Question: Write a Matlab function that computes the Cartesian position and velocity of a satellite on an orbit in the perifocal frame, given the gravitational parameter

Write a Matlab function that computes the Cartesian position and velocity of a satellite on an orbit in the perifocal frame, given the gravitational parameter (mu) , the semi-major axis a, the true anomaly, the eccentricity e, and the true anomaly (theta).

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