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If v(0) be the orbital velocity of an ar...

If `v_(0)` be the orbital velocity of an articial satellite orbital velocity of the same satellite orbiting at an altitude equal to earth's radius is

A

`v_(0)sqrt((2)/(3))`

B

`v_(0)sqrt((3)/(2))`

C

`v_(0)sqrt(2)`

D

`(v_(0))/(sqrt(2))`

Text Solution

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The correct Answer is:
D
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