The correct answer is (d) 64:1
The best I can explain: The time periods (T) of a satellite revolving around the earth of radius R and at height h is:
T = 2 x pi x [(R + h)^3 / (G X M)]^1/2
Hence, the time period is directly proportional to (R + h)^3/2
The ratio of orbits is, therefore, 64:1.