This method can be used with the Step command to advance the Spacecraft to the point in its orbit at which the Spacecraft crosses its central body's instantaneous equatorial plane, moving from the south to the north. It serves as the conditional statement for the "to" statement that can be used with the Step command.
Timing Precision Mode
This page describes functionality in nanosecond timing precision mode.
Note: This is a Stop-Propagation property. See the Stop-Propagation Properties and Methods page for more information.
Note: This property has a state. See the Methods and Properties with State page for more information.