vibe coding an orbital mechanics simulation to try out claude code
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# Test Configuration: Sun + Parabolic Comet
# Comet with parabolic orbit (eccentricity = 1.0)
# Escape trajectory - total energy = 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
}
[[bodies]]
name = "ParabolicComet"
mass = 1.0e14
radius = 5.0e3
parent_index = 0
color = {r = 0.7,g = 0.8,b = 0.9 }
orbit = {
semi_latus_rectum = 2.992e11,
eccentricity = 1.0,
true_anomaly = 0.0
}