CelestialObject.SetKeplerianState Method

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Description

Sets the Keplerian state of the CelestialObject, referenced from the CentralBody. This requires that the CelestialObject uses a TwoBody propagator, and will error if other propagators are used.

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.SetKeplerianState(TimeSpan epoch, Array state)	None	Sets the Keplerian state of the CelestialObject in the ICRF, referenced from the CentralBody. This requires that the CelestialObject uses a TwoBody propagator, and will error if other propagators are used.
CelestialObject.SetKeplerianState(TimeSpan epoch, Array state, Variable referenceFrame)	None	Sets the Keplerian state of the CelestialObject in the specified frame, referenced from the CentralBody. This requires that the CelestialObject uses a TwoBody propagator, and will error if other propagators are used.

See also

CelestialObject Object

CelestialObjects Guide