A stellite of mass m is orbiting the earth (of radius R) at a height h from its surface. The total energy of the stellite in terms of g0, value of acceleration due to gravity at the earth's surface, is
mg0R2/(R+h)
mg0R2/2(R+h)
-mg0R2/2(R+h)
2mg0R2/(R+h)
Solution:
Total energy of the satellite T = -GMm/2r where r = R + h ∴ T = -GMm/2(R+h) Acceleration due to gravity at earth's surface g0 = GM/R2 ⇒ GM = g0R2 ⇒ T = -mg0R2/2(R+h)