Click or drag to resize

ModifiedKeplerianElementsComputeMeanAnomaly Method

Computes the mean anomaly based on the current Keplerian position.

Namespace:  AGI.Foundation.Coordinates
Assembly:  AGI.Foundation.Core (in AGI.Foundation.Core.dll) Version: 24.3.420.0 (24.3.420.0)
Syntax
Copy
public double ComputeMeanAnomaly()

Return Value

Type: Double
The current mean anomaly (radians).
Exceptions
ExceptionCondition
InvalidOperationExceptionIn the case of a hyperbolic orbit, the true anomaly 'v' is bound within: -Pi+ Acos(1/e) < v < Pi - Acos(1/e). Otherwise, the method throws an exception.
See Also