Specific Energy of Circular Orbit evaluator uses Specific Energy of Orbit = -([GM.Earth]^2)/(2*Angular Momentum of Circular Orbit^2) to evaluate the Specific Energy of Orbit, Specific Energy of Circular Orbit formula is defined as the total energy per unit mass required to maintain a satellite in a circular orbit around the Earth, which is a critical parameter in space mission design and orbit determination. Specific Energy of Orbit is denoted by ε symbol.
How to evaluate Specific Energy of Circular Orbit using this online evaluator? To use this online evaluator for Specific Energy of Circular Orbit, enter Angular Momentum of Circular Orbit (hc) and hit the calculate button.