Spacecraft.SetKeplerianState Method

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Description

Sets the Keplerian state of the Spacecraft, 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

Spacecraft.SetKeplerianState(Array state)

None

Sets the Keplerian state of the Spacecraft in the ICRF, referenced from the CentralBody.

Spacecraft.SetKeplerianState(Array state, Variable referenceFrame)

None

Sets the Keplerian state of the Spacecraft in the specified frame, referenced from the CentralBody.

Spacecraft.SetKeplerianState(Array state, Variable referenceFrame, TimeSpan frameEpoch)

None

Sets the Keplerian state of the Spacecraft in the specified frame, referenced from the CentralBody. The reference frame will be evaluated at the specified frameEpoch.

 

 

See also

Spacecraft Object

Spacecraft Propagation Guide

Coverage and Contact Analysis Guide