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: 14SN373 # Created Sat Apr 27 01:16:19 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 34 observations of 34 # Arc: 9.28y # First observation: 2014/09/27 # Last observation: 2024/01/09 # Chi-squared of fit: 8.86 DOF: 62 RMS: 0.09 # Min/Max residuals: -0.22 0.21 # Exact a, adot, b, bdot, g, gdot: 1.687400E-05 2.167081E-02 3.913151E-06 4.024061E-03 2.123722E-02 -9.448820E-03 # Covariance matrix: 1.5012E-13 -2.8121E-14 1.0149E-14 -7.2568E-15 8.0402E-14 -1.3458E-13 -2.8121E-14 8.4841E-14 -1.0565E-14 1.3324E-14 1.0850E-13 3.6263E-13 1.0149E-14 -1.0565E-14 7.9533E-14 -1.6382E-14 -2.7352E-15 -5.6500E-14 -7.2568E-15 1.3324E-14 -1.6382E-14 8.0129E-15 1.1286E-14 6.5726E-14 8.0402E-14 1.0850E-13 -2.7352E-15 1.1286E-14 2.8919E-13 3.9617E-13 -1.3458E-13 3.6263E-13 -5.6500E-14 6.5726E-14 3.9617E-13 1.7261E-12 # lat0 lon0 xBary yBary zBary JD0 -31.437059 45.966692 0.673737 -0.388622 -0.636055 2456927.831398 # Heliocentric elements and errors Epoch: 2456928.5000 = 2014/09/28 Mean Anomaly: 347.41987 +/- 0.006 Argument of Peri: 349.83919 +/- 0.005 Long of Asc Node: 115.69584 +/- 0.000 Inclination: 32.45392 +/- 0.000 Eccentricity: 0.64184899 +/- 0.0001 Semi-Major Axis: 104.53621477 +/- 0.0333 Time of Perihelion: 2470570.6022 +/- 180.1 Perihelion: 37.43975062 +/- 0.0167 Aphelion: 171.63267892 +/- 0.0559 Period (y) 1068.8293 +/- 0.51 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 28.92450262 +/- 0.0007 Ecliptic Y 28.95305825 +/- 0.0007 Ecliptic Z -24.55872378 +/- 0.0006 Ecliptic XDOT -0.00254750 +/- 0.0000 Ecliptic YDOT 0.00138459 +/- 0.0000 Ecliptic ZDOT 0.00107806 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 47.72913081 +/- 0.0007 Geocenter to KBO 47.08750392 +/- 0.0012 # Hcoef: 6.65
The following table shows the complete astrometric record for 14SN373. 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 (14SN373) followed by the observatory code and reference code for the source of the astrometry.
2014 09 27.33062 03 29 37.422 -13 33 48.96 23.2i 14SN373 W84 C~4yUX 2014 09 27.33351 03 29 37.419 -13 33 48.85 24.2g 14SN373 W84 C~4yUX 2014 09 30.31918 03 29 29.763 -13 35 32.82 23.6r 14SN373 W84 C~4yUX 2014 09 30.31918 03 29 29.76 -13 35 32.8 23.6r 14SN373 W84 C~3cnr 2014 09 30.32338 03 29 29.764 -13 35 32.85 23.7i 14SN373 W84 C~4yUX 2014 09 30.32338 03 29 29.76 -13 35 32.9 23.6i 14SN373 W84 C~3cnr 2014 10 23.36292 03 28 13.318 -13 47 13.38 23.1r 14SN373 W84 C~4yUX 2014 10 23.36292 03 28 13.32 -13 47 13.4 23.3r 14SN373 W84 C~3cnr 2014 11 03.33956 03 27 28.897 -13 51 16.68 23.5r 14SN373 W84 C~4yUX 2014 11 03.34093 03 27 28.889 -13 51 16.79 23.5i 14SN373 W84 C~4yUX 2014 11 21.25789 03 26 11.876 -13 55 06.62 24.2g 14SN373 W84 C~4yUX 2016 11 03.26981 03 36 52.109 -12 40 59.39 22.3i 14SN373 W84 C~4yUX 2016 11 03.26981 03 36 52.11 -12 40 59.3 22.4i 14SN373 W84 C~3cnr 2016 11 03.27117 03 36 52.103 -12 40 59.44 23.1r 14SN373 W84 C~4yUX 2016 11 03.27117 03 36 52.10 -12 40 59.4 23.2r 14SN373 W84 C~3cnr 2016 11 09.32861 03 36 26.103 -12 42 44.95 22.3r 14SN373 W84 C~4yUX 2016 11 09.32861 03 36 26.11 -12 42 44.9 22.8r 14SN373 W84 C~3cnr 2016 12 05.24568 03 34 33.330 -12 45 23.14 23.1i 14SN373 W84 C~4yUX 2016 12 05.24568 03 34 33.33 -12 45 23.1 22.9i 14SN373 W84 C~3cnr 2016 12 05.24706 03 34 33.324 -12 45 23.10 24.1g 14SN373 W84 C~4yUX 2016 12 23.19055 03 33 24.486 -12 42 12.61 23.2i 14SN373 W84 C~4yUX 2016 12 23.19055 03 33 24.49 -12 42 12.6 23.4i 14SN373 W84 C~3cnr 2016 12 23.19194 03 33 24.469 -12 42 12.50 23.4r 14SN373 W84 C~4yUX 2016 12 23.19194 03 33 24.47 -12 42 12.5 23.4r 14SN373 W84 C~3cnr 2016 12 23.19333 03 33 24.474 -12 42 12.44 24.3g 14SN373 W84 C~4yUX 2016 12 23.19333 03 33 24.47 -12 42 12.4 24.4g 14SN373 W84 C~3cnr 2017 02 02.08313 03 32 02.611 -12 21 13.15 22.8z 14SN373 W84 C~4yUX 2018 02 09.06351 03 36 43.239 -11 40 19.70 23.3r 14SN373 W84 C~4yUX 2018 02 09.06487 03 36 43.242 -11 40 19.48 23.2i 14SN373 W84 C~4yUX 2020 11 14.380240 03 55 43.104 -10 10 43.95 23.4G 14SN373 G37 C~4NsP 2020 11 14.412780 03 55 42.962 -10 10 43.98 14SN373 G37 C~4NsP 2024 01 09.125340 04 07 24.439 -07 59 26.85 22.7G 14SN373 G37 C~7gqu 2024 01 09.237180 04 07 24.061 -07 59 24.02 14SN373 G37 C~7gqu 2024 01 09.353260 04 07 23.702 -07 59 21.23 14SN373 G37 C~7gqu
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 -0.09 0.00 -0.22
2 0.0000 0.00 -0.03 0.00 -0.01
3 0.0082 0.00 -0.06 0.00 0.02
4 0.0082 0.00 -0.02 0.00 -0.00
5 0.0082 0.00 0.11 0.00 0.06
6 0.0082 0.00 0.17 0.00 0.11
7 0.0713 0.00 0.00 0.00 -0.09
8 0.0713 0.00 0.03 0.00 -0.11
9 0.1013 0.00 0.04 0.00 0.05
10 0.1013 0.00 0.00 0.00 -0.03
11 0.1504 0.00 0.15 0.00 -0.07
12 2.1025 0.00 -0.00 0.00 0.11
13 2.1025 0.00 -0.02 0.00 0.02
14 2.1025 0.00 -0.07 0.00 0.03
15 2.1025 0.00 -0.02 0.00 -0.01
16 2.1191 0.00 -0.07 0.00 -0.01
17 2.1191 0.00 -0.18 0.00 -0.06
18 2.1900 0.00 -0.00 0.00 0.06
19 2.1900 0.00 -0.00 0.00 0.02
20 2.1901 0.00 -0.00 0.00 0.05
21 2.2392 0.00 0.14 0.00 -0.00
22 2.2392 0.00 0.08 0.00 -0.01
23 2.2392 0.00 -0.09 0.00 0.07
24 2.2392 0.00 -0.10 0.00 0.07
25 2.2392 0.00 -0.01 0.00 0.15
26 2.2392 0.00 0.05 0.00 0.11
27 2.3511 0.00 -0.03 0.00 -0.06
28 3.3696 0.00 -0.04 0.00 -0.09
29 3.3696 0.00 0.01 0.00 0.07
30 6.1329 0.00 0.05 0.00 -0.20
31 6.1330 0.00 0.14 0.00 0.21
32 9.2835 0.00 0.19 0.00 0.02
33 9.2838 0.00 -0.16 0.00 0.02
34 9.2841 0.00 -0.06 0.00 -0.16
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.
14SN373 quality flag:3 Type: SCATNEAR SCATNEAR SCATNEAR axisobj 105.899 105.897 105.901 ecceobj 0.644 0.644 0.644 incobj 32.467 32.467 32.467 qmin 35.749 35.222 35.997 qmax 176.516 177.692 176.682 amean 103.779 103.741 103.790 amin 101.868 101.823 101.941 amax 106.693 107.045 106.804 emean 0.640 0.643 0.639 emin 0.631 0.631 0.630 emax 0.656 0.661 0.654 imean 30.701 30.353 30.806 imin 29.889 29.369 30.142 imax 31.266 31.265 31.266 excite_mean 0.819 0.818 0.819 fracstop 1.000 1.000 1.000 cjmean 2.742 2.742 2.742 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 77.6 83.1 76.2 kozaiamp 180.0 180.0 180.0