CelestialObject.GetCartesianStateAtEpoch(Variable) Method |
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DescriptionReturns the X, Y, Z, VX, VY and VZ components of the state of the CelestialObject at the specified epoch in the MJ2000 Earth Equator frame, referenced from the CentralBody. The reference frame will be evaluated at the specified epoch.
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.
Method Signature
Arguments
Return Value
Returns the Cartesian state.
Syntax
See also CelestialObject.GetCartesianStateAtEpoch
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