=============================================================================== File: 1986_kiseleva.data.txt ============================ Contents: - 6 observations made from 1986 Jul. 2 to Aug. 5 References: Kiseleva, T.P., Chanturiia, S.M.: 1988, Photographic positional observations of Phobos at Abastumani in 1986 (In Russian). Abastumanskaia Astrofizicheskaia Observatoriia, Biulleten' (ISSN 0375-6644), n. 63, p. 31-34 Format: Colums Entry 1 Acceptance code - A = Accepted data - D = Deleted (bad quality) data 3-4 Opposition number - 1877 = 1, 1982 = 50 6-19 Observation time (UTC), Not light-time corrected, with the form YYYYMMDD.DDDDD 21-23 (ET-UTC) in tenths of second 25-26 Observer code: Kiseleva = 32 28-30 Observatory code: Abastuman = 119 32 Observed body - 1 = Phobos relative to Mars - 2 = Deimos relative to Mars - 3 = Deimos relative to Phobos 34 Obs. type - 0 = separation and/or position angle - 1 = differential R.A.(*cosine(dec.)) and/or differential declination - 2 = Delta a or Delta d 36 Ref. system - 1 = true equator and equinox of date - 2 = mean equator and equinox of B1900 - 3 = mean equator and equinox of B1950 39-45 1st observation of pair (seconds of arc) - blank if observation absent - see note 4. 48-54 2nd observation of pair (seconds of arc or degrees if position angle) - blank if observation absent - see notes 1 and 4. 58-61 1-sigma noise in 1st obs. of pair (seconds of arc) - blank if observation absent - see notes 3 and 4. 64-67 1-sigma noise in 2nd obs. of pair (seconds of arc) - blank if observation absent - see notes 2, 3 and 4. 70 Observation correction code - 1 = corrected for phase - 2 = corrected for differential refraction - 3 = both 1 and 2 Note 1. The units for the observations are seconds of arc except for position angle when the unit is degrees east of north in the range 0 - 360. Note 2. The units for the observation noise are always seconds of arc. For a position angle p, the noise refers to the product of the error in p and the separation angle. Note 3. In the ESOC system, when the noise is greater or equal to 99.0 the corresponding observation is of bad quality and is not used in the determination of the orbit but its residual is computed and printed. Note 4. When the observation is either Delta a or Delta d the columns normally used for the complementary observation are used to store the position angle, theta. Also, the columns normally used to store the noise of thre complementary observation contain 0.0. ===============================================================================