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Q.

A satellite is revolving in a circular orbit round the earth at a height of h. If the acceleration due to gravity at that height is g. The orbital speed of the satellite.

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a

gh

b

gR

c

2gh

d

g(R+h)

answer is C.

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Detailed Solution

∴mV2r=mg

⇒V=gr=g(R+h)
 

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