Answer:
[tex]12548.5 kgm^{-3}[/tex]
Explanation:
Complete statement of the question is
An artificial satellite is in a circular orbit d = 310 km above the surface of a planet of radius r = 2050 km. The period of revolution of the satellite around the planet is T = 1.15 hours. What is the average density of the planet?
[tex]r[/tex] = radius of the planet = 2050 km = 2.05 x 10⁶ m
[tex]d[/tex] = distance of the satellite above the surface of planet = 310 km = 0.310 x 10⁶ m
[tex]R[/tex] = radius of the orbit = [tex]r + d[/tex] = [tex]2.05\times10^{6} + 0.31\times10^{6} = 2.36\times10^{6} m[/tex]
[tex]M[/tex] = mass of the planet
[tex]T[/tex] = Time period of the planet = 1.15 h = 1.15 x 3600 = 4140 s
Using Kepler's third law
[tex]T^{2} = \frac{4\pi^{2} R^{3} }{GM} \\4140^{2} = \frac{4(3.14)^{2} (2.36\times10^{6})^{3} }{(6.67\times10^{-11})M}\\M = 4.53\times10^{23} kg[/tex]
Volume of the planet is given as
[tex]V = \frac{4\pi r^{3} }{3} \\V = \frac{4(3.14) (2.05\times10^{6})^{3} }{3}\\V = 3.61\times10^{19} m^{3}[/tex]
Average density of the planet is given as
[tex]\rho = \frac{M}{V} \\\rho = \frac{4.53\times10^{23}}{3.61\times10^{19}}\\\rho = 12548.5 kgm^{-3}[/tex]