Name

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  auxelem

Purpose (one Line Only)

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  Compute auxilary orbital elements

Description

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Category

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  Celestial Mechanics

Calling Sequence

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  auxelem,node,arg,inc,px,qx,py,qy,pz,qz

Inputs

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  node - Longitude of ascending node (radians)
  arg - Argument of perihelion (radians)
  inc - Inclination (radians)

Optional Input Parameters

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Keyword Input Parameters

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Outputs

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  px,qx,py,qy,pz,qz - auxilary orbital elements (equinox J2000)

Keyword Output Parameters

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Common Blocks

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Side Effects

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Restrictions

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Procedure

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Modification History

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  2002/05/29 - Marc W. Buie, Lowell Observatory. Ported from fortran routines
    supplied by Larry Wasserman and Ted Bowell. (AE8.F)