A satellite is in an elliptic orbit around the earth. Its sped at perigee A is 8650 m/s.  Use conservation of energy to determine the speed at the apogee C. Radius of earth is 6380 km. Chapter 8 question 99 page 212 figure 8-46 in Giancoli Physics 4th edition

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A satellite is in an elliptic orbit around the earth. Its sped at perigee A is 8650 m/s. 

Use conservation of energy to determine the speed at the apogee C.

Radius of earth is 6380 km.

Chapter 8 question 99 page 212 figure 8-46 in Giancoli Physics 4th edition 

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