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KeplerianElementsComputeMeanAnomaly 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
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public double ComputeMeanAnomaly()

Return Value

Type: Double
The current mean anomaly (radians).
Exceptions
ExceptionCondition
InvalidOperationExceptionThrown if the OrbitType does not represent either a circular or elliptical orbit. To find mean anomaly for parabolic or hyperbolic orbits, convert to ModifiedKeplerianElements.
See Also