KeplerianElements Constructor |
Overload List| Name | Description | |
|---|---|---|
 | KeplerianElements(DelaunayElements) |
Initialize a set of classical Keplerian elements from a set of DelaunayElements.
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| KeplerianElements(EquinoctialElements) |
Initialize a set of classical Keplerian elements from a set of EquinoctialElements.
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| KeplerianElements(ModifiedKeplerianElements) |
Initialize a set of classical Keplerian elements from a set of
ModifiedKeplerianElements.
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| KeplerianElements(MotionCartesian, Double) |
Initializes a new instance from the specified Cartesian motion and gravitational parameter.
The given elements must represent a closed orbit.
For other orbit types, use ModifiedKeplerianElements.
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| KeplerianElements(Cartesian, Cartesian, Double) |
Initialize a set of classical Keplerian elements from a Cartesian position and velocity.
The given elements must represent a closed orbit.
For other orbit types, use ModifiedKeplerianElements.
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| KeplerianElements(DelaunayElements, Double, Double) |
Initialize a set of classical Keplerian elements from a set of DelaunayElements.
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| KeplerianElements(EquinoctialElements, Double, Double) |
Initialize a set of classical Keplerian elements from a set of EquinoctialElements.
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| KeplerianElements(MotionCartesian, Double, Double, Double) |
Initializes a new instance from the specified cartesian motion and gravitational constant.
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| KeplerianElements(Cartesian, Cartesian, Double, Double, Double) |
Initialize a set of classical Keplerian elements from a cartesian position and velocity.
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| KeplerianElements(Double, Double, Double, Double, Double, Double, Double) |
Initialize a set of classical Keplerian orbital elements.
The given elements must represent a closed orbit.
For other orbit types, use ModifiedKeplerianElements.
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See Also