A geostationary orbit is one in which a satellite orbits the Earth (in a circular orbit) in the same time as it takes the Earth to make one full rotation with respect to the stars. a) Given the mass of the Earth, calculate the distance of a geostationary satellite from the center of the Earth. b) If you were standing on the equator with the geostationary satellite at your zenith, how long would it take to receive a radio signal? c) What is the satellite's orbital speed?
A geostationary orbit is one in which a satellite orbits the Earth (in a circular orbit)...
please refer to picture A satellite is in a circular orbit around the Earth. To increase the speed of the satellite while maintaining a circular orbit, one would need to a. b. c. d. increase in the satellite's mass. decrease in the satellite's mass. increase in the satellite's orbital radius. decrease the satellite's orbital radius. none of the above.
A geostationary communications satellite orbits the earth directly above the equator at an altitude of 34800 km .Calculate the time it would take a cell phone signal to travel from a point on the equator to the satellite and back.Would this delay be noticeable in a conversation?
For communications purposes, satellites are typically placed in a circular geosynchronous orbit. If the orbit is in the equatorial plane of the Earth, it is called geostationary. A satellite’s orbital speed in a geostationary orbit is set to match the angular velocity Ωe of the rotating Earth (with mass M), so that as seen from the Earth the satellite is stationary above a fixed point on the Equator. For a satellite of mass m in a geostationary circular orbit then...
Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 502 km above the earth’s surface, while that for satellite B is at a height of 747 km. Find the orbital speed for (a) satellite A and (b) satellite B.
Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 460 km above the earth’s surface, while that for satellite B is at a height of 774 km. Find the orbital speed for (a) satellite A and (b) satellite B.
Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 364 km above the earth's surface, while that for satellite B is at a height of 880. km. Find the orbital speed for satellite A and satellite B. (a) VA = (b) VB =
Exercise 9.5 A geostationary satellite orbits the earth in 24 hours along an orbital path that is parallel to an imaginary plane drawn through the Earth's equator. Such a satellite appears permanently fixed above the same location on the Earth. How high above the earth's surface must it be located?
18. A satellite orbits the earth once every 4 hours. If the mass of the Earth is 6.0e24 kg, what is the radius of the orbit of the satellite (measured from the center of the Earth)? Assume that the satellite's speed is constant and its orbit is circular. R = ? A B C D E 7.81e+006 m 6.93e+007 m 3.04e+007 m 1.28e+007 m 9.11e+007 m
Two identical satellites orbit the earth in stable orbits. One satellite orbits with a speed v at a distance r from the center of the earth. The second satellite travels at a speed that is less than v.At what distance from the center of the earth does the second satellite orbit?At a distance that is less than r.At a distance equal to r.At a distance greater than r.Now assume that a satellite of mass m is orbiting the earth at a distance...
A 544-kg satellite is in a circular orbit about Earth at a height above Earth equal to Earth's mean radius. (a) Find the satellite's orbital speed. m/s (b) Find the period of its revolution. (c) Find the gravitational force acting on it A satellite of Mars, called Phobos, has an orbital radius of 9.4 x 106 m and a period of 2.8 104 s. Assuming the orbit is circular, determine the mass of Mars. x 10 s. Assuming kg