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MHT CET 2021 20th September Morning Shift
MCQ (Single Correct Answer)
+1
-0

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

A
$$\frac{3}{2}$$V
B
$$\sqrt{\frac{3}{2}}$$V
C
$$\sqrt{\frac{2}{3}}$$V
D
$$\frac{2}{3}$$V
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