Spacecraft.Apogee Property |
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DescriptionReturns an instantaneous osculating estimate of the apoapsis distance from the center of its central body to the Spacecraft, based on the current orbital state. The Spacecraft.Apogee 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 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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