Spacecraft.SetKeplerianState(Array) Method

 Top 

Description

Sets the Keplerian state of the Spacecraft 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

Spacecraft.SetKeplerianState(

Array state)

 

 

Arguments

state

Description:

array containing the Keplerian Elements in order: {A, E, I, RAAN, W, TA}

Required Size:

6

 

 

 

Syntax

mySpacecraft1.SetKeplerianState(myArray1);

 

 

See also

Spacecraft Object

Spacecraft.SetKeplerianState

Spacecraft Propagation Guide

Coverage and Contact Analysis Guide