Spacecraft.EVector Property

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Description

Represents the instantaneous eccentricity vector referenced to the ICRF. The eccentricity vector points from the center of the central body toward perigee with a magnitude equal to the eccentricity of the orbit.

Timing Precision Mode

This page describes functionality in nanosecond timing precision mode.

Attributes

Type:	Array of number (size = 3)
Access:	read

Syntax

myVariable1 = mySpacecraft1.EVector[0];