CalculateTrueAnomalyStep

CALCULATE TRUE ANOMALY STEP Calculate the Orbit True Anomaly using the initial position and velocity.

function f = calculateTrueAnomaly(initialStates)

INPUTS:

initialStates - [x0 y0 z0 x0dot y0dot z0dot] Initial position and velocity in m and m/s.

OUTPUTS:

newStep - New step dependant on true anomaly for orbit.

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