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: 14SQ373 # Created Thu Apr 25 01:16:12 2024 # Orbit generated from Bernstein formalism # Fitting 37 observations of 37 # Arc: 3.38y # First observation: 2014/09/24 # Last observation: 2018/02/09 Preliminary a, adot, b, bdot, g, gdot: 0.000056 0.024154 0.000018 0.001038 0.024216 0.000000 # Chi-squared of fit: 7.82 DOF: 68 RMS: 0.08 # Min/Max residuals: -0.30 0.19 # Exact a, adot, b, bdot, g, gdot: 1.573419E-05 2.405694E-02 6.378436E-07 1.062876E-03 2.405829E-02 -2.871037E-03 # Covariance matrix: 1.2400E-13 -5.7215E-16 1.2217E-14 -9.4149E-15 1.0064E-13 -1.6096E-13 -5.7215E-16 6.2149E-13 1.7259E-14 2.7052E-14 6.0689E-13 9.0864E-12 1.2217E-14 1.7259E-14 9.4955E-14 -4.6434E-14 3.8265E-14 -2.8204E-14 -9.4149E-15 2.7052E-14 -4.6434E-14 4.1866E-14 6.9116E-15 7.2770E-13 1.0064E-13 6.0689E-13 3.8265E-14 6.9116E-15 7.3442E-13 7.8975E-12 -1.6096E-13 9.0864E-12 -2.8204E-14 7.2770E-13 7.8975E-12 1.6331E-10 # lat0 lon0 xBary yBary zBary JD0 -30.334951 46.392240 0.716877 -0.356071 -0.608807 2456924.834788 # Heliocentric elements and errors Epoch: 2456920.5000 = 2014/09/20 Mean Anomaly: 310.12930 +/- 0.041 Argument of Peri: 339.30018 +/- 0.085 Long of Asc Node: 131.31999 +/- 0.001 Inclination: 29.90580 +/- 0.000 Eccentricity: 0.16131603 +/- 0.0005 Semi-Major Axis: 46.16439584 +/- 0.0100 Time of Perihelion: 2472791.4209 +/- 12.0 Perihelion: 38.71733877 +/- 0.0255 Aphelion: 53.61145290 +/- 0.0268 Period (y) 313.6671 +/- 0.10 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 25.74616154 +/- 0.0009 Ecliptic Y 25.99424891 +/- 0.0009 Ecliptic Z -20.99294672 +/- 0.0007 Ecliptic XDOT -0.00213932 +/- 0.0000 Ecliptic YDOT 0.00172370 +/- 0.0000 Ecliptic ZDOT 0.00026952 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 42.18138953 +/- 0.0009 Geocenter to KBO 41.56570913 +/- 0.0015 # Hcoef: 6.96
The following table shows the complete astrometric record for 14SQ373. 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 (14SQ373) followed by the observatory code and reference code for the source of the astrometry.
2014 09 24.33401 03 29 46.975 -12 24 11.56 23.2r 14SQ373 W84 C~4yUX 2014 09 24.33401 03 29 46.98 -12 24 11.6 23.2r 14SQ373 W84 C~3cnr 2014 09 24.33537 03 29 46.969 -12 24 11.60 22.6i 14SQ373 W84 C~4yUX 2014 09 24.33537 03 29 46.97 -12 24 11.6 22.9i 14SQ373 W84 C~3cnr 2014 09 27.33062 03 29 39.053 -12 26 15.40 23.0i 14SQ373 W84 C~4yUX 2014 09 27.33062 03 29 39.05 -12 26 15.4 23.0i 14SQ373 W84 C~3cnr 2014 09 30.31779 03 29 30.476 -12 28 16.51 23.6g 14SQ373 W84 C~4yUX 2014 09 30.31779 03 29 30.48 -12 28 16.6 24.0g 14SQ373 W84 C~3cnr 2014 09 30.31918 03 29 30.468 -12 28 16.55 23.1r 14SQ373 W84 C~4yUX 2014 09 30.31918 03 29 30.47 -12 28 16.5 23.1r 14SQ373 W84 C~3cnr 2014 11 13.31471 03 26 26.922 -12 50 14.81 22.7z 14SQ373 W84 C~4yUX 2014 11 16.30434 03 26 12.369 -12 50 58.87 22.2z 14SQ373 W84 C~4yUX 2014 11 16.30434 03 26 12.37 -12 50 58.9 22.4z 14SQ373 W84 C~3cnr 2015 11 08.33496 03 32 15.781 -12 21 53.61 23.1r 14SQ373 W84 C~4yUX 2015 11 08.33496 03 32 15.78 -12 21 53.6 23.2r 14SQ373 W84 C~3cnr 2015 11 08.33634 03 32 15.769 -12 21 53.45 22.7z 14SQ373 W84 C~4yUX 2015 11 22.23549 03 31 08.117 -12 25 22.38 22.6z 14SQ373 W84 C~4yUX 2015 11 30.25938 03 30 29.464 -12 26 12.07 23.0i 14SQ373 W84 C~4yUX 2015 11 30.25938 03 30 29.46 -12 26 12.1 23.1i 14SQ373 W84 C~3cnr 2015 12 11.20245 03 29 39.276 -12 25 51.75 23.3r 14SQ373 W84 C~4yUX 2015 12 11.20245 03 29 39.28 -12 25 51.8 23.5r 14SQ373 W84 C~3cnr 2015 12 11.22058 03 29 39.186 -12 25 51.75 24.3g 14SQ373 W84 C~4yUX 2015 12 15.22674 03 29 21.991 -12 25 18.48 22.7i 14SQ373 W84 C~4yUX 2015 12 15.22674 03 29 21.99 -12 25 18.5 22.7i 14SQ373 W84 C~3cnr 2015 12 15.22810 03 29 21.983 -12 25 18.40 23.2r 14SQ373 W84 C~4yUX 2015 12 15.22810 03 29 21.98 -12 25 18.4 23.3r 14SQ373 W84 C~3cnr 2016 11 05.34169 03 37 50.714 -11 53 45.14 23.3r 14SQ373 W84 C~4yUX 2016 11 05.34169 03 37 50.71 -11 53 45.1 23.3r 14SQ373 W84 C~3cnr 2016 12 23.19055 03 34 09.494 -11 56 24.29 23.0i 14SQ373 W84 C~4yUX 2016 12 23.19055 03 34 09.49 -11 56 24.3 23.1i 14SQ373 W84 C~3cnr 2016 12 23.19194 03 34 09.486 -11 56 24.21 23.3r 14SQ373 W84 C~4yUX 2016 12 23.19194 03 34 09.49 -11 56 24.2 23.2r 14SQ373 W84 C~3cnr 2016 12 23.19333 03 34 09.489 -11 56 24.35 24.8g 14SQ373 W84 C~4yUX 2017 02 02.08313 03 32 38.520 -11 35 02.10 22.7z 14SQ373 W84 C~4yUX 2018 02 09.06351 03 37 55.464 -11 02 55.97 23.5r 14SQ373 W84 C~4yUX 2018 02 09.06487 03 37 55.468 -11 02 55.87 22.9i 14SQ373 W84 C~4yUX 2018 02 09.06626 03 37 55.472 -11 02 55.82 24.3g 14SQ373 W84 C~4yUX
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 0.01
2 0.0000 0.06 0.08 -0.06 -0.05
3 0.0000 -0.08 0.00 -0.02 0.03
4 0.0000 -0.10 -0.01 -0.01 0.04
5 0.0082 -146.20 -0.09 -86.25 -0.10
6 0.0082 -146.16 -0.05 -86.26 -0.11
7 0.0164 -300.73 0.04 -167.24 -0.00
8 0.0164 -300.70 0.07 -167.34 -0.10
9 0.0164 -300.81 0.04 -167.20 0.07
10 0.0164 -300.86 -0.01 -167.24 0.03
11 0.1368 -3248.71 0.08 -682.91 -0.27
12 0.1450 -3465.46 0.01 -666.16 -0.09
13 0.1450 -3465.47 0.01 -666.13 -0.06
14 1.1225 2130.63 0.03 -482.51 0.00
15 1.1225 2130.64 0.04 -482.52 -0.01
16 1.1225 2130.52 0.02 -482.32 0.19
17 1.1606 1120.68 0.07 -402.60 0.18
18 1.1825 563.35 -0.06 -290.70 0.07
19 1.1825 563.41 0.00 -290.69 0.08
20 1.2125 -136.34 -0.09 -64.55 0.07
21 1.2125 -136.38 -0.13 -64.48 0.14
22 1.2126 -137.65 -0.30 -64.11 0.06
23 1.2235 -370.09 0.03 38.50 0.00
24 1.2235 -370.07 0.05 38.52 0.02
25 1.2235 -370.20 -0.00 38.64 0.10
26 1.2235 -370.16 0.04 38.63 0.09
27 2.1164 7323.04 -0.04 -267.12 0.04
28 2.1164 7323.08 0.01 -267.18 -0.02
29 2.2474 4164.17 -0.03 510.48 -0.02
30 2.2474 4164.23 0.03 510.48 -0.03
31 2.2474 4164.14 0.01 510.59 0.04
32 2.2474 4164.20 0.07 510.58 0.03
33 2.2474 4164.14 0.08 510.44 -0.16
34 2.3593 3247.33 -0.04 2119.64 -0.08
35 3.3778 8269.57 -0.04 2635.09 -0.07
36 3.3778 8269.66 0.02 2635.17 -0.05
37 3.3778 8269.73 0.08 2635.20 -0.08
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.
14SQ373 quality flag:3 Type: SCATEXTD SCATEXTD SCATEXTD axisobj 46.493 46.517 46.469 ecceobj 0.161 0.162 0.160 incobj 29.902 29.902 29.902 qmin 37.628 37.557 37.681 qmax 54.938 54.982 54.830 amean 46.109 46.134 46.085 amin 45.730 45.751 45.694 amax 46.542 46.569 46.512 emean 0.165 0.166 0.164 emin 0.151 0.151 0.149 emax 0.181 0.182 0.180 imean 28.375 28.371 28.378 imin 28.006 27.998 28.006 imax 28.686 28.694 28.702 excite_mean 0.503 0.504 0.503 fracstop 1.000 1.000 1.000 cjmean 2.801 2.801 2.801 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 175.6 175.4 175.7 kozaiamp 180.0 180.0 180.0