# Test Configuration: Elliptical Orbit for Analytical Propagation
# Moderate eccentricity to test propagation through apsides

[[bodies]]
name = "Earth"
mass = 5.972e24
radius = 6.371e6
parent_index = -1
color = { r = 0.0, g = 0.5, b = 1.0 }
orbit = {
    semi_major_axis = 0.0,
    eccentricity = 0.0,
    true_anomaly = 0.0
}

 [[spacecraft]]
name = "Elliptical_Orbit_Spacecraft"
mass = 1000.0
parent_index = 0
orbit = {
    semi_major_axis = 2.0e7,
    eccentricity = 0.6,
    true_anomaly = 0.0,
    inclination = 0.0,
    longitude_of_ascending_node = 0.0,
    argument_of_periapsis = 0.0
}