Spacecraft.NoradEquinoctialLongitude Property |
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DescriptionThis property has been Deprecated. Please use the SGP4.EquinoctialLongitude property instead.
Equinoctial Norad based Longitude defined by the mean longitude, defined as: RAAN + w + MA, where RAAN and w are the Right Ascension of the Ascending Node and the Argument of Perigee, respectively, and MA is the Keplerian mean anomaly. These orbit properties are with respect to the True Equator Mean Equinox coordinate frame.
Timing Precision Mode This page describes functionality in nanosecond timing precision mode. Click here to see the documentation for this object in millisecond timing precision mode.
Attributes
Syntax
See also Coverage and Contact Analysis Guide
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