The period of a satellite moving in circular orbit near the surface of a planet is independent of
A
mass of the planet
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B
radius of the planet
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C
mass of the satellite
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D
density of planet
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Solution
The correct option is B mass of the satellite Time period in terms of orbital speed is given by T=2πrvo=2πr√GMr=2π√r3GM From the above equation, we can see that T depends on radius of the orbit and the mass (density) of the planet but not the mass of the satellite.