Determines the entry time, exit time, and duration of a Spacecraft's pass through the shadow of a central body. Events are reported for umbral shadow conditions only. If the specified body is a member of the Earth-Moon system, the counterpart not specified will also be considered in shadow evaluation.
The image below shows the three regions of the spacecraft's central body's shadow, umbra, penumbra, and annular. UmbralShadowTimes reports events for the umbral shadow conditions only.
The three regions of the Spacecraft's central body's shadow.
Note: This method uses a spherical model for the occulting body. Use the options available in the VisibilityCalculator to exercise more control over the analysis.
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.
Determines the entry time, exit time, and duration of a Spacecraft's pass through the shadow of a central body. Events are reported for umbral shadow conditions only. If the specified body is a member of the Earth-Moon system, the counterpart not specified will also be considered in shadow evaluation.
Determines the entry time, exit time, and duration of a Spacecraft's pass through the shadow of a central body. Events are reported for umbral shadow conditions only. If the specified body is a member of the Earth-Moon system, the counterpart not specified will also be considered in shadow evaluation.