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IAgCrdnVectorOrbitAngularMomentum Interface

Description

Vector perpendicular to the plane of an elliptical orbit created from the motion of the specified point with respect to the center of the specified central body.

Object Model



Public Properties

Public Property CentralBody Specify a central body.
Public Property MeanElementType Specify the mean element theory type for approximating motion.
Public Property ReferencePoint Eliptical 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 orbit angular momentum of the specified point with respect to the specified central body.

CoClasses that Implement IAgCrdnVectorOrbitAngularMomentum

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STK Programming Interface 11.0.1