Spacecraft.W Property

Top

Description

The Keplerian argument of perigee (w). The angle measured at the center of the central body, from the ascending node to the point in the satellite's orbit closest to the central body.

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
Units:	deg
Default Value:	171.130489033293
Valid Range:	0 ≤ Spacecraft.W ≤ 360

Syntax

myVariable1 = mySpacecraft1.W;

mySpacecraft1.W = myVariable1;