Discover The Simple Steps To Determine The Semi-Major Axis Of An Elliptical Orbit
To find the semi-major axis (a) of an elliptical orbit, use the following steps: 1) Determine the mean distance between the orbiting body and the focus of the ellipse and apply Kepler’s third law to calculate the orbital period (T). 2) Utilize the equation a³ = GM(T²/4π²) to derive the semi-major axis, where G is…