// Copyright (c) CNES 2008
//
// This software is part of CelestLab, a CNES toolbox for Scilab
//
// This software is governed by the CeCILL license under French law and
// abiding by the rules of distribution of free software. You can use,
// modify and/ or redistribute the software under the terms of the CeCILL
// license as circulated by CEA, CNRS and INRIA at the following URL
// 'http://www.cecill.info'.
function [cireq,jacob] = CL__oe_kep2cireq(kep)
// Keplerian to circular equatorial orbital elements
//
// Calling Sequence
// [cireq, jacob] = CL__oe_kep2cireq(kep)
//
// Description
//
//
Converts classical Keplerian orbital elements to circular equatorial orbital elements.
//
The transformation jacobian is optionally computed.