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: 15VN166 # Created Fri Apr 19 01:17:52 2024 # Orbit generated from Bernstein formalism # Fitting 35 observations of 36 # Arc: 3.08y # First observation: 2014/11/17 # Last observation: 2017/12/16 Preliminary a, adot, b, bdot, g, gdot: 0.000482 0.028053 -0.000049 -0.002960 0.025581 0.000000 # Chi-squared of fit: 10.76 DOF: 64 RMS: 0.10 # Min/Max residuals: -0.31 0.19 # Exact a, adot, b, bdot, g, gdot: 1.703845E-05 2.904737E-02 -1.779984E-06 -3.064796E-03 2.618387E-02 9.917822E-03 # Covariance matrix: 3.8857E-13 -4.4414E-13 -1.9686E-14 3.5621E-14 -1.7452E-13 -3.8793E-12 -4.4414E-13 6.6535E-13 3.4090E-14 -6.1664E-14 2.7880E-13 6.7175E-12 -1.9686E-14 3.4090E-14 1.8977E-13 -1.0244E-13 1.5809E-14 3.8326E-13 3.5621E-14 -6.1664E-14 -1.0244E-13 7.4199E-14 -2.8715E-14 -6.9326E-13 -1.7452E-13 2.7880E-13 1.5809E-14 -2.8715E-14 2.7022E-13 3.1163E-12 -3.8793E-12 6.7175E-12 3.8326E-13 -6.9326E-13 3.1163E-12 7.5523E-11 # lat0 lon0 xBary yBary zBary JD0 -0.050014 47.646433 -0.119648 -0.000699 -0.982196 2456978.906378 # Heliocentric elements and errors Epoch: 2456970.5000 = 2014/11/09 Mean Anomaly: 21.40613 +/- 0.013 Argument of Peri: 119.38351 +/- 0.020 Long of Asc Node: 227.36330 +/- 0.000 Inclination: 6.02840 +/- 0.001 Eccentricity: 0.47983743 +/- 0.0003 Semi-Major Axis: 62.69786794 +/- 0.0260 Time of Perihelion: 2446188.1567 +/- 0.8 Perihelion: 32.61308414 +/- 0.0244 Aphelion: 92.78265173 +/- 0.0435 Period (y) 496.4635 +/- 0.31 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 26.29986673 +/- 0.0005 Ecliptic Y 29.03150641 +/- 0.0006 Ecliptic Z -0.03343084 +/- 0.0000 Ecliptic XDOT -0.00155035 +/- 0.0000 Ecliptic YDOT 0.00280741 +/- 0.0000 Ecliptic ZDOT -0.00032127 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 39.17285376 +/- 0.0005 Geocenter to KBO 38.19145402 +/- 0.0008 # Hcoef: 9.18
The following table shows the complete astrometric record for 15VN166. 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 (15VN166) followed by the observatory code and reference code for the source of the astrometry.
2014 11 17.40560 03 00 47.436 +17 02 49.39 25.2r 15VN166 568 C~2lVf 2014 11 17.51968 03 00 46.846 +17 02 46.73 25.2r 15VN166 568 C~2lVf 2014 11 23.41643 03 00 17.096 +17 00 31.44 24.9r 15VN166 568 C~2lVf 2015 08 11.57225 03 12 19.708 +17 42 02.28 24.5w 15VN166 568 C~2lVf 2015 09 06.61892 03 12 18.016 +17 41 03.41 25.5w 15VN166 568 C~2lVf 2015 10 08.44583 03 10 50.140 +17 34 12.32 25.6w 15VN166 568 C~2lVf 2015 10 08.50488 03 10 49.905 +17 34 11.15 25.4w 15VN166 568 C~2lVf 2015 11 07.35377 03 08 29.994 +17 23 56.06 25.2r 15VN166 568 C~2lVf 2015 11 07.39585 03 08 29.779 +17 23 55.13 25.1r 15VN166 568 C~2lVf 2015 11 07.43803 03 08 29.566 +17 23 54.17 24.9r 15VN166 568 C~2lVf 2015 11 10.52298 03 08 13.721 +17 22 44.92 25.3w 15VN166 568 C~2lVf 2015 11 17.36965 03 07 38.600 +17 20 11.29 25.4w 15VN166 568 C~2lVf 2015 11 17.41626 03 07 38.370 +17 20 10.14 25.0w 15VN166 568 C~2lVf 2015 12 06.37850 03 06 05.737 +17 13 22.68 25.3w 15VN166 568 C~2lVf 2015 12 13.31287 03 05 35.460 +17 11 08.27 25.4w 15VN166 568 C~2lVf 2015 12 13.37141 03 05 35.215 +17 11 06.87 25.1w 15VN166 568 C~2lVf 2016 01 01.36607 03 04 28.691 +17 06 06.24 25.6w 15VN166 568 C~2lVf 2016 01 07.31283 03 04 13.910 +17 04 56.88 25.0w 15VN166 568 C~2lVf 2016 02 04.28927 03 03 51.023 +17 02 45.13 25.3w 15VN166 568 C~2lVf 2016 02 10.27908 03 03 56.709 +17 03 01.44 25.1w 15VN166 568 C~2lVf 2016 09 06.61138 03 18 52.608 +17 56 01.22 25.1w 15VN166 568 C~2lVf 2016 10 10.40808 03 17 19.369 +17 48 52.35 24.9w 15VN166 568 C~2lVf 2016 10 10.46643 03 17 19.111 +17 48 51.32 25.4w 15VN166 568 C~2lVf 2016 10 27.49100 03 16 02.674 +17 43 23.61 25.7w 15VN166 568 C~2lVf 2016 10 27.50259 03 16 02.607 +17 43 23.40 26.1w 15VN166 568 C~2lVf 2016 11 02.59707 03 15 32.500 +17 41 15.76 25.9w 15VN166 568 C~2lVf 2016 11 02.60863 03 15 32.446 +17 41 15.48 25.6w 15VN166 568 C~2lVf 2016 11 03.51606 03 15 27.882 +17 40 55.95 25.5w 15VN166 568 C~2lVf 2016 11 03.52763 03 15 27.822 +17 40 55.75 25.3w 15VN166 568 C~2lVf 2016 12 29.37514 03 11 14.658 +17 22 59.05 25.5w 15VN166 568 C~2lVf 2017 01 02.38235 03 11 03.025 +17 22 07.90 24.9w 15VN166 568 C~2lVf 2017 01 26.27742 03 10 24.545 +17 19 09.14 25.9w 15VN166 568 C~2lVf 2017 09 15.58856 03 25 07.482 +18 08 46.09 15VN166 568 C~2lVf 2017 09 22.57478 03 24 51.657 +18 07 31.62 15VN166 568 C~2lVf 2017 12 16.34929 03 18 36.352 +17 41 35.16 25.7w 15VN166 568 C~2lVf 2017 12 16.36856 03 18 36.273 +17 41 34.76 25.5w 15VN166 568 C~2lVf
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 0.10 0.00 -0.01
2 0.0003 -8.87 0.13 -0.18 -0.02
3 0.0165 -456.38 -0.11 -10.30 -0.05
4 0.7315 10184.28 -0.10 -443.64 -0.02
5 0.8028 10145.22 0.17 -494.03 0.10
6 0.8899 8822.03 -0.02 -555.01 -0.00
7 0.8901 8818.48 0.02 -555.24 -0.15
8 0.9718 6722.09 -0.12 -608.59 0.09
9 0.9719 6718.87 -0.06 -608.65 0.08
10 0.9720 6715.67 0.02 -608.75 0.04
11 0.9805 6478.34 -0.17 -613.96 0.05
12 0.9992 5952.21 -0.08 -625.32 0.16
13 0.9993 5948.73 0.06 -625.53 0.01
14 1.0513 4560.20 -0.00 -655.58 0.05
15 1.0702 4105.94 0.08 -665.93 0.11
16 1.0704 4102.18 0.06 -666.31 -0.21
17 1.1224 3102.43 -0.14 -693.04 0.07
18 1.1387 2879.55 -0.05 -701.23 -0.08
19 1.2153 2527.67 0.01 -737.16 -0.01
20 1.2317 2610.56 ( 0.18) -744.04 ( 0.60)
21 1.8048 15842.03 -0.02 -1104.04 0.19
22 1.8973 14437.79 0.18 -1174.21 -0.10
23 1.8975 14433.95 -0.06 -1174.24 -0.05
24 1.9441 13289.26 -0.03 -1206.27 -0.06
25 1.9441 13288.28 -0.16 -1206.23 0.00
26 1.9608 12837.85 0.12 -1216.87 0.12
27 1.9609 12837.03 0.18 -1216.94 0.07
28 1.9633 12768.71 -0.03 -1218.70 -0.11
29 1.9634 12767.82 -0.03 -1218.67 -0.06
30 2.1163 8980.29 -0.05 -1298.31 -0.11
31 2.1272 8805.81 0.14 -1303.04 -0.31
32 2.1927 8226.11 0.06 -1327.57 0.03
33 2.8287 21252.01 0.02 -1723.14 0.01
34 2.8478 21012.49 -0.07 -1738.95 0.02
35 3.0799 15392.18 -0.03 -1883.17 0.12
36 3.0800 15390.98 -0.02 -1883.26 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.
15VN166 quality flag:3 Type: 3:1EE 3:1EE 3:1EE Type: 3:1II axisobj 63.761 63.840 63.683 ecceobj 0.489 0.490 0.488 incobj 6.014 6.014 6.014 qmin 31.619 31.756 31.494 qmax 95.447 95.401 95.564 amean 62.631 62.631 62.631 amin 61.717 61.713 61.841 amax 63.854 63.919 63.882 emean 0.484 0.481 0.484 emin 0.471 0.470 0.471 emax 0.495 0.494 0.496 imean 6.011 6.812 5.632 imin 5.556 6.399 4.439 imax 6.967 7.258 6.966 excite_mean 0.495 0.496 0.494 fracstop 1.000 1.000 1.000 cjmean 2.991 2.991 2.992 libcent 0 73.2 80.3 70.0 libamp 0 30.0 47.1 18.3 libcent 1 -180.0 -180.0 275.4 libamp 1 -180.0 -180.0 51.0 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 146.1 198.0 103.7 kozaiamp 34.6 83.0 18.6