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 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:	136.750848428115
Valid Range:	0 ≤ Spacecraft.NonSingularE5 ≤ 360

Syntax

myVariable1 = mySpacecraft1.NonSingularE5;

mySpacecraft1.NonSingularE5 = myVariable1;