CelestialObject.SetKeplerianState(TimeSpan, Array) Method

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Description

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.

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.

Method Signature

CelestialObject.SetKeplerianState(	TimeSpan epoch,
	Array state)

Arguments

epoch
Description:	The epoch at which the CelestialObject's state is evaluated.

state
Description:	array containing the Keplerian Elements in order: {A, E, I, RAAN, W, TA}
Required Size:	6

Syntax

myCelestialObject1.SetKeplerianState(myTimeSpan1, myArray1);