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 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.

Attributes

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

Syntax

myVariable1 = mySpacecraft1.EVector[0];