The recently suggested SEE (Satellite Energy Exchange) method of measuring
the gravitational constant G, possible equivalence principle violation
(measured by the E\"{o}tv\"{o}s parameter η) and the hypothetic 5th force
parameters α and λ on board a drag-free Earth's satellite is
discussed and further developed. Various particle trajectories near a heavy
ball are numerically simulated. Some basic sources of error are analysed. The
G measurement procedure is modelled by noise insertion to a ``true''
trajectory. It is concluded that the present knowledge of G,α (for
λ≥1 m) and η can be improved by at least two orders of
magnitude.Comment: (only two misprints on title page) 7 page