Specific Energy of Circular Orbit Given Orbital Radius evaluator uses Specific Energy of Orbit = -([GM.Earth])/(2*Orbit Radius) to evaluate the Specific Energy of Orbit, Specific Energy of Circular Orbit Given Orbital Radius formula is defined as a measure of the total energy per unit mass required to maintain a satellite in a circular orbit around the Earth, considering the gravitational attraction between the satellite and the Earth. Specific Energy of Orbit is denoted by ε symbol.
How to evaluate Specific Energy of Circular Orbit Given Orbital Radius using this online evaluator? To use this online evaluator for Specific Energy of Circular Orbit Given Orbital Radius, enter Orbit Radius (r) and hit the calculate button.