(a)(c)A certain satellite has eccentricity of 9.5981 x 10-3 and its semimajor axis is knownto be 7194.9 km. The true anomaly v of the satellite is 204.81° and the mean motionis 14.2171404 rev/day. Calculatei.ii.iii.iv.V.Given the orbital elements of a particular satellite are:(i)the orbital period of the satellite in minutes.the magnitude of position vector r.position vector r in PQW frame.altitude of the satellite at zenith.satellite velocity at epoch(ii)= 300°; w = 60°; i = 65°; rp = -6500 km; ro = 4000 kmCalculate the position vector r in the IJK frame.Calculate the magnitude of position vector.

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Answered: A certain satellite has eccentricity of…

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