Spacecraft.BL_RAAN Property |
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DescriptionThe mean right ascension of the ascending node in the Brouwer-Lyddane Mean Element set. The angle, measured at the center of the Earth, from the vernal equinox to the ascending node. The ascending node is the point where the satellite crosses the fundamental plane of the ICRF going from south to north.
Timing Precision Mode This page describes functionality in millisecond timing precision mode. Millisecond timing precision mode is deprecated and will be removed in a future release. We recommend that you migrate your Mission Plans to nanosecond timing precision mode. Click here to see the documentation for this object in nanosecond timing precision mode.
Attributes
Syntax
See also Coverage and Contact Analysis Guide
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