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, The Eccentricity of Elliptical Orbit given Apogee and Perigee formula is defined as mathematical expression used to determine the degree of elongation or deviation from a perfect circle in the path of a celestial body or satellite, this formula calculates eccentricity by taking into account the distances of the apogee and the perigee from the center of the central body, such as Earth. 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).