CelestialObject.SetKeplerianState(Variable, Array, Variable) Method

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Description

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.

Timing Precision Mode

This page describes functionality in millisecond timing precision mode. Millisecond timing precision mode is deprecated and will be removed in a future release. We recommend that you migrate your Mission Plans to nanosecond timing precision mode.

Click here to see the documentation for this object in nanosecond timing precision mode.

Method Signature

CelestialObject.SetKeplerianState(	Variable epoch,
	Array state,
	Variable referenceFrame)

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

referenceFrame

Description:

The reference frame in which the state elements will be evaluated.

Valid Values:

Value	Label
1	ICRF
2	Mean of J2000 Earth Ecliptic
3	Mean of 1950 Earth Equator

Syntax

myCelestialObject1.SetKeplerianState(myVariable1, myArray1, myVariable2);