Spacecraft.EquinoctialLongitude Property

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Description

Equinoctial Longitude defined by the mean longitude, defined as: RAAN + w + MA, where RAAN and w are the Right Ascension of the Ascending Node and the Argument of Perigee, respectively, and MA is the Keplerian mean anomaly. These orbit properties are with respect to the ICRF.

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:	252.791158382791
Valid Range:	0 ≤ Spacecraft.EquinoctialLongitude ≤ 360

Syntax

myVariable1 = mySpacecraft1.EquinoctialLongitude;

mySpacecraft1.EquinoctialLongitude = myVariable1;