Perigee Radius of Hyperbolic Orbit given Angular Momentum and Eccentricity evaluator uses Perigee Radius = Angular Momentum of Hyperbolic Orbit^2/([GM.Earth]*(1+Eccentricity of Hyperbolic Orbit)) to evaluate the Perigee Radius, The Perigee Radius of Hyperbolic Orbit given Angular Momentum and Eccentricity formula is defined as the distance from the center of the central body to the closest point of the hyperbolic orbit, this formula allows for the calculation of the perigee radius based on two critical parameters: angular momentum and eccentricity. Perigee Radius is denoted by rperigee symbol.
How to evaluate Perigee Radius of Hyperbolic Orbit given Angular Momentum and Eccentricity using this online evaluator? To use this online evaluator for Perigee Radius of Hyperbolic Orbit given Angular Momentum and Eccentricity, enter Angular Momentum of Hyperbolic Orbit (hh) & Eccentricity of Hyperbolic Orbit (eh) and hit the calculate button.