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IAgCrdnVectorEccentricity Interface

Description

A vector directed from the center of the specified central body toward the nearest point of an elliptical orbit created from the motion of the specified point.

Public Properties

Public Property CentralBodySpecify a central body.
Public Property MeanElementTypeSpecify the mean element theory type for approximating motion.
Public Property ReferencePointElliptical orbit is fit to the current motion of the reference point according to the selected mean theory.

Remarks

At any time, the orbit is fit to the current motion of the specified point according to the specified type orbital elements. Available types are: osculating, Brouwer-Lyddane long and short, and Kozai. The vector's magnitude is equal to the current eccentricity of the fit orbit.

Interfaces

CoClasses that Implement IAgCrdnVectorEccentricity

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