To determine the time period of rotation of the satellite, we will use Kepler's Third Law, which states that the square of the period of any planet (or satellite) is proportional to the cube of the semi-major axis of its orbit.
Mathematically, for two bodies orbiting the same celestial body, the law is expressed as:
\(\frac{T_1^2}{R_1^3} = \frac{T_2^2}{R_2^3}\)
Where:
According to the question:
Substituting into Kepler's Third Law:
\(\frac{T_1^2}{R_1^3} = \frac{T_2^2}{(R_1/9)^3}\)
Solving for \(T_2\):
\(\frac{27^2}{R_1^3} = \frac{T_2^2}{R_1^3/729}\)
\(T_2^2 = 27^2 \times 729\)
\(T_2^2 = 27^2 \times 27^2\)
\(T_2 = 27/9\)
\(T_2 = 1\) day
Thus, the time period of rotation of the satellite is 1 day.
Hence, the correct answer is 1 day.
A black body is at a temperature of 2880 K. The energy of radiation emitted by this body with wavelength between 499 nm and 500 nm is U1, between 999 nm and 1000 nm is U2 and between 1499 nm and 1500 nm is U3. The Wien's constant, b = 2.88×106 nm-K. Then,

What will be the equilibrium constant of the given reaction carried out in a \(5 \,L\) vessel and having equilibrium amounts of \(A_2\) and \(A\) as \(0.5\) mole and \(2 \times 10^{-6}\) mole respectively?
The reaction : \(A_2 \rightleftharpoons 2A\)