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 Mean of J2000 Earth-Equator 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

Units:

deg

Default Value:

136.913078665814

Valid Range:

0 ≤ Spacecraft.ModifiedEquinoctialL ≤ 360

 

Syntax

myVariable1 = mySpacecraft1.ModifiedEquinoctialL;

 

mySpacecraft1.ModifiedEquinoctialL = myVariable1;

 

See also

Spacecraft Object

Spacecraft Propagation Guide

Coverage and Contact Analysis Guide