KeplerianElementsTrueAnomaly Property

public double TrueAnomaly { get; }

Public ReadOnly Property TrueAnomaly As Double
	Get

public:
property double TrueAnomaly {
	double get ();
}

member TrueAnomaly : float with get

Property Value

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).

Reference