A small satellite revolves around a planet in an orbit just above planet's surface. Taking the mean density of the planet `8000 kg m^(-3)` and `G = 6.67 xx 10^(-11) N //kg^(-2)`, find the time period of the satellite.

A small satellite revolves round a planet in an orbit just above planet's surface. Taking the mean density of planet 8000 kg m^-3 and g= 6.67 * 10^(-11) ,Nm^-2/kg^-2 ,.calculate the time period of the satellite.

A small satellite revolves round a planet in an orbit just above planet's surface. Taking the mean density of planet as rho , calculate the time period of the satellite.

A small satellite revolves round a planet in an orbit just above planet's surface. Taking the mean density of planet as rho , calculate the time period of the satellite.

A satellite revolves round a planet in an orbit just above the surface of planet. Taking G=6.67xx10^(-11) Nm^(2) kg^(-2) and the mean density of the planet =8.0xx10^(3) kg m^(-3) , find the period of satellite.

A satellite revolve round a planet in an orbit just above the surface of a planet. Taking G = 6.67 xx 10^(-11) Nm^(2) kg^(2) and mean density of the planet 5.51 xx 10^(3) kg//m^(3) find the period of the planet.

A satellite revolves around a planet of mean density 4.38 xx 10^(3)kg//m^(3) , in an orbit close to its surface. Calculate the time period of the satellite. Take, G = 6.67 xx 10^(-11) Nm^(2) kg^(-2) .

A small satellite revolves around a planet of average density 10 g*cm^(-3) . The radius of the orbit of the satellite is slightly more than the radius of the planet. Find the time period of rotation of the satellite. G=6.68xx10^(-8) CGS unit.

A satellite revolves in an orbit close to the surface of a planet of mean density 5.51 xx 10^(3) kg m^(-3) . Calculate the time period of satellite. Given G = 6.67 xx 10^(-11) Nm^(2) kg^(-2) .

An artificial satellite revolves around a planet in circular orbit close to its surface. Obtain the formula for period of the satellite in terms of density U and radius R of planet.

If the period of revolution of an artificial satellite just above the earth be T second and the density of earth be rho , kg//m^(3) then (G = 6.67 xx 10^(-11) m^(3)//kg . "second"^(2) )