An artificial satellite is in a circular orbit around a planet of radius r = 2.25 × 103 km at a distance d = 380.0 km from the planet\'s surface. The period of revolution of the satellite around the planet is T = 1.15 hours. What is the average density of the planet?
given r= 2.25 x 10³ km
Using Orbital Period Equation
T²/R³ = (4 x П²)/ (G x Mcentral)
|Where,
T = period of the satellite
Mcentral = mass of the central body about which the satellite
orbits
G = Gravitational constant ( which equals 6.673 x 10-¹¹
N m2/kg2 )
П = 3.14
Given that
T = 1.15 hours = 4140 seconds
R = ( Radius of planet + distance of satellite from planet's
surface)
= ( 2.25 x 10³) + 380
= 2630 km
= 2630000 meters
Mcentral = (4 x П² x R³)/ (G x T²)
= [4 x (3.14)² x (2630000)³ ] / [ 6.673×10¯¹¹ x (4140)² ]
= 6.273 x 10²³ kg
Volume of planet(V) = 4/3 x П x R³
.'. V = 4/3 x 3.14 x (2630000)³
= 7.616 x 10¹⁹ metre³
Hence, average density of planet = Mass/volume
= Mcentral/ Volume
= (6.273 x 10²³ kg) / (7.616 x 10¹⁹ metre³)
= 8236.607 Kg/m³
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