mv²/R=GmM/R ²
v= sqrt (GM/R) =…
T=2πR/v= …
Determine the time it takes for a satellite to orbit the Saturn in a circular "near-Saturn" orbit. A "near-Saturn" orbit is at a height above the surface of the Saturn that is very small compared to the radius of the Saturn. [Hint: You may take the acceleration due to gravity as essentially the same as that on the surface.]
2 answers
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2 answers