A satellite is orbiting with areal velocity va. At what height from the surface of the earth, it is rotating, if the radius of earth is R?
4va2gR2−R
2va2gR2−R
va2gR2−R
3va2gR2−R
va=dAdt=12rv0=12rGMr⇒4va2=GMr=GM(R+h)⇒4va2=gR2(R+h) ⇒h=4va2gR2−R