example_LEO_sim.txt

#CNES - STELA VERSION: 2.5.1
#LEO Simulation Report 
[ General ]
 Model : GTO
 Author : CNES
 Comment : LEO example simulation
 Simulation duration : 100.0 years
 Ephemeris step : 86400.0 s
 Difference between terrestrial and universal time : 67.184 s
 Integration Step : 86400.0 s
 Atmospheric drag switch : true
 Drag quadrature Points : 33
 Atmospheric Drag Recompute step : 1 steps
 Solar radiation pressure switch : true
 Solar radiation pressure quadrature Points : 11
 Sun switch : true
 Moon switch : true
 Zonal order : 7
 Earth Tesseral switch : false
 Reentry Altitude : 120.0 km
 Tesseral Min Period : 5
 Warning Flag : false
 Iterative Mode : false
 
[ Space Object ]
 Mass : 1470.0 kg
 Drag Area : 15.0 m^2
 Reflecting Area : 15.0 m^2
 Reflectivity Coefficient : 1.5
 Orbit Type : LEO
 Drag Coefficent Type : VARIABLE
 Name : EXAMPLE space object
 
[ Atmospheric Model ]
 Atmospheric model : NRLMSISE-00

[ Solar Activity ]
 Solar Activity Type : VARIABLE
 
[ Initial Bulletin ]
 Date : 2009-07-29T00:00:00.000
 Type : Keplerian
 Frame : CELESTIAL_MEAN_OF_DATE
 Nature : MEAN
 a (Semi major axis) : 7062.5 km
 e (Eccentricity) : 0.0159292035
 I (Inclination) : 98.59 deg
 RAAN (Right Ascension of Ascending Node) : 277.51331 deg
 w (Argument of perigee) : 0.0 deg
 M (Mean anomaly) : 0.0 deg
 
[Iteration Data]
Function Value Accuracy : 10 years
Simulation Minus Expiring Duration : 75.25
Iteration Method : FrozenOrbit
Expiring Duration : 24.75