ModifiedKeplerianElementsComputeEccentricAnomaly Method

Computes the eccentric anomaly based on the current Keplerian position.

Namespace: AGI.Foundation.Coordinates
Assembly: AGI.Foundation.Core (in AGI.Foundation.Core.dll) Version: 25.2.423.0 (25.2.423.0)

Syntax

public double ComputeEccentricAnomaly()

Public Function ComputeEccentricAnomaly As Double

public:
double ComputeEccentricAnomaly()

member ComputeEccentricAnomaly : unit -> float

Type: Double
The current eccentric anomaly, in radians.

Exceptions

Exception	Condition
InvalidOperationException	Thrown when the OrbitType is not circular or elliptical.

ModifiedKeplerianElementsAddLanguageSpecificTextSet("LST1B503349_0?cpp=::|nu=.");ComputeEccentricAnomaly Method