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KeplerianElements Constructor (MotionCartesian, Double, Double, Double)

Initializes a new instance from the specified cartesian motion and gravitational constant.

Namespace:  AGI.Foundation.Coordinates
Assembly:  AGI.Foundation.Core (in AGI.Foundation.Core.dll) Version: 25.1.421.0 (25.1.421.0)
Syntax
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public KeplerianElements(
	Motion<Cartesian> motion,
	double gravitationalParameter,
	double eccentricityTolerance,
	double inclinationTolerance
)

Parameters

motion
Type: AGI.FoundationMotionCartesian
The cartesian position and velocity (distance and distance per time).
gravitationalParameter
Type: SystemDouble
The gravitational parameter for the central body (distance cubed per time squared).
eccentricityTolerance
Type: SystemDouble
The tolerance which defines the value of 'zero' to use when checking whether the eccentricity is zero below which the orbit is circular.
inclinationTolerance
Type: SystemDouble
The tolerance which defines the value of 'zero' to use when checking whether the inclination is zero below which the orbit is equatorial.
Exceptions
ExceptionCondition
ArgumentExceptionThe given elements must represent a closed orbit. The exception is thrown if the eccentricity is negative or not below unity or if the semimajor axis is not finitely positive. For other orbit types, use ModifiedKeplerianElements.
ArgumentOutOfRangeExceptionThrown if either eccentricityTolerance or inclinationTolerance is negative.
See Also