A satellite travels in an elliptical orbit around Earth

PHYSICS · Single correct · A Level · Physics · Fields and their consequences · Fields and their consequences

Problem

A satellite travels in an elliptical orbit around Earth. At perigee (point P) its distance from Earth’s center is rPr_P, and at apogee (point A) its distance is rAr_A with rA>rPr_A>r_P. Which of the following correctly compares the satellite’s kinetic energies KPK_P and KAK_A at these two points? (a) KP=KAK_P = K_A (b) KP>KAK_P > K_A (c) KP<KAK_P < K_A (d) The relationship cannot be determined without knowing the satellite’s mass.

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