Physics, asked by Anonymous, 1 year ago

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The orbital velocity of an artificial satellite in a circular orbit just above the centre’s surface is v.
For a satellite orbiting at an altitude of half of the earth’s radius, find the orbital velocity .

OPTIONS :
(a) 3 v / 2
(b) √(3 /2 )v
(c) 2 v / 3
(d) √(2/3) v

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Answers

Answered by Anonymous
5
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Answered by TEJ1234576
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