The dynamics of asteroids near mean motion resonances is considered in the
paper. Results of study of orbital evolution of NEAs 2608 Seneca, 3103 Eger
, 3838 Epona, 1994 RE, 1994 CB are presented. Equations of the motion of as
teroids have been integrated numerically. In the process of numerical integ
ration perturbations from planets and the Moon have been taken into account
. The interval of time is ranging from -3000 to 3000 yr. Evolution of ensem
bles of 100 test particles with orbital elements nearby their nominal orbit
s has been considered for each object. (C) 2001 Elsevier Science Ltd. All r
ights reserved.