Specific Energy of Elliptic Orbit given Semi Major Axis evaluator uses Specific Energy of Elliptical Orbit = -[GM.Earth]/(2*Semi Major Axis of Elliptic Orbit) to evaluate the Specific Energy of Elliptical Orbit, Specific Energy of Elliptic Orbit given Semi Major Axis formula is defined as a measure of the total energy of an object in an elliptical orbit around a celestial body, which is a critical parameter in understanding the motion of objects in space. Specific Energy of Elliptical Orbit is denoted by εe symbol.
How to evaluate Specific Energy of Elliptic Orbit given Semi Major Axis using this online evaluator? To use this online evaluator for Specific Energy of Elliptic Orbit given Semi Major Axis, enter Semi Major Axis of Elliptic Orbit (ae) and hit the calculate button.