Spacecraft.EVector Property |
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DescriptionRepresents 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
Syntax
See also Coverage and Contact Analysis Guide
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