Spacecraft.ModifiedEquinoctialP Property

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Description

The semiparameter p is defined by: p = a*(1-e^2) where a and e are the Keplerian Semi-Major Axis and Eccentricity.

Timing Precision Mode

This page describes functionality in nanosecond timing precision mode.

Click here to see the documentation for this object in millisecond timing precision mode.

myVariable1 = mySpacecraft1.ModifiedEquinoctialP;

mySpacecraft1.ModifiedEquinoctialP = myVariable1;