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[" The orbital velocity of an artificial...

[" The orbital velocity of an artificial satellite in a circular orbit "],[" just above the earth's surface is "v." For a satellite orbiting at "],[" an altitude of half of the earth's radius,the orbital velocity is "],[" (A) "(3)/(2)v],[" (B) "sqrt((3)/(2))v],[" (C) "sqrt((2)/(3))v]

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