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A satelite revolving in a circular equat...

A satelite revolving in a circular equatorial orbit from west to east appears over a certain point on the equator every 8 hours therefore it's period is

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A satellite revolving in a circular equatorial orbit of radius R = 2xx10^(4) km from west to east appears over a certain point at the equator every t = 11.6 hours. Calculate the mass of the earth. The gravitational contant G= 6.67 xx 10^(-11) SI units. [Hint : omega_(app) =omega_("earth") or omega_("real") = 2pi ((1)/(T)+(1)/(t)) ]

A satellite revolving in a circular equatorial orbit of radius R = 2.0 xx 10^(4) km from west to east appears over a certain point at the equator every 11.6 h . From these data, calculate the mass of the earth. (G = 6.67 xx 10^(-11) N m^(2))

A satellite revolving in a circular equatorial orbit of radius R = 2.0 xx 10^(4) km from west to east appears over a certain point at the equator every 11.6 h . From these data, calculate the mass of the earth. (G = 6.67 xx 10^(-11) N m^(2))

A satellite is revolving in the circular equatorial orbit of radius R=2xx10^(4)km from east to west. Calculate the interval after which it will appear at the same equatorial town. Given that the radius of the earth =6400km and g (acceleration due to gravity) =10ms^(-2)

A satellite is revolving in the circular equatorial orbit of radius R=2xx10^(4)km from east to west. Calculate the interval after which it will appear at the same equatorial town. Given that the radius of the earth =6400km and g (acceleration due to gravity) =10ms^(-2)

A satelite is revolving in a circular orbit at a height h above the surface of the earth of radius R. The speed of the satellite in its orbit is one-fourth the escape velocity from the surface of the earth. The relation between h and R is

A satelite is revolving in a circular orbit at a height h above the surface of the earth of radius R. The speed of the satellite in its orbit is one-fourth the escape velocity from the surface of the earth. The relation between h and R is

A satelite is revolving in a circular orbit at a height h above the surface of the earth of radius R. The speed of the satellite in its orbit is one-fourth the escape velocity from the surface of the earth. The relation between h and R is

A spy satellite S_(1), travelling above the equator is taking pictures at quick intervals. The satellite is travelling from west to east and is ready with picture around the whole equator in 8 hours. Another similar satellite S_(2), travelling in the same plane is travelling from east to west and is able to take pictures around the whole equator in 6 hours. Find the ratio of radii of the circular paths of the satellite S_(1) and S_(2).