How to Calculate Semimajor Axis of Elliptic Orbit given Apogee and Perigee Radii?
Semimajor Axis of Elliptic Orbit given Apogee and Perigee Radii calculator uses Semi Major Axis of Elliptic Orbit = (Apogee Radius in Elliptic Orbit+Perigee Radius in Elliptic Orbit)/2 to calculate the Semi Major Axis of Elliptic Orbit, The Semimajor Axis of Elliptic Orbit given Apogee and Perigee Radii can be defined using the apogee and perigee radii, which are the distances from the center of the central body to the farthest and closest points of the orbit, respectively, the semimajor axis represents half of the longest diameter of the ellipse and is computed as the average of the apogee and perigee radii. Semi Major Axis of Elliptic Orbit is denoted by ae symbol.
How to calculate Semimajor Axis of Elliptic Orbit given Apogee and Perigee Radii using this online calculator? To use this online calculator for Semimajor Axis of Elliptic Orbit given Apogee and Perigee Radii, enter Apogee Radius in Elliptic Orbit (re,apogee) & Perigee Radius in Elliptic Orbit (re,perigee) and hit the calculate button. Here is how the Semimajor Axis of Elliptic Orbit given Apogee and Perigee Radii calculation can be explained with given input values -> 16.944 = (27110000+6778000)/2.