/01:30:43.870
Vector Time (MET): 001/16:16:36.889
Weight (LBS) : 246903.6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 44507.54 A = 6709231.75 meter
Y = 4270023.10 meter E = .0011448
Z = -5173488.19 I = 51.72621
XDOT = -7486.661687 Wp = 3.18246
YDOT = 1443.346049 meter/sec RA = 162.32349 deg
ZDOT = 1138.222280 TA = 277.59286
MA = 277.72288
Ha = 187.088 n.mi
Hp = 176.578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 146022.10 X = 21862.96
Y = 14009262.13 feet Y = 4270394.67 meter
Z = -16973386.46 Z = -5173326.75
XDOT = -24562.538343 XDOT = -7507.781876
YDOT = 4735.387301 feet/sec YDOT = 1359.464960 meter/sec
ZDOT = 3734.325066 ZDOT = 1101.801852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4109729.58 X = 1252645.58
Y = -13394713.69 feet Y = -4082708.73 meter
Z = -16972576.81 Z = -5173241.41
XDOT = 23864.053886 XDOT = 7273.763624
YDOT = 2820.302360 feet/sec YDOT = 859.628159 meter/sec
ZDOT = 3589.861463 ZDOT = 1094.189774
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 10041.07698533 .00020000 00000-0 20000-3 0 9028
2 36394 51.6452 163.2844 0019314 314.5621 45.3967 15.77953453 281
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10041.07698533 = yrday.fracday
Element set: 902
Inclination: 51.6452 deg
RA of node: 163.2844 deg
Eccentricity: .0019314
Arg of perigee: 314.5621 deg
Mean anomaly: 45.3967 deg
Mean motion: 15.77953453 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 28
Checksum: 296
Coasting Arc #4 (Orbit 28)
---------------------------------------
Vector Time (GMT): 2010/041/02:28:38.000
Vector Time (MET): 001/17:14:31.019
Weight (LBS) : 246702.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4866106.14 A = 6722117.03 meter
Y = -3789686.40 meter E = .0006088
Z = 2678319.05 I = 51.75395
XDOT = 4980.344796 Wp = 29.81331
YDOT = 2706.393622 meter/sec RA = 162.10497 deg
ZDOT = -5208.910684 TA = 119.71093
MA = 119.65032
Ha = 187.216 n.mi
Hp = 181.267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15964915.15 X = 4895132.24
Y = -12433354.32 feet Y = -3735080.80 meter
Z = 8787135.99 Z = 2702028.24
XDOT = 16339.713898 XDOT = 4974.998811
YDOT = 8879.244167 feet/sec YDOT = 2762.085498 meter/sec
ZDOT = -17089.601982 ZDOT = -5184.729672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16651673.64 X = -5075430.13
Y = 11424928.05 feet Y = 3482318.07 meter
Z = 8881067.40 Z = 2706949.34
XDOT = -15025.959415 XDOT = -4579.912430
YDOT = -8664.552446 feet/sec YDOT = -2640.955586 meter/sec
ZDOT = -16993.541068 ZDOT = -5179.631317
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 10041.14035887 .00020000 00000-0 20000-3 0 9034
2 36394 51.6429 162.9598 0013108 307.5740 52.4233 15.76417169 290
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10041.14035887 = yrday.fracday
Element set: 903
Inclination: 51.6429 deg
RA of node: 162.9598 deg
Eccentricity: .0013108
Arg of perigee: 307.5740 deg
Mean anomaly: 52.4233 deg
Mean motion: 15.76417169 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 29
Checksum: 291
Coasting Arc #5 (Orbit 29)
---------------------------------------
Vector Time (GMT): 2010/041/03:45:32.301
Vector Time (MET): 001/18:31:25.320
Weight (LBS) : 246615.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -974774.83 A = 6714461.13 meter
Y = -4054609.82 meter E = .0010034
Z = 5268063.73 I = 51.72653
XDOT = 7381.087163 Wp = 322.51708
YDOT = -2172.080247 meter/sec RA = 161.84804 deg
ZDOT = -298.488644 TA = 130.35712
MA = 130.26946
Ha = 187.653 n.mi
Hp = 182.320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3198080.15 X = -954930.48
Y = -13302525.64 feet Y = -4065405.14 meter
Z = 17283673.65 Z = 5263376.38
XDOT = 24216.165234 XDOT = 7406.289023
YDOT = -7126.247529 feet/sec YDOT = -2089.357568 meter/sec
ZDOT = -979.293452 ZDOT = -262.571217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6782711.06 X = 2067370.33
Y = 11909151.62 feet Y = 3629909.41 meter
Z = 17264912.92 Z = 5262345.46
XDOT = -20513.484699 XDOT = -6252.510136
YDOT = 12932.180565 feet/sec YDOT = 3941.728636 meter/sec
ZDOT = -836.853039 ZDOT = -255.072806
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 10041.20376499 .00020000 00000-0 20000-3 0 9049
2 36394 51.6440 162.6306 0011323 310.9490 49.0694 15.75988662 309
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10041.20376499 = yrday.fracday
Element set: 904
Inclination: 51.6440 deg
RA of node: 162.6306 deg
Eccentricity: .0011323
Arg of perigee: 310.9490 deg
Mean anomaly: 49.0694 deg
Mean motion: 15.75988662 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 30
Checksum: 285
Coasting Arc #6 (Orbit 45)
---------------------------------------
Vector Time (GMT): 2010/042/03:50:13.702
Vector Time (MET): 002/18:36:06.721
Weight (LBS) : 246615.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6200965.81 A = 6723872.01 meter
Y = 501996.32 meter E = .0012799
Z = 2528047.54 I = 51.78641
XDOT = 1737.533832 Wp = 25.24929
YDOT = -5305.125849 meter/sec RA = 156.71321 deg
ZDOT = 5316.926405 TA = 3.37969
MA = 3.37105
Ha = 188.045 n.mi
Hp = 182.029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20344376.02 X = -6218401.24
Y = 1646969.55 feet Y = 432520.53 meter
Z = 8294119.22 Z = 2497881.83
XDOT = 5700.570314 XDOT = 1770.929736
YDOT = -17405.268532 feet/sec YDOT = -5285.499213 meter/sec
ZDOT = 17443.984270 ZDOT = 5325.448002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18900237.25 X = 5760792.31
Y = -7833161.01 feet Y = -2387547.48 meter
Z = 8174422.21 Z = 2491563.89
XDOT = -550.781489 XDOT = -167.878198
YDOT = 16904.711004 feet/sec YDOT = 5152.555914 meter/sec
ZDOT = 17477.591950 ZDOT = 5327.170026
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 10042.21832701 .00020000 00000-0 20000-3 0 9055
2 36394 51.6440 157.4050 0011448 315.5826 44.4419 15.75971278 465
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10042.21832701 = yrday.fracday
Element set: 905
Inclination: 51.6440 deg
RA of node: 157.4050 deg
Eccentricity: .0011448
Arg of perigee: 315.5826 deg
Mean anomaly: 44.4419 deg
Mean motion: 15.75971278 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 46
Checksum: 277
Coasting Arc #7 (Orbit 60)
---------------------------------------
Vector Time (GMT): 2010/043/03:54:33.157
Vector Time (MET): 003/18:40:26.177
Weight (LBS) : 246615.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3519993.91 A = 6722031.15 meter
Y = 4755021.72 meter E = .0009896
Z = -3178153.77 I = 51.80805
XDOT = -5892.622263 Wp = 342.12468
YDOT = -1132.213194 meter/sec RA = 151.51110 deg
ZDOT = 4837.740008 TA = 340.85283
MA = 340.89000
Ha = 188.076 n.mi
Hp = 181.746
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11548536.45 X = -3557492.21
Y = 15600464.96 feet Y = 4715429.33 meter
Z = -10427013.68 Z = -3195344.35
XDOT = -19332.750208 XDOT = -5903.017013
YDOT = -3714.610215 feet/sec YDOT = -1198.199757 meter/sec
ZDOT = 15871.850421 ZDOT = 4809.089283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5470671.33 X = 1667460.62
Y = -18584709.54 feet Y = -5664619.47 meter
Z = -10495053.20 Z = -3198892.22
XDOT = 18171.295954 XDOT = 5538.611007
YDOT = -3540.120304 feet/sec YDOT = -1079.028669 meter/sec
ZDOT = 15758.088101 ZDOT = 4803.065253
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 10043.16946607 .00020000 00000-0 20000-3 0 9062
2 36394 51.6440 152.5064 0011574 318.6853 41.3435 15.75996520 618
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10043.16946607 = yrday.fracday
Element set: 906
Inclination: 51.6440 deg
RA of node: 152.5064 deg
Eccentricity: .0011574
Arg of perigee: 318.6853 deg
Mean anomaly: 41.3435 deg
Mean motion: 15.75996520 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 61
Checksum: 287
|
