Spacecraft.EVector Property

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Description

Represents the instantaneous eccentricity vector referenced to the Mean of J2000 Earth-Equator coordinate system. 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];

 

See also

Spacecraft Object

Spacecraft Propagation Guide

Coverage and Contact Analysis Guide