SGP4Properties.EquinoctialP Property

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Description

The p component of the SGP4 based Equinoctial element set, defined by: p = tan(i/2)sin(RAAN), where i is the orbit inclination and RAAN is the SGP4 Right Ascension of the Ascending Node. These orbit properties are with respect to the True Equator Mean Equinox coordinate frame.

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.

Attributes

Type:	number
Access:	read/write
Default Value:	-0.979230283604418

Syntax

myVariable1 = mySGP4Properties1.EquinoctialP;

mySGP4Properties1.EquinoctialP = myVariable1;