

1. A geosynchronous orbit is one that if a satellite is placed equatorially in it will...
A geosynchronous orbit is one that if a satellite is placed equatorially in it will appear stationary above the same geographical spot. Starting from Newton's law of universal gravitation for circular orbits calculate the radius of this orbit. (You must show all steps). (8 points) TTT Anal 3(1201) .T.E.E.
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...
A geosynchronous satellite is placed above the equator and orbiting around the earth to facilitate communication around the world. (You may consider that the mass of the satellite is m, mass of the earth is M(6x1024 kg), center-to-center distance between the satellite and the earth is r, radius of the earth is R(6.4×106 m), and the universal gravitational constant G = 6.67x10-11 N.m2/kg2.) Satellite Earth Applying newton's 2nd law, write an equation describing the circular motion of the satellite. (4...
A satellite is said to be in a geosynchronous orbit. a) what is the period of this orbit? b) at what distance from the center of Earth must such a satellite be placed into orbit? (Hint: Use Newton's form of Kepler's third law)
a satellite in a geosynchronous orbit remains above the same
point on Earth
2. A satellite in a geosynchronous orbit remains above the same point on Earth provided it orbits in the equatorial plane in the same direction as Earth's rotation. (a) Calculate the speed of a satellite in such an orbit. (b) Calculate the total energy of a satellite in such an orbit.
Previous Question: A satellite is said to be in a “geosynchronous” orbit if it appears always to remain over the exact same spot on the rotating Earth. What is the period of this orbit? [enter your answer in hours.] (a) At what distance (in km) from the center of the Earth must such a satellite be placed into orbit? [Enter your answer in regular decimal notation instead of scientific notation, i.e. not 3.97 x 10^5, but 397000 .] (b) Why...
A satellite of mass 42.5 kg in geosynchronous orbit at an altitude of 3.58 ✕ 104 km above the Earth's surface remains above the same spot on the Earth. Assume its orbit is circular. Find the magnitude of the gravitational force exerted by the Earth on the satellite. Hint: The answer is not 417 N
Major Tom orbits the planet Earth aboard a geosynchronous space station. In a geosynchronous orbit, the station stays above the same spot on the surface of the planet and orbits in time with Earth’s rotation. A) What is the space station’s orbital speed? Assume the radius is perfectly circular. B) What is the only possible radius for such an orbit? (You may calculate the radius from the center of the Earth) C) Major Tom’s weight on the surface of Earth...
6.43- Satellites and Kepler's Laws: An Argument for Simplicity A geosynchronous Earth satellite is one that has an orbital period of precisely 1 day. Such orbits are useful for communication and weather observation because the satellite remains above the same point on Earth (provided it orbits in the equatorial plane in the same direction as Earth's rotation). Calculate the radius of such an orbit based on the data for the moon using the following data: Distance from Earth to Moon...
Consider a 435 satellite in a circular orbit at a distance of 3.19X10^4 above the Earth’s surface. What is the minimum amount of work W the satellite’s thrusters must do to raise the satellite to a geosynchronous orbit? Geosynchronous orbits occur at approximately 3.6X10^4 above the Earth’s surface. The radius of the Earth and the mass of the Earth are RE=6.37X10^3 and 5.97X10^24 respectively. The gravitational constant is G = 6.67X10^-11 Assume the change in mass of the satellite is...