SGP4Properties.EquinoctialK Property

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Description

The k component of the SGP4 based Equinoctial element set, defined by: k = e*cos(RAAN + w), where e, w, and RAAN are the SGP4 Eccentricity, Argument of Perigee and Right Ascension of the Ascending Node respectively. 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:	-0.000508347956724512

Syntax

myVariable1 = mySGP4Properties1.EquinoctialK;

mySGP4Properties1.EquinoctialK = myVariable1;