Circular Orbit Period Using Only Radius

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Jul 24, 2020, 6:28:07 PM

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Nov 23, 2014, 2:51:39 AM

T = \frac{2 π r^{\frac{3}{2}}}{\sqrt{G m_{E}}}

$T = (2pi r ^(3/2))/sqrt(Gm_E)$

(r) Radius

$(r)"Radius"$

University Physics 12th Edition, Chapter 12, Equation #12.12

This equation, Circular Orbit Period Using Only Radius, references 2 pages

• G (Gravitational Constant) - metric by MichaelBartmess

• Mass_ Earth (Kg) by GerryPerham

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