write an expression for angular momentum of a sattilite
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We are asked about the angular momentum of the satellite with respect to the centre of earth. We know that the equation for angular momentum is given by, →L=r×→p, where 'L' is angular momentum, 'r' is radius and 'p' is momentum.
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This is ur correct answer . l have read it in a book
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L= r × p
In circular orbit,
r× p
=rp=mvr
∴L=m GMr or, L∝ r
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