To solve this problem, we need to understand the relationship between the time period of a satellite and its distance from the Earth. The time period of a satellite in circular orbit around the Earth is given by Kepler's Third Law:
T^2 = \frac{4\pi^2}{GM}a^3
Where:
Given that the satellite initially has a time period of 24 hours, we need to find the new time period when the distance is reduced to one fourth of its original value.
Let the initial distance be a and the initial time period be T = 24 hours. We use the formula:
T_1^2 \propto a^3
When the distance becomes \frac{a}{4}, the new time period T_2 is given by:
T_2^2 \propto \left(\frac{a}{4}\right)^3 = \frac{a^3}{64}
The ratio of the squares of the time periods is:
\frac{T_2^2}{T_1^2} = \frac{\left(\frac{a}{4}\right)^3}{a^3} = \frac{1}{64}
Solving for T_2, we have:
T_2 = T_1 \times \frac{1}{8}
Substitute T_1 = 24 hours:
T_2 = 24 \times \frac{1}{8} = 3 hours
Therefore, the new time period of the satellite is 3 hours, which matches the given correct answer.