Spacecraft.StepToApsis(Variable, Variable) Method |
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DescriptionSteps to the specified apsis of the Spacecraft's orbit based on its current central body, in the specified direction.
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.
Method Signature
Arguments
Return Value
Returns the duration of the total step taken.
Syntax
See also Coverage and Contact Analysis Guide
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