Spacecraft.GetKeplerianState() Method

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Description

Returns the A, E, I, RAAN, W, TA components of the state of the Spacecraft in the ICRF, 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

Spacecraft.GetKeplerianState(

)

 

 

Return Value

Type:

Array of number (size = 6)

 

 

Returns the Keplerian state.

 

Syntax

myArray1 = mySpacecraft1.GetKeplerianState();

 

 

See also

Spacecraft Object

Spacecraft.GetKeplerianState

Spacecraft Propagation Guide

Coverage and Contact Analysis Guide