Solving for satellite orbit period.

Note:

G is the universal gravitational constant

G = 6.6726 x 10^{-11}N-m^{2}/kg^{2}

satellite mean orbital radius (r) = 0 = 0 meter |

planet mass (M) = 0 = 0 kilogram |

satellite orbit period (T) = NOT CALCULATED |

Select an equation to solve for a different unknown

References - Books:

Tipler, Paul A.. 1995. Physics For Scientists and Engineers. Worth Publishers. 3rd ed.

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