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Determine the time it takes for a satellite to orbit the Mars in a circular near-Mars orbit. A near-Mars orbit is at a height above
Determine the time it takes for a satellite to orbit the Mars in a circular "near-Mars" orbit. A "near-Mars" orbit is at a height above the surface of the Mars that is very small compared to the radius of the Mars. [Hint: You may take the acceleration due to gravity as essentially the same as that on the surface.]
Does your result depend on the mass of the satellite?
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