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: 14QP562 # Created Sun Nov 24 02:09:56 2024 # Orbit generated from Bernstein formalism # Fitting 16 observations of 16 # Arc: 4.24y # First observation: 2014/08/19 # Last observation: 2018/11/15 Preliminary a, adot, b, bdot, g, gdot: 0.000284 0.033994 0.000011 -0.000114 0.027611 0.000000 # Chi-squared of fit: 4.71 DOF: 26 RMS: 0.10 # Min/Max residuals: -0.25 0.21 # Exact a, adot, b, bdot, g, gdot: 1.990259E-05 3.435583E-02 -1.577879E-07 -9.336090E-05 2.739773E-02 4.786368E-03 # Covariance matrix: 5.0076E-13 -2.6617E-13 2.5517E-15 -1.7211E-15 7.9589E-14 -1.4883E-12 -2.6617E-13 7.7810E-13 4.1828E-15 -3.5320E-15 6.1576E-13 6.1141E-12 2.5517E-15 4.1828E-15 4.1176E-13 -1.4217E-13 1.2646E-14 1.5115E-14 -1.7211E-15 -3.5320E-15 -1.4217E-13 6.3516E-14 -9.4827E-15 -1.5497E-14 7.9589E-14 6.1576E-13 1.2646E-14 -9.4827E-15 1.0451E-12 4.0917E-12 -1.4883E-12 6.1141E-12 1.5115E-14 -1.5497E-14 4.0917E-12 5.4994E-11 # lat0 lon0 xBary yBary zBary JD0 -24.874459 -4.517111 0.498716 -0.371642 -0.801867 2456888.802848 # Heliocentric elements and errors Epoch: 2456880.5000 = 2014/08/11 Mean Anomaly: 5.67263 +/- 0.009 Argument of Peri: 247.80857 +/- 0.033 Long of Asc Node: 86.12474 +/- 0.001 Inclination: 24.30982 +/- 0.000 Eccentricity: 0.52119368 +/- 0.0002 Semi-Major Axis: 76.16385343 +/- 0.0239 Time of Perihelion: 2453054.8657 +/- 5.5 Perihelion: 36.46773433 +/- 0.0167 Aphelion: 115.85997253 +/- 0.0384 Period (y) 664.7090 +/- 0.31 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 33.85012156 +/- 0.0012 Ecliptic Y -3.17245149 +/- 0.0001 Ecliptic Z -15.35279061 +/- 0.0006 Ecliptic XDOT 0.00069417 +/- 0.0000 Ecliptic YDOT 0.00338435 +/- 0.0000 Ecliptic ZDOT -0.00020953 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 37.30420027 +/- 0.0011 Geocenter to KBO 36.49937193 +/- 0.0014 # Hcoef: 7.79
The following table shows the complete astrometric record for 14QP562. 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 (14QP562) followed by the observatory code and reference code for the source of the astrometry.
2014 08 19.30207 00 25 40.754 -24 28 40.67 23.4r 14QP562 W84 C~52Tr 2014 08 19.30343 00 25 40.754 -24 28 40.60 24.1g 14QP562 W84 C~52Tr 2014 09 25.20616 00 22 48.951 -24 52 34.22 23.9g 14QP562 W84 C~52Tr 2016 09 06.38227 00 39 40.478 -22 58 11.09 23.3r 14QP562 W84 C~52Tr 2016 09 06.38366 00 39 40.458 -22 58 11.17 23.5g 14QP562 W84 C~52Tr 2016 10 28.13808 00 35 23.067 -23 18 43.39 24.6g 14QP562 W84 C~52Tr 2016 11 04.11642 00 34 52.577 -23 18 36.60 23.7r 14QP562 W84 C~52Tr 2016 11 04.23780 00 34 52.062 -23 18 36.21 23.4i 14QP562 W84 C~52Tr 2016 11 07.23051 00 34 39.922 -23 18 18.81 24.4g 14QP562 W84 C~52Tr 2017 09 24.27680 00 45 40.046 -22 15 46.10 23.2i 14QP562 W84 C~52Tr 2017 09 24.27818 00 45 40.042 -22 15 46.21 23.3r 14QP562 W84 C~52Tr 2017 09 26.22911 00 45 30.165 -22 16 46.82 23.5r 14QP562 W84 C~52Tr 2017 09 26.23049 00 45 30.161 -22 16 46.92 23.3i 14QP562 W84 C~52Tr 2017 10 21.13016 00 43 23.232 -22 25 31.22 24.7g 14QP562 W84 C~52Tr 2017 10 22.20104 00 43 18.016 -22 25 42.27 22.5z 14QP562 W84 C~52Tr 2018 11 15.15184 00 48 50.561 -21 32 34.86 23.5i 14QP562 W84 C~52Tr
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 -0.02 0.00 0.02
2 0.0000 0.03 0.10 0.06 0.11
3 0.1010 -2731.78 -0.05 -277.17 -0.01
4 2.0509 12757.85 0.01 -295.80 -0.10
5 2.0509 12757.56 -0.17 -295.74 -0.03
6 2.1926 9024.64 -0.03 220.56 -0.11
7 2.2117 8652.08 0.05 416.08 0.08
8 2.2120 8645.91 -0.03 419.62 -0.07
9 2.2202 8504.16 -0.03 510.51 -0.25
10 3.0992 18381.33 0.02 -340.42 0.13
11 3.0992 18381.23 0.02 -340.49 0.05
12 3.1045 18230.51 0.05 -330.10 0.08
13 3.1045 18230.41 0.06 -330.16 0.01
14 3.1727 16414.86 -0.08 25.32 0.21
15 3.1756 16345.21 0.19 49.09 -0.08
16 4.2405 21972.28 -0.09 710.66 -0.06
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.
14QP562 quality flag:3 Type: SCATNEAR SCATNEAR SCATNEAR axisobj 77.473 77.553 77.393 ecceobj 0.529 0.530 0.529 incobj 24.324 24.324 24.324 qmin 35.646 35.560 35.646 qmax 120.693 120.604 120.066 amean 76.980 76.856 76.618 amin 75.676 75.740 75.527 amax 78.661 78.472 78.202 emean 0.520 0.520 0.518 emin 0.503 0.504 0.501 emax 0.535 0.537 0.535 imean 23.364 23.229 23.351 imin 22.513 22.435 22.519 imax 24.294 24.240 24.293 excite_mean 0.654 0.653 0.652 fracstop 1.000 1.000 1.000 cjmean 2.899 2.899 2.899 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 169.5 171.9 175.5 kozaiamp 180.0 180.0 180.0