please solve part A, C, D, and E

Consider a 1000 kg communication satellite that needs Part B to be boosted from an orbit 250 km above the earth to a Part A geosynchronous orbit 35,900 km above the earth. Outer Find the velocity of at the low point on the elliptical orbit Find the velocity 1 on the inner circular orbit. orbit that spans the two circular orbits Express your answer to three significant figures and include the appropriate units. Express your answer to three significant figures and include the appropriate units. View Available Hint(s) Inner View Available Hint(s) orbit v = 1.02x104 m HA Submit Previous Answers Transfer ellipse Value Correct Units Part A Submit Part C Part C Part D Part E How much work must the rocket motor do to transfer Now find the velocity , at the high point of the the satellite from the circular orbit to the elliptical orbit? elliptical orbit. Express your answer to three significant figures and Now find the velocity va of the outer circular orbit. include the appropriate units. Express your answer to three significant figures and include the appropriate units. Express your answer to three significant figures and include the appropriate units. View Available Hint(s) >View Available Hint(s) > View Available Hint(s) HA LA HA 2.50 . 1010 W Value Value U2 Submit Previous Answers Request Answer Units Units Submit " Incorrect; Try Again; 5 attempts Submit remaining