Please Asap A satellite is in an elliptic orbit around the Earth. Its speed at theperigee A is 8526 m/s (Figure 1).Figure16,460 kmB14.255 kmA8230 km 8230 km1 of 1 >Part AUse conservation of energy to determine its speed at B. The radius of the Earth is 6380 km.Express your answer in meters per second.IV-I ΑΣΦVB=21774678.53SubmitPart BX Incorrect; Try Again; 26 attempts remainingVc =Previous Answers Request AnswerSubmitUse conservation of energy to determine the speed at the apogee C.Express your answer in meters per second.IVE ΑΣΦ 5www. ?Request Answer< Return to AssignmentProvide Feedbackm/swww. ?m/s

Laws of energy conservation satellite orbit around the earth: A satellite's total energy (T.E) at…

A satellite is in an elliptic orbit around the Earth. Its speed at the perigee A is 8526 m/s (Figure 1). Figure 16,460 km B 14,255 km A 8230 km 8230 km 1 of 1 > Part A Use conservation of energy to determine its speed at B. The radius of the Earth is 6380 km. Express your answer in meters per second. UB= Submit Previous Answers Request Answer -Η ΑΣΦ 21774678.53 Part B X Incorrect; Try Again; 26 attempts remaining VC= Use conservation of energy to determine the speed at the apogee C. Express your answer in meters per second. - ΑΣΦ " Submit Request Answer ? < Return to Assignment Provide Feedback m/s ? m/s