The following information shows the result of the orbit fit based on Gary Bernstein's method. Most of the information should be self-explanatory. Take special note that while the original Bernstein software works with barycentric coordinates, we convert these results into a heliocentric coordinate system.
# Object: 14SS403 # Created Sat Apr 27 01:16:24 2024 # Orbit generated from Bernstein formalism # Fitting 12 observations of 12 # Arc: 3.04y # First observation: 2014/09/24 # Last observation: 2017/10/10 Preliminary a, adot, b, bdot, g, gdot: 0.000117 0.027532 -0.000123 0.003511 0.026932 0.000000 # Chi-squared of fit: 5.05 DOF: 18 RMS: 0.11 # Min/Max residuals: -0.23 0.37 # Exact a, adot, b, bdot, g, gdot: 1.636805E-05 2.751719E-02 2.341202E-06 3.476805E-03 2.589968E-02 -7.828009E-04 # Covariance matrix: 2.9071E-13 -4.6801E-13 -1.6585E-14 -4.4999E-14 2.4482E-13 -4.5059E-12 -4.6801E-13 5.3424E-12 -3.8248E-14 7.0965E-13 -4.7935E-13 6.3604E-11 -1.6585E-14 -3.8248E-14 2.7732E-13 -1.0146E-13 -2.9423E-13 -5.6514E-13 -4.4999E-14 7.0965E-13 -1.0146E-13 1.5858E-13 2.9483E-14 8.5785E-12 2.4482E-13 -4.7935E-13 -2.9423E-13 2.9483E-14 3.2810E-12 -4.6352E-12 -4.5059E-12 6.3604E-11 -5.6514E-13 8.5785E-12 -4.6352E-12 7.6631E-10 # lat0 lon0 xBary yBary zBary JD0 -24.965063 -54.435775 -0.824654 -0.242871 -0.521993 2456924.549578 # Heliocentric elements and errors Epoch: 2456920.5000 = 2014/09/20 Mean Anomaly: 357.65319 +/- 0.372 Argument of Peri: 289.55979 +/- 0.491 Long of Asc Node: 18.70836 +/- 0.001 Inclination: 25.73441 +/- 0.000 Eccentricity: 0.13315384 +/- 0.0003 Semi-Major Axis: 45.14408840 +/- 0.0176 Time of Perihelion: 2457642.7292 +/- 114.5 Perihelion: 39.13297961 +/- 0.0192 Aphelion: 51.15519719 +/- 0.0231 Period (y) 303.3259 +/- 0.18 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 21.36204800 +/- 0.0014 Ecliptic Y -28.46066594 +/- 0.0020 Ecliptic Z -16.29609489 +/- 0.0011 Ecliptic XDOT 0.00240817 +/- 0.0000 Ecliptic YDOT 0.00162208 +/- 0.0000 Ecliptic ZDOT 0.00036823 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 39.13961304 +/- 0.0017 Geocenter to KBO 38.61051149 +/- 0.0027 # Hcoef: 7.36
The following table shows the complete astrometric record for 14SS403. The first three columns show the date of observation. The next six columns are RA and DEC. The next column (when provided) is the observed magnitude and filter. The next column is the object name (14SS403) followed by the observatory code and reference code for the source of the astrometry.
2014 09 24.04880 21 04 06.265 -42 53 20.80 22.9r 14SS403 W84 C~55S8 2014 09 26.03587 21 03 58.408 -42 52 37.38 24.0g 14SS403 W84 C~55S8 2014 10 02.07153 21 03 37.225 -42 50 07.63 22.8i 14SS403 W84 C~55S8 2014 10 19.08761 21 03 00.964 -42 40 51.47 24.2g 14SS403 W84 C~55S8 2014 10 22.02387 21 02 58.429 -42 38 57.86 23.5r 14SS403 W84 C~55S8 2014 10 26.02513 21 02 56.880 -42 36 15.28 23.4r 14SS403 W84 C~55S8 2016 08 23.23708 21 22 15.800 -41 29 23.64 23.1z 14SS403 W84 C~55S8 2017 09 12.09324 21 27 45.084 -40 43 00.94 23.7g 14SS403 W84 C~55S8 2017 09 12.11571 21 27 44.960 -40 43 00.73 23.0r 14SS403 W84 C~55S8 2017 10 10.09550 21 25 47.651 -40 35 01.53 23.7r 14SS403 W84 C~55S8 2017 10 10.09686 21 25 47.597 -40 35 01.66 23.1i 14SS403 W84 C~55S8 2017 10 10.09823 21 25 47.603 -40 35 01.58 23.7g 14SS403 W84 C~55S8
The following table shows the residuals to the orbit fit. The first coumn is the point number. The second column is the time, in years, measured from the first observation. The third and fifth columns are the regularized positions used in the orbit fit. The fourth and sixth columns are the residuals, in arc seconds, for RA and Dec respectively.
1 0.0000 0.00 0.09 0.00 -0.05
2 0.0054 -68.24 -0.03 68.45 0.02
3 0.0220 -242.16 -0.06 283.93 -0.06
4 0.0686 -447.00 0.17 937.27 0.12
5 0.0766 -438.04 -0.18 1053.93 0.01
6 0.0875 -403.46 0.01 1213.72 -0.07
7 1.9143 13116.35 -0.01 605.56 0.08
8 2.9680 17633.01 -0.03 1803.20 -0.10
9 2.9680 17631.78 -0.00 1803.93 -0.02
10 3.0446 16569.63 0.37 2754.63 -0.02
11 3.0446 16569.01 -0.23 2754.74 0.04
12 3.0446 16569.10 -0.11 2754.79 0.04
The following table comes from a 10My integration of the orbit of the object. Three columns are shown. The first column is the result of integrating the nominal orbit. The other two columns are based on clones of the nominal orbit that are +/- 3 sigma from the nominal orbit. If all three types agree then the classificiation is deemed secure. The basis for these calculations is described in more detail in AJ, 129, 1117 (2005). Any use made of these calculations should refer to and credit this publication and the Deep Ecliptic Survey Team.
14SS403 quality flag:3 Type: SCATEXTD SCATEXTD SCATEXTD axisobj 45.273 45.330 45.216 ecceobj 0.137 0.138 0.136 incobj 25.735 25.735 25.735 qmin 38.594 38.582 38.601 qmax 52.476 52.635 52.379 amean 45.387 45.444 45.308 amin 45.022 45.069 44.936 amax 45.779 45.852 45.720 emean 0.133 0.133 0.132 emin 0.119 0.120 0.118 emax 0.147 0.148 0.146 imean 25.647 25.652 25.640 imin 25.314 25.315 25.327 imax 25.984 25.985 25.976 excite_mean 0.453 0.453 0.452 fracstop 1.000 1.000 1.000 cjmean 2.857 2.858 2.857 libcent 0 -180.0 -180.0 -180.0 libamp 0 -180.0 -180.0 -180.0 libcent 1 -180.0 -180.0 -180.0 libamp 1 -180.0 -180.0 -180.0 libcent 2 -180.0 -180.0 -180.0 libamp 2 -180.0 -180.0 -180.0 libcent 3 -180.0 -180.0 -180.0 libamp 3 -180.0 -180.0 -180.0 libcent 4 -180.0 -180.0 -180.0 libamp 4 -180.0 -180.0 -180.0 kozaimean 174.4 174.0 174.2 kozaiamp 180.0 180.0 180.0