[OrbFit5.0 Options and Setup Files] An options file and a few setup files to get you up and running with Orbfit v5.0 #orbfit #ephemeris #orbital_elements #settings

dummy.obs

04067J38D01T* A2000 01 01.000   00 00.0     +00 00               00.0   BZ020024

orbfit-template-run-options.oop

!! MODE OF USE OPTIONS !!
operations.
    .init_orbdet = 0
    .diffcor = 0
    .ident = 0
    .ephem = 1

!! OBJECT 1 DETAILS !!
object1.
    .name = '1999 YQ10'
    .inc_name = '1999 YQ10'
    .obs_fname = dummy
    .obs_dir = .
    .inc_files = astorb.dat[BA2]

object2.
    .name = '1999 YQ10'
    .inc_name = '1999 YQ10'
    .obs_fname = dummy
    .obs_dir = .
    .inc_files = astorb.dat[BA2]

!! ORBITAL ELEMENT OPTIONS !!
output.
    .epoch = MJD 50982.94143519 UTC
    .elements = EQU
output_files.
    .elem = '1999 YQ10.oel'

!! EPHEMERIS OPTIONS !!
ephem.
    .objects = 1 2
    .epoch.start = MJD 57916.0 UTC
    .epoch.end = MJD 57916.0 UTC
    .step = 1.0
    .obscode = 500
    .timescale = UTC
    .fields = cal,mjd,coord,mag,delta,r,elong,phase,glat,appmot,skyerr

!! APPARENT MOTION FORMAT !!
ephem.appmot.
    .format = 'rectangular'
    .units = arcsec/s

!! ORBIT PROPAGATION OPTIONS !!
propag.
    .output_des = false
    .ab_mag = true
    .iast = 0
    .ilun = 1
    .imerc = 1
    .iplut = 1
    .irel  = 1
    .filbe = 'CPV' 
    .iclap = 1
    .iaber = 1
    .istat = 1
    .npoint= 100

error_model.
    .name='fcct14'      ! Error model