Orbital eccentricity describes how much an orbit deviates from a perfect circle. An eccentricity of 0 corresponds to a circular orbit, while values approaching 1 indicate increasingly elongated ellipses.
In a twoβbody system the shape of the orbit can be determined from the distances at the farthest (apoapsis, (r_a)) and nearest (periapsis, (r_p)) points to the primary body. These distances are directly measurable for satellites and planets, making them practical inputs for eccentricity calculations.
The relationship between apoapsis, periapsis, and eccentricity is given by a simple ratio. Knowing the eccentricity helps predict orbital speed variations, energy requirements for maneuvers, and the stability of the trajectory.
How do I calculate orbital eccentricity?
What does an eccentricity of 0 mean?
Can I use this calculator for planets too?
What happens if r_a equals r_p?
How does orbital eccentricity affect planetary motion?
Is there a maximum value for eccentricity?
Can this calculator help with satellite orbits too?
Results are for informational purposes only and do not constitute professional advice.
