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: 14QV495 # Created Sat Apr 20 01:16:10 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 35 observations of 35 # Arc: 5.42y # First observation: 2014/08/19 # Last observation: 2020/01/18 # Chi-squared of fit: 73.17 DOF: 64 RMS: 0.26 # Min/Max residuals: -0.80 1.64 # Exact a, adot, b, bdot, g, gdot: 1.966383E-05 3.358809E-02 4.977403E-06 7.533913E-03 2.733559E-02 5.463407E-03 # Covariance matrix: 1.4543E-13 -6.8104E-14 9.1159E-15 -1.8218E-14 7.8910E-14 -4.8403E-13 -6.8104E-14 2.0593E-13 -2.1077E-14 5.3573E-14 4.9474E-14 1.5243E-12 9.1159E-15 -2.1077E-14 6.9846E-14 -3.1880E-14 -4.0073E-16 -1.8665E-13 -1.8218E-14 5.3573E-14 -3.1880E-14 4.3444E-14 7.6238E-15 4.6576E-13 7.8910E-14 4.9474E-14 -4.0073E-16 7.6238E-15 1.3473E-13 2.6273E-13 -4.8403E-13 1.5243E-12 -1.8665E-13 4.6576E-13 2.6273E-13 1.3192E-11 # lat0 lon0 xBary yBary zBary JD0 -20.531123 12.368833 0.733547 -0.245810 -0.656727 2456888.834488 # Heliocentric elements and errors Epoch: 2456888.5000 = 2014/08/19 Mean Anomaly: 5.74018 +/- 0.004 Argument of Peri: 277.12970 +/- 0.014 Long of Asc Node: 69.24002 +/- 0.001 Inclination: 23.38109 +/- 0.000 Eccentricity: 0.54276954 +/- 0.0001 Semi-Major Axis: 79.24984417 +/- 0.0165 Time of Perihelion: 2452779.6597 +/- 2.9 Perihelion: 36.23544253 +/- 0.0113 Aphelion: 122.26424582 +/- 0.0268 Period (y) 705.5143 +/- 0.22 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 34.30325503 +/- 0.0005 Ecliptic Y 6.77425145 +/- 0.0001 Ecliptic Z -12.82985119 +/- 0.0002 Ecliptic XDOT 0.00003356 +/- 0.0000 Ecliptic YDOT 0.00344816 +/- 0.0000 Ecliptic ZDOT 0.00051485 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 37.24515179 +/- 0.0004 Geocenter to KBO 36.58225747 +/- 0.0005 # Hcoef: 6.86
The following table shows the complete astrometric record for 14QV495. 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 (14QV495) followed by the observatory code and reference code for the source of the astrometry.
2014 08 19.33371 01 17 54.975 -14 00 12.86 23.1g 14QV495 W84 C~4yTz 2014 08 19.33371 01 17 54.98 -14 00 12.9 23.1g 14QV495 W84 C~3cnP 2014 08 19.33507 01 17 54.977 -14 00 12.85 22.0z 14QV495 W84 C~4yTz 2014 08 19.33507 01 17 54.98 -14 00 12.9 22.0z 14QV495 W84 C~3cnP 2014 08 19.33618 01 17 54.971 -14 00 12.78 22.3Y 14QV495 W84 C~4yTz 2014 09 16.25983 01 16 15.901 -14 17 33.06 21.7z 14QV495 W84 C~4yTz 2014 09 25.23259 01 15 34.207 -14 22 35.29 23.2g 14QV495 W84 C~4yTz 2014 09 25.23259 01 15 34.21 -14 22 35.3 23.4g 14QV495 W84 C~3cnP 2014 09 25.233437 01 15 34.20 -14 22 35.1 23.1r 14QV495 W84 C~35bt 2014 09 25.23533 01 15 34.192 -14 22 35.38 22.4i 14QV495 W84 C~4yTz 2014 09 25.23533 01 15 34.19 -14 22 35.4 22.4i 14QV495 W84 C~3cnP 2014 11 21.18686 01 11 02.047 -14 35 42.70 22.4i 14QV495 W84 C~4yTz 2014 11 21.18686 01 11 02.05 -14 35 42.7 22.4i 14QV495 W84 C~3cnP 2014 11 21.19377 01 11 02.018 -14 35 42.58 22.6r 14QV495 W84 C~4yTz 2014 11 21.19377 01 11 02.02 -14 35 42.6 22.8r 14QV495 W84 C~3cnP 2014 12 22.08427 01 09 48.246 -14 24 26.39 22.4i 14QV495 W84 C~4yTz 2014 12 22.08427 01 09 48.25 -14 24 26.4 22.4i 14QV495 W84 C~3cnP 2014 12 30.065336 01 09 44.27 -14 19 29.0 22.2z 14QV495 W84 C~35bt 2014 12 30.06586 01 09 44.259 -14 19 29.21 22.2z 14QV495 W84 C~4yTz 2015 09 13.27672 01 23 02.482 -13 05 29.30 22.5i 14QV495 W84 C~4yTz 2015 09 13.27672 01 23 02.48 -13 05 29.3 22.4i 14QV495 W84 C~3cnP 2015 09 13.27810 01 23 02.472 -13 05 29.38 22.3r 14QV495 W84 C~4yTz 2015 09 13.27810 01 23 02.47 -13 05 29.4 22.6r 14QV495 W84 C~3cnP 2015 09 13.27948 01 23 02.478 -13 05 29.38 23.3g 14QV495 W84 C~4yTz 2015 09 13.27948 01 23 02.48 -13 05 29.3 23.7g 14QV495 W84 C~3cnP 2015 09 23.26337 01 22 18.351 -13 11 12.34 22.8z 14QV495 W84 C~4yTz 2015 10 07.188530 01 21 10.35 -13 18 09.6 22.6r 14QV495 W84 C~35bt 2015 11 20.10905 01 17 40.484 -13 26 40.14 22.1z 14QV495 W84 C~4yTz 2015 11 20.10905 01 17 40.48 -13 26 40.1 22.1z 14QV495 W84 C~3cnP 2016 11 07.11352 01 24 59.170 -12 17 16.92 21.9z 14QV495 W84 C~4yTz 2016 11 07.11352 01 24 59.17 -12 17 16.9 21.9z 14QV495 W84 C~3cnP 2018 10 01.26729 01 40 34.244 -09 46 15.67 22.6z 14QV495 W84 C~4yTz 2018 11 16.08750 01 36 51.733 -09 59 37.30 22.8i 14QV495 W84 C~4yTz 2020 01 18.096920 01 40 50.016 -08 30 03.00 22.8G 14QV495 G37 C~3jSo 2020 01 18.177520 01 40 50.249 -08 29 59.81 14QV495 G37 C~3jSo
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 0.01 0.00 -0.14
2 0.0000 0.00 0.08 0.00 -0.18
3 0.0000 0.00 0.09 0.00 -0.08
4 0.0000 0.00 0.13 0.00 -0.13
5 0.0000 0.00 0.04 0.00 0.04
6 0.0765 0.00 -0.13 0.00 -0.05
7 0.1010 0.00 0.03 0.00 -0.03
8 0.1010 0.00 0.08 0.00 -0.04
9 0.1010 0.00 -0.01 0.00 0.19
10 0.1010 0.00 -0.02 0.00 -0.05
11 0.1010 0.00 0.01 0.00 -0.03
12 0.2570 0.00 0.04 0.00 -0.06
13 0.2570 0.00 -0.01 0.00 -0.06
14 0.2570 0.00 -0.02 0.00 -0.02
15 0.2570 0.00 -0.05 0.00 0.00
16 0.3415 0.00 0.05 0.00 -0.10
17 0.3415 0.00 -0.01 0.00 -0.09
18 0.3634 0.00 0.05 0.00 0.16
19 0.3634 0.00 -0.12 0.00 -0.07
20 1.0676 0.00 0.09 0.00 0.07
21 1.0676 0.00 0.12 0.00 0.07
22 1.0676 0.00 0.02 0.00 0.02
23 1.0676 0.00 0.05 0.00 0.04
24 1.0676 0.00 0.26 0.00 0.17
25 1.0676 0.00 0.23 0.00 0.09
26 1.0949 0.00 -0.01 0.00 0.17
27 1.1331 0.00 -0.37 0.00 0.11
28 1.2533 0.00 -0.06 0.00 0.09
29 1.2533 0.00 -0.00 0.00 0.05
30 2.2198 0.00 -0.16 0.00 0.14
31 2.2198 0.00 -0.16 0.00 0.12
32 4.1175 0.00 -0.41 0.00 -0.17
33 4.2430 0.00 -0.49 0.00 -0.12
34 5.4148 0.00 -0.80 0.00 0.04
35 5.4150 0.00 1.64 0.00 -0.09
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.
14QV495 quality flag:3 Type: SCATNEAR SCATNEAR SCATNEAR axisobj 80.809 80.809 80.809 ecceobj 0.552 0.552 0.552 incobj 23.385 23.385 23.385 qmin 35.457 35.533 35.534 qmax 126.329 126.666 126.389 amean 79.555 79.711 79.638 amin 78.184 78.526 78.447 amax 81.281 81.444 81.352 emean 0.536 0.537 0.537 emin 0.520 0.521 0.521 emax 0.554 0.556 0.555 imean 22.971 22.974 22.973 imin 22.000 21.990 22.023 imax 23.899 23.944 23.900 excite_mean 0.663 0.664 0.664 fracstop 1.000 1.000 1.000 cjmean 2.905 2.905 2.905 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 169.1 171.7 168.5 kozaiamp 180.0 179.9 180.0