Short Answer

Orbital Equation Parameters

A satellite trajectory analyst is deriving the standard equation for a horizontal elliptical orbit centered at the origin, which is written in the form x2a2+y2b2=1\frac{x^2}{a^2} + \frac{y^2}{b^2} = 1. What is the specific mathematical formula the analyst must use to calculate the value of the denominator b2b^2 when the semi-major axis aa and the focal distance cc are known?

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Updated 2026-05-22

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