# Test Configuration: Extreme Orientation Mixed Cases
# Tests combined high inclination + high eccentricity orbital mechanics
# Tests singularity handling at Ω=0 and ω=0

[[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
}

# Test body 1: High inclination + high eccentricity
# i = 1.2 rad (68.8°), e = 0.85
[[spacecraft]]
name = "High_Inc_High_Ecc"
mass = 1000.0
parent_index = 0
orbit = {
    semi_major_axis = 5.0e7,
    eccentricity = 0.85,
    true_anomaly = 0.0,
    inclination = 1.2,
    longitude_of_ascending_node = 0.5,
    argument_of_periapsis = 0.3
}

# Test body 2: Very high inclination near polar + moderate eccentricity
# i = 1.4 rad (80°), e = 0.5
[[spacecraft]]
name = "Polar_Moderate_Ecc"
mass = 1000.0
parent_index = 0
orbit = {
    semi_major_axis = 2.0e7,
    eccentricity = 0.5,
    true_anomaly = 0.0,
    inclination = 1.4,
    longitude_of_ascending_node = 1.0,
    argument_of_periapsis = 0.5
}

# Test body 3: High eccentricity near parabolic with moderate inclination
# e = 0.99, i = 0.5 rad (28.6°)
[[spacecraft]]
name = "Near_Parabolic_Mod_Inc"
mass = 1000.0
parent_index = 0
orbit = {
    semi_major_axis = 7.0e8,
    eccentricity = 0.99,
    true_anomaly = 0.0,
    inclination = 0.5,
    longitude_of_ascending_node = 0.8,
    argument_of_periapsis = 1.2
}

# Test body 4: Edge case near Ω singularity (Ω = 0) with high inclination/eccentricity
[[spacecraft]]
name = "Omega_Zero"
mass = 1000.0
parent_index = 0
orbit = {
    semi_major_axis = 4.0e7,
    eccentricity = 0.8,
    true_anomaly = 0.0,
    inclination = 1.2,
    longitude_of_ascending_node = 0.0,
    argument_of_periapsis = 0.6
}

# Test body 5: Edge case near ω singularity (ω = 0) with high inclination/eccentricity
[[spacecraft]]
name = "Arg_Peri_Zero"
mass = 1000.0
parent_index = 0
orbit = {
    semi_major_axis = 4.0e7,
    eccentricity = 0.8,
    true_anomaly = 0.0,
    inclination = 1.2,
    longitude_of_ascending_node = 0.7,
    argument_of_periapsis = 0.0
}