Semi-Major Axis using $μ & P$ $mu & P$

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on

Jul 24, 2020, 6:28:07 PM

Created by

on

Jul 11, 2014, 10:42:41 AM

a = {({(\frac{P}{2 π})}^{2} \cdot μ)}^{\frac{1}{3}}

$a = (( "P" /(2 pi))^2*mu)^(1/3)$

Orbit Period

$"Orbit Period"$

Notes

The semi-major axis, $a$ $a$ , is the distance between the ellipse center and the apogee point.

This equation, Semi-Major Axis using

μ & P

$mu & P$ , references 2 pages

•

π

$pi$ by MichaelBartmess

• Earth Gravitational Constant (

μ

$mu$ ) :

m^{3}

$m^3$ /

\sec^{2}

$sec^2$ by MichaelBartmess

This equation, Semi-Major Axis using

μ & P

$mu & P$ , is used in 0 pages

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SemiMajorAxisusingmuP-illustration.png

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