The speed of near satellite is V. its orbital speed, when its altitude is increased by half of earth's radius is
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A “satellite orbiting” at an altitude at “half of the earth’s radius” is
Explanation:
The orbital velocity at height h above the earth surface is,
Orbital velocity just above the earth surface is (V)
Orbital velocity at height of half of earth radius
Where,
Orbiting at an altitude at “half of the earth’s radius” is,
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