Calculate the speed required to maintain a satellite in an orbit 500 miles above the surface of the earth?
Calculate the speed required to maintain a satellite in an orbit 500 miles above the surface...
A satellite in a circular orbit 500 miles above the surface of the Earth. What is the period of the orbit? You may use the following constants: Radius of the Earth: 4000 miles Gravitational Constant: 66710?11m3(kgs2) Mass of earth: 5981024kg Number of Meters in a mile: 1609 Period= ? seconds
A satellite is in orbit around Earth at a height of 120 km above Earth’s surface. Find the orbital speed of the satellite. (Mass of the earth is 6*1024 kg and the radius of Earth is 6371 km)
A 180 kg satellite is orbiting on a circular orbit 6355 km above the Earth's surface. Determine the speed of the satellite. (The mass of the Earth is 5.97x1024 kg, and the radius of the Earth is 6370 km.) Submit Answer Tries 0/12
A satellite of mass 210 kg is placed into Earth orbit at a height of 500 km above the surface. (a) Assuming a circular orbit, how long does the satellite take to complete one orbit? (b) What is the satellite's speed? m/s (C) Starting from the satellite on the Earth's surface, what is the minimum energy input necessary to place this satellite in orbit? Ignore air resistance but include the effect of the planet's daily rotation.
A 270 kg satellite is orbiting on a circular orbit 6180 km above the Earth's surface. Determine the speed of the satellite. (The mass of the Earth is 5.97×1024 kg, and the radius of the Earth is 6370 km.)
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.
Find the orbital speed of a satellite in a geosynchronous circular orbit 3.45×107 m above the surface of the Earth.
A geostationary satellite is a satellite located in an orbit such that it remains above the same point on the Earth’s surface. [Assume it takes 23 hours 56 minutes 4.09 seconds for the Earth to spin around once.] a) What is the angular velocity of such a satellite? b) What is the altitude of such a satellite? c) Calculate the period of a satellite orbiting 200km above the Earth.
An Earth satellite moves in a circular orbit 724 km above Earth's surface with a period of 99.07 min. What are (a) the speed and (b) the magnitude of the centripetal acceleration of the satellite? 3 sig figs please
12.104. A satellite describes a circular orbit at an altitude of 19 110 km above the surface of the earth. Determine (a) the increase in speed required at point A for the satellite to achieve the escape velocity and enter a parabolic orbit, (b) the decrease in speed required at point A for the satellite to enter an elliptic orbit with a minimum altitude of 6370 km, (c) the eccentricity e of the elliptic orbit. R = 6370 km 19...