YR/MON/DAY/HOUR JD RA(1950), DEC(1950), DELTA DELTADOT R RDOT THETA BETA MOON PSANG PSAMV (UT) (MIN/HOUR) (ARCMIN/HOUR) ------------------------------------------------------------------------------------------------------------------------------ 1986 7 29 0.0 2446640.50 10 48.685( 0.025) -5 43.20(-0.12) 3.4954 41.7115 2.8267 21.2136 42.2 14.0 126.2 126.7 90.5 1986 7 30 0.0 2446641.50 10 49.284( 0.025) -5 46.01(-0.12) 3.5194 41.3255 2.8390 21.1758 41.4 13.7 114.9 127.1 90.7 1986 7 31 0.0 2446642.50 10 49.883( 0.025) -5 48.89(-0.12) 3.5431 40.9357 2.8512 21.1382 40.7 13.4 103.7 127.5 90.9 1986 8 1 0.0 2446643.50 10 50.485( 0.025) -5 51.83(-0.12) 3.5667 40.5423 2.8634 21.1008 39.9 13.2 92.4 127.9 91.1 ------------------------------------------------------------------------------------------------------------------------------ |----------------------------------------------------------------------------------------------------------------| | NOTE: Above ephemerides represent fully-perturbed, light-time-corrected solutions to data spanning 1835-1989 | | (cf. the EPHEM.TXT file by D. Yeomans in the DOCUMENT directory). Ephemerides for HOUR=0.0 UT are directly | | from Yeomans; values within a UT day have been generated using a 7-point interpolation scheme and Yeomans' | | daily (0h UT) values. The first and last lines in the table span the time interval between the beginning of | | this data directory and the beginning of the next one. | |----------------------------------------------------------------------------------------------------------------| DEFINITIONS OF LESS OBVIOUS FIELDS IN THE EPHEMERIS TABLE: THETA = Sun-Earth-Comet angle (degrees) BETA = Sun-Comet-Earth angle (degrees) MOON = Angular separation of comet and moon (degrees) PSANG = Position angle of prolonged radius vector (degrees, measured from north through east) PSAMV = Position angle of minus orbital velocity vector (degrees, measured from north through east) ---------------------------------------------------------------------------------------------------------------