Step-by-step explanation:
Lets consider
Circumference of orbit = T
as it is mentioned in the question that a satellite is in orbit that is very close to the surface of planet. so
circumference of orbit = circumference of planet
Time period = T
radius of planet = R
orbital velocity = V
gravitational constant = G
mass of planet = m
Solution:
Time period for a uniform circular motion of orbit is,
T =
where p = density
T = 2.17 hours = 7812 sec
(7812)² = [( 3×3.14)/6.67×
×ρ)]
ρ = 6.28/6.67×
×6.10×
ρ = 6.28/40.687×
ρ = 0.1543×
kg/m³
ρ = 15.43×
kg/m³