A satellite is orbiting the earth at a height of 100 km. What extra velocity, in km/s, must be applied to it so that it leaves earth in a parabolic orbit? Round your answer to two digits after the decimal place. Me = 6x1024kg 6400km Re G = 6.673x10-"Nm²kg Hint: Do you remember the derivation of escape velocity?

A satellite is orbiting the earth at a height of 100 km. What extra velocity, in km/s, must be applied to it so that it leaves earth in a parabolic orbit? Round your answer to two digits after the decimal place. Me = 6x1024kg 6400km Re G = 6.673x10-"Nm²kg Hint: Do you remember the derivation of escape velocity?