DESCRIPTION
The tasks dumps the contents of the orbit file in the current ODF
(pointed at via environment variable SAS_ODF) to stdout in the
format t x y z d vx vy vz vabs
where
t time in Mission-Elapsed-Time [s]
x, y, z components of S/C position vector in Earth-centeredJ2000 reference frame [km]
d norm of vector (x, y, z) [km]
vx, vy, vz components of S/C velocity vector in Earth-centeredJ2000 reference frame [km/s]
vabs norm of vector (vx, vy, vz)
The time increment between successive elements is given via task
parameter tstep which has a default value of 10s.
offsett=true causes all time tags to be offset by the time of first
element which, hence, is assigned 
.
