This property has been Deprecated. Please use the SGP4.EquinoctialK property instead.
The k component of the Norad based Equinoctial element set, defined by: k = e*cos(RAAN + w), where e, w, and RAAN are the Norad Eccentricity, Argument of Perigee and Right Ascension of the Ascending Node respectively. These orbit properties are with respect to the True Equator Mean Equinox coordinate frame.
Timing Precision Mode
This page describes functionality in millisecond timing precision mode.