vibe coding an orbital mechanics simulation to try out claude code
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[[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
}
[[bodies]]
name = "Earth"
mass = 5.972e24
radius = 6.371e6
parent_index = 0
color = { r = 0.0, g = 0.5, b = 1.0 }
orbit = {
semi_major_axis = 1.496e11,
eccentricity = 0.0,
true_anomaly = 0.0
}
[[bodies]]
name = "Mars"
mass = 6.39e23
radius = 3.3895e6
parent_index = 0
color = { r = 0.8, g = 0.3, b = 0.1 }
orbit = {
semi_major_axis = 2.279e11,
eccentricity = 0.0,
true_anomaly = 0.0
}
[[bodies]]
name = "Spacecraft"
mass = 1.0
radius = 1000.0
# Position at LEO altitude: Earth position + (Earth radius + 200km altitude)
# Earth: 1.496e11, LEO offset: 6.571e6, Total: 1.49606571e11
parent_index = 1
color = { r = 1.0, g = 0.0, b = 0.5 }
orbit = {
# Semi-major axis: Earth radius + 200km LEO altitude
semi_major_axis = 6.571e6,
eccentricity = 0.0,
true_anomaly = 0.0
}