vibe coding an orbital mechanics simulation to try out claude code
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# Test Configuration: Extreme Timescales for Analytical Propagation
[[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 }
[[bodies]]
name = "Sun"
mass = 1.989e30
radius = 6.96e8
parent_index = -1
color = { r = 1.0, g = 1.0, b = 0.0 }
orbit = { semi_major_axis = 0.0, eccentricity = 0.0, true_anomaly = 0.0 }
[[spacecraft]]
name = "Fast_Orbit_LEO"
mass = 1000.0
parent_index = 0
orbit = { semi_major_axis = 6.771e6, eccentricity = 0.0, true_anomaly = 0.0, inclination = 0.0, longitude_of_ascending_node = 0.0, argument_of_periapsis = 0.0 }
[[spacecraft]]
name = "Mercury_Like_Orbit"
mass = 1000.0
parent_index = 1
orbit = { semi_major_axis = 5.79e10, eccentricity = 0.2056, true_anomaly = 0.0, inclination = 0.0, longitude_of_ascending_node = 0.0, argument_of_periapsis = 0.0 }
[[spacecraft]]
name = "Long_Period_Orbit"
mass = 1000.0
parent_index = 1
orbit = { semi_major_axis = 5.2e11, eccentricity = 0.0489, true_anomaly = 0.0, inclination = 0.0, longitude_of_ascending_node = 0.0, argument_of_periapsis = 0.0 }
[[spacecraft]]
name = "Low_Altitude_Orbit"
mass = 1000.0
parent_index = 0
orbit = { semi_major_axis = 6.471e6, eccentricity = 0.0, true_anomaly = 0.0, inclination = 0.0, longitude_of_ascending_node = 0.0, argument_of_periapsis = 0.0 }
[[spacecraft]]
name = "Super_Synchronous_Orbit"
mass = 1000.0
parent_index = 0
orbit = { semi_major_axis = 4.5e7, eccentricity = 0.0, true_anomaly = 0.0, inclination = 0.0, longitude_of_ascending_node = 0.0, argument_of_periapsis = 0.0 }
[[spacecraft]]
name = "Geosynchronous_Orbit"
mass = 1000.0
parent_index = 0
orbit = { semi_major_axis = 4.2164e7, eccentricity = 0.0, true_anomaly = 0.0, inclination = 0.0, longitude_of_ascending_node = 0.0, argument_of_periapsis = 0.0 }