Spacecraft.ModifiedEquinoctialP Property

Top

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 millisecond timing precision mode. Millisecond timing precision mode is deprecated and will be removed in a future release. We recommend that you migrate your Mission Plans to nanosecond timing precision mode.

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

Attributes

Type:	number
Access:	read/write
Units:	km
Default Value:	7088.43664188243

Syntax

myVariable1 = mySpacecraft1.ModifiedEquinoctialP;

mySpacecraft1.ModifiedEquinoctialP = myVariable1;