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Media Share 9
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trjmkr.zip
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HOST.HED
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1992-08-09
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1KB
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39 lines
Units 1
Model_type 1
Vector option 1
Output_type 1
Orbital elements:
Semimajor axis 22809.000000
Eccentricity 0.330000
Inclination 63.440000
Asc. node longitude 90.000000
Argument of perigee 270.000000
Time past perigee 0.000000
ECI state vector:
X 6833.126531
Y 0.000000
Z -13669.265625
XD -0.000000
YD 2.336914
ZD 0.000000
True anomaly 0.000000
Mean anomaly 0.000000
Eccentric anomaly 0.000000
Energy -1.375557
Period 86403.590530
Kepler flight time 0.000000
Initial altitude 11847.350781
Lower altitude bound 11838.112610
Upper altitude bound 26903.599305
Ascending node rate -0.007505 deg/day
Argument of perigee rate -0.000003 deg/day
Date and time of injection:
Year 0 Month 0 Day 0
Hour 0 Minutes 0 Seconds 0
Mission duration time 86400.000000
Propagation increment 300.000000
Output frequency 300.000000
Map execution time 14 seconds
Execution time 21 seconds