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KeplerianElementsTrueAnomaly Property

Gets the true anomaly of the orbit, in radians.

Namespace:  AGI.Foundation.Coordinates
Assembly:  AGI.Foundation.Core (in AGI.Foundation.Core.dll) Version: 20.2.404.0 (20.2.404.0)
Syntax
public double TrueAnomaly { get; }

Property Value

Type: Double
Remarks

True anomaly is used to represent the satellite's instantaneous position with respect to periapsis, shown here as the angle θ:

In the above diagram, ω is the argument of periapsis, i is the inclination, and Ω is the right ascension of the ascending node (RAAN).

See Also