CelestialObject.GetKeplerianStateAtEpoch Method

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Description

Returns the A, E, I, RAAN, W, TA 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.GetKeplerianStateAtEpoch(TimeSpan epoch)

Array

Returns the A, E, I, RAAN, W, TA components of the state of the CelestialObject at the specified epoch in the MJ2000 Earth Equator frame, referenced from the CentralBody.

CelestialObject.GetKeplerianStateAtEpoch(TimeSpan epoch, Variable referenceFrame)

Array

Returns the A, E, I, RAAN, W, TA components of the state of the CelestialObject at the specified epoch in the specified frame, referenced from the CentralBody.

 

 

See also

CelestialObject Object

CelestialObjects Guide