eme2000-to-true-of-date conversion
==================================

UTC epoch        Apr 6, 2004 07:51:28.386009

UTC Julian date  2453101.8274119


true-of-date state vector and orbital elements
----------------------------------------------

      rx (km)             ry (km)             rz (km)             rmag (km)
 +5.0945147804e+003  +6.1273664612e+003  +6.3803445328e+003  +1.0208207333e+004  

      vx (kps)            vy (kps)            vz (kps)            vmag (kps)
 -4.7460885670e+000  +7.8607722200e-001  +5.5319312880e+000  +7.3311348276e+000  


      sma (km)         eccentricity      inclination (deg)      argper (deg)
 +1.6370586847e+004  +4.2497571368e-001  +6.3097546621e+001  +2.1396765469e+000 

     raan (deg)      true anomaly (deg)     arglat (deg)        period (min)
 +2.6288914132e+001  +4.2357214502e+001  +4.4496891049e+001  +3.4742102917e+002 


eme2000 state vector and orbital elements
-----------------------------------------

      rx (km)             ry (km)             rz (km)             rmag (km)
 +5.1025096000e+003  +6.1230115200e+003  +6.3781363000e+003  +1.0208207333e+004  

      vx (kps)            vy (kps)            vz (kps)            vmag (kps)
 -4.7432195996e+000  +7.9053660026e-001  +5.5337561903e+000  +7.3311348276e+000  


      sma (km)         eccentricity      inclination (deg)      argper (deg)
 +1.6370586847e+004  +4.2497571368e-001  +6.3105627394e+001  +2.1161700602e+000 

     raan (deg)      true anomaly (deg)     arglat (deg)        period (min)
 +2.6248067011e+001  +4.2357214502e+001  +4.4473384562e+001  +3.4742102917e+002