A satellite of mass m is moving in a circular orbit of radius r.
Calculate its angular momentum with respect to the centre of the orbit in terms of the mass of earth???.
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mass= m
velocity=v
radius=r
IT IS SAID THAT THE CENTRE OF THE ORBIT IS THE TERM OF THE MASS OF THE EARTH
Radius of the earth = 6.4×10^6m
Mass of the earth = 6× 10^24KG
angular momentum (L) = Mass × Velocity ×Radius
= M×V×R
=6×10^24×V ×6.4×10^6
=384×10^29×V
(10^29=1000000000000000000000000000000)
THEREFORE THE THE ANGULAR MASS OF THE SATELLITE IS 384×10^29×V kg/metre
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