1.

A satellite of mass m orbits around the Earth of mas M in an elliptical orbit of semi - major and semi - minor axes 2a and a respectively. The angular momentum of the satellite about the centre of the Earth is

Answer»

`pimsqrt((GMA)/(4))`
`pim sqrt((GMa)/(4))`
`msqrt((GM a)/(8))`
`msqrt((GM a)/(2))`

Answer :D


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