1.

What will be velocity of a satellite revolving around the earth at a height h above surface of earth of radius is R

Answer»

the orbit to be circular. Takeradius of the EARTH as 6400 km and g at the surface of the earth to be 9.8 m/s2. ... Given: height of satellite above the surface of earth = h = 700 km, RADIUS of earth = R = 6400 km, G = 6.67 x 10-11 N m2/kg2 ; g = 9.8 m/s2.



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