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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: 25.1.421.0 (25.1.421.0)
Syntax
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public double ComputeMeanAnomaly()

Return Value

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