Spacecraft.ModifiedEquinoctialL Property

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Description

The True Longitude, L, is defined by: L = RAAN + w + TA, where RAAN and w are the Right Ascension of the Ascending Node and the Argument of Perigee, respectively, and TA is the Keplerian true anomaly. These orbit properties are with respect to the ICRF.

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
Units:	deg
Default Value:	136.913078665814
Valid Range:	0 ≤ Spacecraft.ModifiedEquinoctialL ≤ 360

Syntax

myVariable1 = mySpacecraft1.ModifiedEquinoctialL;

mySpacecraft1.ModifiedEquinoctialL = myVariable1;