The orbital angular momentum of a satellite revolving at a distance \( r \) from the centre is \...
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The orbital angular momentum of a satellite revolving at a distance \( r \) from the centre is \( L \). If the distance is increased to \( 16 r \), then the new angular momentum will be
(a) \( 16 L \)
(b) \( 64 L \)
(c) \( \frac{L}{4} \)
(d) \( 4 L \)
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