CelestialObject.GetCartesianStateAtEpoch(Variable) Method

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Description

Returns the X, Y, Z, VX, VY and VZ components of the state of the CelestialObject at the specified epoch in the ICRF, referenced from the CentralBody. The reference frame will be evaluated at the specified epoch.

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.GetCartesianStateAtEpoch(

Variable epoch)

Arguments

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

Return Value

Type:

Array of number (size = 6)

Returns the Cartesian state.

Syntax

myArray1 = myCelestialObject1.GetCartesianStateAtEpoch(myVariable1);