Properties for Equinoctial elements.
Formulation | Retrograde, which has its singularity at an inclination of 0 deg. Posigrade, which has its singularity at an inclination of 180 deg. |
h | h/k collectively describe the shape of the satellite's orbit and the position of perigee. Dimensionless. |
k | h/k collectively describe the shape of the satellite's orbit and the position of perigee. Dimensionless. |
MeanLongitude | Specifies a satellite's position within its orbit at epoch and equals the sum of the classical Right Ascension of the Ascending Node, Argument of Perigee, and Mean Anomaly. Uses Angle Dimension. |
MeanMotion | Gets or sets the average angular rate of the satellite based on 2 body motion. Uses Rate Dimension. |
p | p/q collectively describe the orientation of the satellite's orbit plane. Dimensionless. |
q | p/q collectively describe the orientation of the satellite's orbit plane. Dimensionless. |
SemiMajorAxis | Half the length of the major axis of the orbital ellipse. Uses Distance Dimension. |
Implemented Interface |
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IAgVAElement |