Spacecraft.EPV(AcqData) Method |
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DescriptionExtended Precision Vectors give spacecraft position and velocity information in the Geocentric True of Date Rotating reference frame.
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.
Note: This is an interval method. See the Interval Methods page for more information. Note: This method has a state. See the Methods and Properties with State page for more information.
Method Signature
Arguments
Return Value
Returns spacecraft position and velocity information in the Geocentric True of Date Rotating reference frame.
Syntax
See also Coverage and Contact Analysis Guide
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