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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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
Transcribed Image Text: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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