  The action sphere method program is written. The initial conditions set at
pericenter of planetocentric orbits. When action sphere radius is reached, the
heliocentric orbit is calculated and data redirected to numeric integration
program. The method is useful for capture and collision problem investigation.
The very preliminary numeric results were obtained and discussed. A manifold in
orbital elements space, leads to temporary capture about 50 year (4 Jupiter
revolutions), was found.
