WebA satellite is in a circular orbit around the Earth at an altitude of 1.98 × 1 0 6 m. (a) Find the period of the orbit. (Hint: Modify Kepler's third law so it is suitable for objects orbiting the Earth rather than the Sun. The radius of the Earth is 6.38 × 1 0 6 m, and the mass of the Earth is. 5.98 × 1 0 24 kg.) h (b) Find the speed of the ... WebAccording to Kepler’sthird law, the orbital period of satellite is directly related to radius of orbit as: T ∝ r 3 2. Where, T = Orbital period of the satellite r = Orbital radius. As the …
Speed of satellite and its period: Numerical problems - The Fact …
WebA satellite is in a circular orbit around the Earth at an altitude of 1.98 × 1 0 6 m. (a) Find the period of the orbit. (Hint: Modify Kepler's third law so it is suitable for objects orbiting the … WebPhysics. Physics questions and answers. A) A satellite is placed in a circular orbit around the Earth at an altitude of 1,200 km. Calculate the satellite's orbital period, in hours. B) A … setting up powerchute
The time period of an artificial satellite in a circular orbit is ...
WebApr 7, 2024 · Here the satellite has a revolutionary time period. The amount of time an object (satellite) rotates in circular orbits depends on the radius of the circular path. By … WebThe correct option is A. the mass of the satellite. Time period in terms of orbital speed is given by. T = 2πr vo = 2πr √GM r = 2π√ r3 GM. where, T = time period of satellite. M = … WebApr 2, 2015 · For a circular orbit orbital velocity is constant at $$\sqrt ... The orbital period of a satellite is solely determined by the semi-major axis of its orbit and the body it’s … setting up postfix mail server on ubuntu