Answered: In a hyperbolic orbit of eccentricity… | bartleby

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This question is a MCQ type question and it is attached as an image. Thank you.

In a hyperbolic orbit of eccentricity 1.4 the true anomaly is 30° and semi major
axis is 26000 km. The distance of the satellite from the occupied focus is
a) 9215.36 km
b) 11281.68 km
c) 13589.58 km
d) 7893.53 km

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