SGP4Properties.EquinoctialQ Property

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Description

The q component of the SGP4 based Equinoctial element set, defined by: q = tan(i/2)cos(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 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
Default Value:	0.614627033889727

Syntax

myVariable1 = mySGP4Properties1.EquinoctialQ;

mySGP4Properties1.EquinoctialQ = myVariable1;