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: 14QT510 # Created Fri Apr 19 01:16:15 2024 # Orbit generated from Bernstein formalism # Fitting 34 observations of 34 # Arc: 4.19y # First observation: 2014/08/29 # Last observation: 2018/11/08 Preliminary a, adot, b, bdot, g, gdot: 0.000505 0.035847 0.000156 0.007887 0.031530 0.000000 # Chi-squared of fit: 10.95 DOF: 62 RMS: 0.10 # Min/Max residuals: -0.35 0.24 # Exact a, adot, b, bdot, g, gdot: 1.770123E-05 3.683923E-02 3.887891E-06 8.195145E-03 3.161904E-02 4.269418E-03 # Covariance matrix: 2.0992E-13 -1.2269E-13 5.1985E-15 -4.2704E-14 2.7206E-13 -7.4259E-13 -1.2269E-13 2.9861E-13 -5.1169E-14 5.1854E-14 4.2718E-13 1.9291E-12 5.1985E-15 -5.1169E-14 1.4302E-13 -5.3066E-14 -1.4050E-13 -3.2920E-13 -4.2704E-14 5.1854E-14 -5.3066E-14 4.9993E-14 -1.1223E-13 4.7236E-13 2.7206E-13 4.2718E-13 -1.4050E-13 -1.1223E-13 3.3186E-12 1.5792E-12 -7.4259E-13 1.9291E-12 -3.2920E-13 4.7236E-13 1.5792E-12 1.4437E-11 # lat0 lon0 xBary yBary zBary JD0 -26.475559 -61.997882 -0.615540 -0.358420 -0.719913 2456898.560488 # Heliocentric elements and errors Epoch: 2456890.5000 = 2014/08/21 Mean Anomaly: 28.87159 +/- 0.025 Argument of Peri: 250.19564 +/- 0.039 Long of Asc Node: 1.17628 +/- 0.001 Inclination: 28.74884 +/- 0.000 Eccentricity: 0.22164088 +/- 0.0002 Semi-Major Axis: 39.37147704 +/- 0.0113 Time of Perihelion: 2449653.8237 +/- 5.4 Perihelion: 30.64514836 +/- 0.0109 Aphelion: 48.09780571 +/- 0.0153 Period (y) 247.0477 +/- 0.11 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 14.21079263 +/- 0.0008 Ecliptic Y -25.41484278 +/- 0.0014 Ecliptic Z -14.09948864 +/- 0.0008 Ecliptic XDOT 0.00311549 +/- 0.0000 Ecliptic YDOT 0.00092179 +/- 0.0000 Ecliptic ZDOT 0.00047049 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 32.35207012 +/- 0.0012 Geocenter to KBO 31.62651029 +/- 0.0018 # Hcoef: 8.03
The following table shows the complete astrometric record for 14QT510. 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 (14QT510) followed by the observatory code and reference code for the source of the astrometry.
2014 08 29.05971 20 29 59.012 -46 20 10.70 22.6i 14QT510 W84 C~4yU0 2014 08 29.05971 20 29 59.02 -46 20 10.6 23.2i 14QT510 W84 C~3cnQ 2014 08 29.06111 20 29 58.990 -46 20 10.84 23.3g 14QT510 W84 C~4yU0 2014 09 12.03252 20 28 30.248 -46 14 54.45 23.3r 14QT510 W84 C~4yU0 2014 09 12.03252 20 28 30.25 -46 14 54.4 23.2r 14QT510 W84 C~3cnQ 2014 09 19.99626 20 27 50.518 -46 10 35.06 23.2r 14QT510 W84 C~4yU0 2014 09 19.99626 20 27 50.52 -46 10 35.1 23.6r 14QT510 W84 C~3cnQ 2015 09 12.06656 20 39 15.154 -45 12 51.38 23.6r 14QT510 W84 C~4yU0 2015 09 12.06656 20 39 15.15 -45 12 51.4 23.6r 14QT510 W84 C~3cnQ 2015 09 13.06053 20 39 09.477 -45 12 25.77 23.1r 14QT510 W84 C~4yU0 2015 09 13.06053 20 39 09.48 -45 12 25.8 23.2r 14QT510 W84 C~3cnQ 2015 09 13.06190 20 39 09.470 -45 12 25.75 22.9i 14QT510 W84 C~4yU0 2015 09 13.06190 20 39 09.47 -45 12 25.7 23.1i 14QT510 W84 C~3cnQ 2015 09 13.06327 20 39 09.469 -45 12 25.70 23.7g 14QT510 W84 C~4yU0 2015 09 13.06327 20 39 09.47 -45 12 25.7 23.8g 14QT510 W84 C~3cnQ 2016 09 08.14736 20 49 49.213 -44 08 43.17 23.8g 14QT510 W84 C~4yU0 2016 09 09.06602 20 49 43.509 -44 08 25.23 22.7z 14QT510 W84 C~4yU0 2016 09 09.08642 20 49 43.358 -44 08 25.08 22.8i 14QT510 W84 C~4yU0 2016 09 24.99391 20 48 20.195 -44 01 15.13 22.9i 14QT510 W84 C~4yU0 2016 09 24.99391 20 48 20.19 -44 01 15.2 23.1i 14QT510 W84 C~3cnQ 2016 10 02.04368 20 47 54.037 -43 56 54.50 23.7r 14QT510 W84 C~4yU0 2016 10 02.04368 20 47 54.04 -43 56 54.5 23.7r 14QT510 W84 C~3cnQ 2017 09 12.08228 20 59 13.706 -42 59 36.46 23.8r 14QT510 W84 C~4yU0 2017 09 12.08365 20 59 13.692 -42 59 36.21 23.7g 14QT510 W84 C~4yU0 2017 09 23.04368 20 58 14.657 -42 55 13.86 23.2r 14QT510 W84 C~4yU0 2017 09 23.04506 20 58 14.640 -42 55 13.82 23.3g 14QT510 W84 C~4yU0 2017 09 23.99767 20 58 10.200 -42 54 46.06 22.9z 14QT510 W84 C~4yU0 2017 09 25.99568 20 58 01.258 -42 53 44.80 22.5i 14QT510 W84 C~4yU0 2017 10 17.09018 20 57 01.195 -42 39 43.08 23.1i 14QT510 W84 C~4yU0 2017 10 17.09155 20 57 01.183 -42 39 43.10 23.0r 14QT510 W84 C~4yU0 2017 10 17.13316 20 57 01.141 -42 39 41.02 24.0g 14QT510 W84 C~4yU1 2018 09 10.20149 21 08 47.139 -41 49 57.31 23.1g 14QT510 W84 C~4yU1 2018 10 28.06188 21 06 05.119 -41 22 43.07 22.5i 14QT510 W84 C~4yU1 2018 11 08.06878 21 06 15.172 -41 12 42.53 23.1r 14QT510 W84 C~4yU1
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 0.15 0.00 0.04
2 0.0000 -0.11 0.04 -0.07 -0.03
3 0.0000 -0.36 -0.12 -0.15 -0.15
4 0.0383 -801.57 -0.04 551.38 0.02
5 0.0383 -801.54 -0.00 551.42 0.07
6 0.0601 -1130.48 -0.04 910.75 0.03
7 0.0601 -1130.49 -0.05 910.79 0.08
8 1.0377 6729.17 0.02 2217.77 0.04
9 1.0377 6729.22 0.07 2217.78 0.04
10 1.0404 6679.56 -0.01 2260.09 -0.03
11 1.0404 6679.54 -0.03 2260.13 0.01
12 1.0404 6679.49 -0.01 2260.22 0.04
13 1.0404 6679.48 -0.03 2260.17 -0.01
14 1.0404 6679.49 0.05 2260.22 -0.02
15 1.0404 6679.48 0.04 2260.22 -0.02
16 2.0290 14379.60 0.14 3754.42 -0.03
17 2.0315 14327.29 0.14 3791.63 0.19
18 2.0316 14325.79 -0.17 3792.30 0.03
19 2.0751 13616.40 -0.17 4492.85 -0.12
20 2.0751 13616.48 -0.09 4492.90 -0.07
21 2.0944 13433.31 0.06 4831.71 -0.08
22 2.0944 13433.28 0.03 4831.72 -0.07
23 3.0391 21622.45 -0.06 5563.63 -0.35
24 3.0391 21622.40 -0.04 5563.92 -0.11
25 3.0691 21104.29 0.06 6041.04 0.11
26 3.0691 21104.13 -0.05 6041.14 0.15
27 3.0717 21067.96 -0.09 6084.53 -0.04
28 3.0772 20996.98 -0.02 6176.94 0.03
29 3.1349 20671.08 0.13 7202.83 0.06
30 3.1349 20670.95 -0.01 7202.86 0.02
31 3.1350 20671.25 0.17 7204.99 0.03
32 4.0332 29186.54 -0.29 7132.12 -0.08
33 4.1643 28106.56 0.24 9353.64 0.14
34 4.1944 28444.51 -0.01 9875.17 0.07
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.
14QT510 quality flag:3 Type: 3:2E 3:2E 3:2E axisobj 39.346 39.382 39.311 ecceobj 0.220 0.221 0.220 incobj 28.743 28.743 28.742 qmin 28.009 28.542 27.677 qmax 51.444 51.133 51.756 amean 39.454 39.454 39.454 amin 38.952 38.928 38.972 amax 40.038 40.075 40.022 emean 0.249 0.248 0.255 emin 0.207 0.210 0.203 emax 0.288 0.276 0.296 imean 28.449 28.501 28.280 imin 27.505 27.782 27.243 imax 29.398 29.312 29.426 excite_mean 0.538 0.538 0.538 fracstop 1.000 1.000 1.000 cjmean 2.711 2.711 2.711 libcent 0 180.6 179.7 180.4 libamp 0 115.5 122.3 106.7 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 268.4 269.2 266.0 kozaiamp 34.8 30.7 36.7