Correct answer: 12 √2 h
The time period of a satellite is proportional to the square root of the cube of its orbital radius (T ∝ R^(3/2)). For the geostationary satellite, the orbital radius is 7R (6R + R). For the second satellite, the orbital radius is 3.5R (2.5R + R). Using the ratio of time periods, T2/T1 = (R2/R1)^(3/2), we find T2 = 12√2 h.