Description
Returns the X, Y, Z, VX, VY and VZ components of the state of the CelestialObject at the specified epoch, referenced from the CentralBody.
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.
Overload List
Signatures
|
Return Value
|
Description
|
CelestialObject.GetCartesianStateAtEpoch(TimeSpan epoch)
|
Array
|
Returns the X, Y, Z, VX, VY and VZ components of the state of the CelestialObject at the specified epoch in the ICRF, referenced from the CentralBody. The reference frame will be evaluated at the specified epoch.
|
CelestialObject.GetCartesianStateAtEpoch(TimeSpan epoch, Variable referenceFrame)
|
Array
|
Returns the X, Y, Z, VX, VY and VZ components of the state of the CelestialObject at the specified epoch in the specified frame, referenced from the CentralBody. The reference frame will be evaluated at the specified epoch.
|
CelestialObject.GetCartesianStateAtEpoch(TimeSpan epoch, Variable referenceFrame, TimeSpan frameEpoch)
|
Array
|
Returns the X, Y, Z, VX, VY and VZ components of the state of the CelestialObject at the specified epoch in the specified frame, referenced from the CentralBody. The reference frame will be evaluated at the specified frameEpoch.
|
See also
CelestialObject Object
CelestialObjects Guide
|