KeplerianElementsInclination Property

public double Inclination { get; }

Public ReadOnly Property Inclination As Double
	Get

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

member Inclination : float with get

Property Value

The inclination of the orbit is its tilt with reference to the Equatorial plane, or, in the diagram below, the angle i between the central body's spin (Z) axis and the orbit's angular momentum vector.

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

Reference