object1. .name = '410777' ! Object name .obs_dir = 'mpcobs' ! Observations directory .inc_files = 'epoch/410777.eq0' ! Input file output. .elements='EQU' ! Output elements operations. .init_orbdet = 0 ! Initial orbit determination ! (0 = no, 1 = yes) .diffcor = 1 ! Differential correction ! (0 = no, 1 = yes) .ident = 0 ! Orbit identification ! (0 = no, 1 = yes) .ephem = 0 ! Ephemerides ! (0 = no, 1 = yes) error_model. .name='fcct14' ! Error model propag. .iast=17 ! 0=no asteroids with mass, n=no. of massive asteroids (def=0) .filbe='AST17' ! name of the asteroid ephemerides file (def='CPV') .npoint=600 ! minimum number of data points for a deep close appr (def=100) .dmea=0.2d0 ! min. distance for control of close-app. to the Earth only (def=0.1) .dter=0.05d0 ! min. distance for control of close-app. ! to terrestrial planets (MVM)(def=0.1) .yark_exp=2.d0 ! A2/r^yark_exp model (def=2) .ngr_opt=.TRUE. ! Reading from option file/orbit file .iyark=3 ! Including the Yarkovsky effect in the dynamical model ! (0 = no, 3=secula acceleration) (def=0) .det_drp=2 ! Solving-for the Yarkovsky effect ! (0=no non-grav perturbations, 1=A/M, 2=Yarko, 3=both) ! (def=0) .irel=2 ! Relativity difcor. .yarko_apriori=.TRUE. ! A priori value adopted (def=FALSE) .yarko_nominal=0.d0 ! Nominal value (def = 0.d0) .yarko_std=3.25d-4 ! Standard deviation (no default) IERS. .extrapolation=.T. ! extrapolation of Earth rotation reject. .rejopp=.FALSE. ! reject entire opposition