Spacecraft.Apoapsis Property |
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DescriptionReturns an instantaneous osculating estimate of the apoapsis distance from the center of the CentralBody to the Spacecraft, based on the current orbital state. The Spacecraft.Apoapsis property is not based on a force model and is computed directly from the instantaneous Keplerian elements where the instantaneous Keplerian elements are computed from the active state of the Spacecraft.
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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