How to Calculate Eccentricity of Elliptical Orbit given Apogee and Perigee?
Eccentricity of Elliptical Orbit given Apogee and Perigee calculator uses Eccentricity of Elliptical Orbit = (Apogee Radius in Elliptic Orbit-Perigee Radius in Elliptic Orbit)/(Apogee Radius in Elliptic Orbit+Perigee Radius in Elliptic Orbit) to calculate the Eccentricity of Elliptical Orbit, Eccentricity of Elliptical Orbit given Apogee and Perigee formula is defined as a measure of how elliptical an orbit is, with higher values indicating a more elongated shape and lower values indicating a more circular shape, providing a way to describe the shape of an elliptical orbit in space. Eccentricity of Elliptical Orbit is denoted by ee symbol.
How to calculate Eccentricity of Elliptical Orbit given Apogee and Perigee using this online calculator? To use this online calculator for Eccentricity of Elliptical Orbit given Apogee and Perigee, enter Apogee Radius in Elliptic Orbit (re,apogee) & Perigee Radius in Elliptic Orbit (re,perigee) and hit the calculate button. Here is how the Eccentricity of Elliptical Orbit given Apogee and Perigee calculation can be explained with given input values -> 0.599976 = (27110000-6778000)/(27110000+6778000).