Three-Body Integrator &
Lagrange Point Explorer

Integration Parameters:

Accuracy: of Integration
Integration Time: Orbital Periods and Output Interval: Days

2 Bodies in Bound Orbit:

Mass of the Sun: and Planet: in Solar Masses
Sun to Planet Distance: AU and Eccentricity:

3rd Body (of Infinitesimal Mass):

Location: 3rd Body is near
Displacement from Location and Velocity in Rotating Frame:
x: AU
Vx: km/s
y: AU
Vy: km/s
z: AU
Vz: km/s

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Three-Body Integrator and Lagrange Point Explorer written by Heather Cohen and Dr. Douglas P. Hamilton