The mean radius of earth is R, its angular speed
on its own axis is w and the acceleration due to
gravity at earth's surface is g. What will be the
radius of the orbit of a geostationary satellite?
(a) (R²g /⍵² )¹/₃(b) (Rg / ⍵² )¹/₃
(c) (R²⍵² / g)¹/₃ (d) (R²g /⍵)¹/₃
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Answer:
Hey!
=> (Rg / ⍵² )¹/₃
hope it will be helpful ✌️
Thank you ❤️
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