c2kecirc.out

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Enter input file name: 
filename = c2kecirc.in
Input pos/vel: 
    7378.1400000000000000        0.0000000000000000        0.0000000000000000
       0.0000000000000000        7.3501404378844740        0.0000000000000000
Input mu:   398600.8000000000000000
lan is undefined; orbit is equatorial. 
e or node vec is zero; arg of perigee is undefined 
Output elements (a,e,i,lan,w,m):
    7378.1400000000000000        0.0000000000000000        0.0000000000000000
       0.0000000000000000        0.0000000000000000        0.0000000000000000
True anom, eccen anom, semi-latus rectum: 
     360.0000000000000000        0.0000000000000000     7378.1400000000000000
Period: 
    6307.1204195462790000