ModifiedKeplerianElements Methods |
The ModifiedKeplerianElements type exposes the following members.
Name | Description | |
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![]() | Clone |
Clones this object using the specified context.
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![]() | ComputeEccentricAnomaly |
Computes the eccentric anomaly based on the current Keplerian position.
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![]() | ComputeEccentricity |
Computes the eccentricity based on the current elements.
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![]() | ComputeHyperbolicAnomaly |
Computes the hyperbolic anomaly based on the current Keplerian position.
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![]() | ComputeMeanAnomaly |
Computes the mean anomaly based on the current Keplerian position.
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![]() | ComputeMeanMotion |
Computes the mean motion based on the current Keplerian elements.
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![]() | ComputeParabolicAnomaly |
Computes the parabolic anomaly based on the current Keplerian position.
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![]() | ComputePeriod |
Computes the orbital period of the current Keplerian elements.
For parabolic and hyperbolic orbits the method returns PositiveInfinity.
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![]() | ComputeRadiusOfApoapsis |
Computes the radius of apoapsis based on the current elements.
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![]() | Equals | Determines whether the specified object is equal to the current object. (Inherited from Object.) |
![]() | GetDefinitionHashCode |
Gets a hash code representing the definition of this object.
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![]() | GetHashCode | Serves as the default hash function. (Inherited from Object.) |
![]() | GetType | Gets the Type of the current instance. (Inherited from Object.) |
![]() | IsSameDefinition |
Determines if this object has the same definition as another object.
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![]() | ToCartesian |
Returns a cartesian representation of these orbital elements.
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![]() | ToString | Returns a string that represents the current object. (Inherited from Object.) |