Question

A satellite in an elliptical orbit has a speed of 9.00km/s when it is at its closes approach to the Earth(perigee). The satellite is 7.00x10^6 m from the center of the Earth at this time. When the satellite is at its greatest distance from the center of the Earth (apogee), its speed is 3.66km/s. Find the distance from the satellite to the center of the Earth at apogee. (assume any energy losses are negligible.)

Related Questions

Among elliptical orbits, some more circular than others. false true Just need to know if m... Statuary Hal is an elliptical room in the U.S. Capitol. Teh room is also called the Whispering Galle... the base of s is a elliptical region with boudary cuvrve 16x^2 +16y^2 =4. cross sections perpandicul... How are spiral and elliptical galaxies similar. (give 2 comparisons) Elliptical galaxies are the largest and contain the oldest stars An elliptical clause is a(n) ______________ in which words are missing. (1 point) Responses adj... An elliptical clause is a(n) missing. clause in which words are (1 point) adjectival verbal... What do most elliptical and spiral galaxies have at their cores? (1 point) Responses A cluste... What do most elliptical and spiral galaxies have at their cores? (1 point) Responses A cluste... Elliptical trainer