Spacecraft.StepToApsis Method

Top

Description

Steps to the specified apsis of the Spacecraft's orbit based on its current central body. The next or previous apsis is selected based on the sign of the current propagator stepsize.

Timing Precision Mode

This page describes functionality in millisecond timing precision mode.

Click here to see the documentation for this object in nanosecond timing precision mode.

Overload List

Signatures	Return Value	Description
Spacecraft.StepToApsis(Variable apsis)	Variable	Steps to the specified apsis of the Spacecraft's orbit based on its current central body. The next or previous apsis is selected based on the sign of the current propagator stepsize.
Spacecraft.StepToApsis(Variable apsis, Variable direction)	Variable	Steps to the specified apsis of the Spacecraft's orbit based on its current central body, in the specified direction.