Spacecraft.NonSingularE5 Property

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Description

The e5 component of the NonSingular Keplerian element set, defined by: e5 = RAAN + w + MA, where RAAN is the Right Ascension of the Ascending Node, w is the Right Ascension of the Ascending Node, and MA is the Mean 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:

136.750848428115

Valid Range:

0 ≤ Spacecraft.NonSingularE5 ≤ 360

 

Syntax

myVariable1 = mySpacecraft1.NonSingularE5;

 

mySpacecraft1.NonSingularE5 = myVariable1;

 

See also

Spacecraft Object

Spacecraft Propagation Guide

Coverage and Contact Analysis Guide