Description
Returns the elevation angle measured between the orbital plane and the CentralBody-Sun vector. Note that the orbital plane is defined by the orbital momentum vector evaluated in the ICRF.
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.
Attributes
Type: |
number |
Access: |
read |
Units: |
deg |
Syntax
myVariable1 = mySpacecraft1.BetaAngle; |
See also
Coverage and Contact Analysis Guide