CelestialObject.GetKeplerianStateAtEpoch(TimeSpan) 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 in the MJ2000 Earth Equator frame, 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.

 

Method Signature

CelestialObject.GetKeplerianStateAtEpoch(

TimeSpan epoch)

 

 

Arguments

epoch


Description:

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

 

 

 

Return Value

Type:

Array of number (size = 6)

 

 

Returns the Keplerian state.

 

Syntax

myArray1 = myCelestialObject1.GetKeplerianStateAtEpoch(myTimeSpan1);

 

 

See also

CelestialObject Object

CelestialObject.GetKeplerianStateAtEpoch

CelestialObjects Guide