Package org.episteme.natural.physics.astronomy.mechanics
package org.episteme.natural.physics.astronomy.mechanics
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ClassesClassDescriptionLow-precision planetary ephemeris calculator.Solar system body declaration with orbital elements at J2000.Solver for Lambert's problem: finding the orbit between two points in space for a given duration.Orbital mechanics calculations.Calculations for Keplerian Orbits.Orbital maneuvers and transfer orbits.