Question

The orbit of a certain a satellite has a semimajor axis of 1.5 x107m and an eccentricity of 0.20. Its perigee (minimum distance) and apogee (maximum distance) are respectively:
A) 1.2 x107m, 1.8 x107m
B) 3.0 x106m, 1.2 x107m
C) 6.0 x106m, 9.0 x106m
D) 1.0 x107m, 1.2 x107m
E) 9.6 x106m, 1.8 x107m

Answer

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