#<AM-acces:COL-V2.0>
<INIT:
Logiciel="JPSIMU"
VERSION="V11.4.1"
<COL:
  1 : EVENT ~ (Event code)
  2 : DDD ~cal (date)
  3 : TIME ~s (duration since initial conditions)
  4 : A ~km (semi-major axis)
  5 : E ~ (eccentricity)
  6 : I ~deg (inclination)
  7 : ALTG ~km (geodetic altitude)
  8 : LATG ~deg (geodetic latitude)
  9 : LON ~deg (longitude)
>
>
 Constant thrust maneuver Maneuver1 start: Relative date (0j00h10m00s)     2000-01-01T00:10:00.000        6.00000000000000e+02        7.00000006665629e+03        9.52233579255254e-09        5.15999981057783e+01        6.26650567709823e+02        2.83267318798703e+01       -7.73441356109702e+01
 Constant thrust maneuver Maneuver1 end: Date (2000-01-01T00:12:12.000)    2000-01-01T00:11:40.000        7.00000000000000e+02        7.07569671802727e+03        1.06930031433105e-02        5.15999981057783e+01        6.28194776514761e+02        3.26360096408306e+01       -7.25917790877161e+01
