example_LEO_sim_extreme.cfg

#Config file generated by SatGen V. 0.0.1.1
#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 = CONSTANT
Constant Drag Coef = 2.1
Name = Example
Edge Length = 0.1

[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) = 6628 km
e (Eccentricity) = 0.001
I (Inclination) = 95.00 deg
RAAN (Right Ascension of Ascending Node) = 0.0 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