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: 14WL616 # Created Fri Nov 22 02:10:12 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 61 observations of 61 # Arc: 20.90y # First observation: 2003/01/29 # Last observation: 2023/12/24 # Chi-squared of fit: 41.35 DOF: 116 RMS: 0.15 # Min/Max residuals: -0.55 0.36 # Exact a, adot, b, bdot, g, gdot: 1.558501E-05 2.723531E-02 7.146340E-06 1.046075E-02 2.656830E-02 8.108645E-04 # Covariance matrix: 5.2850E-13 -6.9046E-14 1.1893E-13 -2.0740E-14 -6.7754E-14 -7.3397E-14 -6.9046E-14 1.0401E-14 -2.0104E-14 3.5106E-15 9.4828E-15 1.2426E-14 1.1893E-13 -2.0104E-14 2.4957E-13 -2.2195E-14 -2.4012E-14 -2.7060E-14 -2.0740E-14 3.5106E-15 -2.2195E-14 2.4855E-15 3.9978E-15 4.7224E-15 -6.7754E-14 9.4828E-15 -2.4012E-14 3.9978E-15 9.4164E-14 1.4036E-14 -7.3397E-14 1.2426E-14 -2.7060E-14 4.7224E-15 1.4036E-14 1.6714E-14 # lat0 lon0 xBary yBary zBary JD0 -13.723205 109.803458 -0.324839 -0.219437 -0.898609 2452668.930262 # Heliocentric elements and errors Epoch: 2452668.5000 = 2003/01/29 Mean Anomaly: 9.11163 +/- 0.002 Argument of Peri: 312.95308 +/- 0.003 Long of Asc Node: 141.32419 +/- 0.000 Inclination: 24.79868 +/- 0.000 Eccentricity: 0.18757099 +/- 0.0000 Semi-Major Axis: 47.23548717 +/- 0.0028 Time of Perihelion: 2449667.3038 +/- 0.7 Perihelion: 38.37547994 +/- 0.0029 Aphelion: 56.09549440 +/- 0.0037 Period (y) 324.6466 +/- 0.03 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X -13.00896518 +/- 0.0002 Ecliptic Y 35.16674473 +/- 0.0004 Ecliptic Z -8.92886581 +/- 0.0001 Ecliptic XDOT -0.00276163 +/- 0.0000 Ecliptic YDOT -0.00063820 +/- 0.0000 Ecliptic ZDOT 0.00102758 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 38.54420694 +/- 0.0004 Geocenter to KBO 37.63886418 +/- 0.0004 # Hcoef: 5.70
The following table shows the complete astrometric record for 14WL616. 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 (14WL616) followed by the observatory code and reference code for the source of the astrometry.
2003 01 29.429519 07 17 43.62 +08 23 24.6 14WL616 T14 C~6oD9 2003 01 29.431235 07 17 43.61 +08 23 24.6 14WL616 T14 C~6oD9 2010 01 06.52128 08 05 40.90 +10 42 42.9 14WL616 F51 C~6oD9 2010 01 06.53045 08 05 40.84 +10 42 43.4 14WL616 F51 C~6oD9 2010 02 08.36460 08 02 52.49 +10 55 17.2 14WL616 F51 C~6oD9 2010 02 08.37437 08 02 52.42 +10 55 17.9 22.3g 14WL616 F51 C~6oD9 2010 11 03.62250 08 15 19.89 +10 55 12.2 14WL616 F51 C~6oD9 2010 11 03.63371 08 15 19.88 +10 55 12.1 21.2i 14WL616 F51 C~6oD9 2011 01 23.54432 08 10 46.16 +11 07 28.2 14WL616 F51 C~6oD9 2012 01 15.54645 08 18 00.85 +11 22 33.4 21.4i 14WL616 F51 C~6oD9 2012 01 15.55914 08 18 00.77 +11 22 33.4 21.5i 14WL616 F51 C~6oD9 2012 01 21.52934 08 17 29.90 +11 24 49.6 21.5r 14WL616 F51 C~6oD9 2012 01 21.54085 08 17 29.83 +11 24 50.0 21.5r 14WL616 F51 C~6oD9 2012 10 30.61019 08 28 03.13 +11 30 05.2 14WL616 F51 C~6oD9 2013 01 07.52782 08 25 08.55 +11 37 30.5 14WL616 F51 C~6oD9 2013 01 07.54077 08 25 08.46 +11 37 30.5 21.4r 14WL616 F51 C~6oD9 2013 01 21.47670 08 23 57.80 +11 42 41.4 21.3i 14WL616 F51 C~6oD9 2013 01 21.48965 08 23 57.73 +11 42 41.9 21.3i 14WL616 F51 C~6oD9 2013 11 17.56130 08 34 22.36 +11 45 07.8 21.4z 14WL616 F51 C~6oD9 2013 12 25.61070 08 32 38.53 +11 50 15.1 21.4i 14WL616 F51 C~6oD9 2013 12 25.62264 08 32 38.50 +11 50 15.2 21.6i 14WL616 F51 C~6oD9 2014 01 25.32252 08 30 10.30 +12 01 05.5 14WL616 F51 C~6oD9 2014 11 29.51043 08 40 28.42 +12 01 21.8 22.1w 14WL616 F51 C~77rn 2014 11 29.52302 08 40 28.39 +12 01 22.0 21.9w 14WL616 F51 C~77ro 2014 11 29.53561 08 40 28.36 +12 01 21.8 21.9w 14WL616 F51 C~77ro 2014 11 29.54824 08 40 28.35 +12 01 22.0 22.0w 14WL616 F51 C~77ro 2015 01 26.50247 08 36 35.63 +12 17 45.8 21.7w 14WL616 F51 C~77ro 2015 01 26.51618 08 36 35.56 +12 17 46.4 21.6w 14WL616 F51 C~77ro 2015 01 26.54372 08 36 35.41 +12 17 47.0 21.6w 14WL616 F51 C~77ro 2015 02 18.28618 08 34 42.18 +12 28 05.8 21.8w 14WL616 F51 C~77ro 2015 02 18.29914 08 34 42.12 +12 28 05.9 21.9w 14WL616 F51 C~77ro 2015 02 18.32468 08 34 41.99 +12 28 06.6 21.6w 14WL616 F51 C~77ro 2015 04 05.107265 08 32 18.45 +12 47 11.3 21.2i 14WL616 W84 C~6oD9 2016 01 14.253561 08 44 07.37 +12 28 10.7 21.7r 14WL616 W84 C~6oD9 2016 01 14.254754 08 44 07.36 +12 28 10.8 22.2g 14WL616 W84 C~6oD9 2016 01 16.208281 08 43 57.75 +12 28 57.1 21.7r 14WL616 W84 C~6oD9 2016 01 16.209662 08 43 57.75 +12 28 57.2 22.3g 14WL616 W84 C~6oD9 2017 01 26.38033 08 49 30.19 +12 48 30.2 21.8w 14WL616 F51 C~77ro 2017 01 26.39112 08 49 30.12 +12 48 30.5 21.7w 14WL616 F51 C~77ro 2017 01 26.40191 08 49 30.07 +12 48 30.7 21.7w 14WL616 F51 C~77ro 2017 01 26.41285 08 49 30.01 +12 48 31.2 21.7w 14WL616 F51 C~77ro 2017 02 03.46768 08 48 49.02 +12 52 11.1 21.7w 14WL616 F51 C~77ro 2017 02 03.47906 08 48 48.96 +12 52 11.4 21.6w 14WL616 F51 C~77ro 2017 02 03.49042 08 48 48.88 +12 52 11.2 21.7w 14WL616 F51 C~77ro 2017 02 03.5018 08 48 48.84 +12 52 12.1 21.7w 14WL616 F51 C~77ro 2017 02 19.23983 08 47 31.45 +12 59 35.5 21.8w 14WL616 F51 C~77ro 2017 02 19.25042 08 47 31.40 +12 59 35.8 22.2w 14WL616 F51 C~77ro 2017 02 19.261 08 47 31.36 +12 59 36.1 21.6w 14WL616 F51 C~77ro 2017 02 19.27155 08 47 31.30 +12 59 36.3 21.8w 14WL616 F51 C~77ro 2018 04 13.979037 08 51 15.80 +13 35 04.5 22.5g 14WL616 W84 C~6oD9 2018 04 13.980290 08 51 15.79 +13 35 04.5 21.7i 14WL616 W84 C~6oD9 2018 12 10.250628 09 05 30.17 +12 59 44.7 21.7r 14WL616 W84 C~6oD9 2018 12 11.312538 09 05 27.60 +12 59 58.0 22.3g 14WL616 W84 C~6oD9 2019 01 27.257953 09 02 18.27 +13 16 39.9 21.5i 14WL616 W84 C~6oD9 2021 02 16.176660 09 13 19.53 +13 52 03.5 21.6i 14WL616 W84 C~6oD9 2023 11 19.90529 09 36 50.76 +13 53 17.6 22.1w 14WL616 O18 C~7X8Z 2023 11 19.90963 09 36 50.76 +13 53 17.9 22.2w 14WL616 O18 C~7X8Z 2023 11 19.91397 09 36 50.77 +13 53 17.8 22.4w 14WL616 O18 C~7X8Z 2023 12 24.605920 09 36 06.728 +14 00 29.42 21.8w 14WL616 F51 C~7dJF 2023 12 24.617611 09 36 06.686 +14 00 29.74 21.8w 14WL616 F51 C~7dJF 2023 12 24.641149 09 36 06.630 +14 00 30.22 22.0w 14WL616 F51 C~7dJF
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 0.10 0.00 -0.21
2 0.0000 0.00 0.08 0.00 -0.25
3 6.9380 0.00 -0.19 0.00 -0.21
4 6.9380 0.00 -0.39 0.00 0.12
5 7.0279 0.00 0.24 0.00 -0.21
6 7.0279 0.00 -0.08 0.00 0.23
7 7.7623 0.00 0.07 0.00 0.01
8 7.7624 0.00 -0.06 0.00 -0.00
9 7.9839 0.00 -0.09 0.00 -0.04
10 8.9613 0.00 0.09 0.00 0.28
11 8.9613 0.00 -0.12 0.00 0.00
12 8.9777 0.00 -0.01 0.00 0.16
13 8.9777 0.00 -0.15 0.00 0.29
14 9.7527 0.00 0.16 0.00 0.20
15 9.9414 0.00 0.30 0.00 0.25
16 9.9414 0.00 -0.08 0.00 -0.01
17 9.9796 0.00 -0.08 0.00 0.15
18 9.9796 0.00 -0.11 0.00 0.33
19 10.8012 0.00 0.09 0.00 0.11
20 10.9054 0.00 -0.29 0.00 -0.08
21 10.9054 0.00 0.02 0.00 -0.17
22 10.9894 0.00 0.21 0.00 -0.17
23 11.8332 0.00 0.10 0.00 -0.03
24 11.8332 0.00 0.04 0.00 0.10
25 11.8333 0.00 -0.02 0.00 -0.17
26 11.8333 0.00 0.22 0.00 -0.04
27 11.9920 0.00 0.12 0.00 -0.08
28 11.9920 0.00 0.15 0.00 0.16
29 11.9921 0.00 0.05 0.00 0.05
30 12.0544 0.00 -0.04 0.00 0.36
31 12.0544 0.00 -0.02 0.00 0.10
32 12.0545 0.00 -0.15 0.00 0.08
33 12.1798 0.00 0.03 0.00 -0.00
34 12.9578 0.00 0.12 0.00 -0.06
35 12.9578 0.00 0.06 0.00 0.01
36 12.9631 0.00 -0.05 0.00 -0.09
37 12.9631 0.00 0.06 0.00 -0.02
38 13.9930 0.00 0.04 0.00 0.02
39 13.9931 0.00 -0.18 0.00 0.03
40 13.9931 0.00 -0.09 0.00 -0.06
41 13.9931 0.00 -0.14 0.00 0.14
42 14.0152 0.00 0.03 0.00 -0.02
43 14.0152 0.00 0.01 0.00 -0.03
44 14.0152 0.00 -0.31 0.00 -0.55
45 14.0153 0.00 -0.03 0.00 0.04
46 14.0583 0.00 -0.09 0.00 -0.11
47 14.0584 0.00 -0.09 0.00 -0.11
48 14.0584 0.00 0.06 0.00 -0.12
49 14.0584 0.00 -0.08 0.00 -0.21
50 15.2048 0.00 0.11 0.00 -0.05
51 15.2048 0.00 -0.02 0.00 -0.07
52 15.8626 0.00 0.07 0.00 -0.11
53 15.8655 0.00 0.01 0.00 -0.02
54 15.9941 0.00 0.11 0.00 0.01
55 18.0500 0.00 0.17 0.00 -0.14
56 20.8062 0.00 -0.10 0.00 -0.12
57 20.8062 0.00 -0.13 0.00 0.17
58 20.8063 0.00 0.00 0.00 0.05
59 20.9012 0.00 0.06 0.00 -0.02
60 20.9013 0.00 -0.05 0.00 0.06
61 20.9013 0.00 0.14 0.00 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.
14WL616 quality flag:3 Type: SCATEXTD SCATEXTD SCATEXTD axisobj 47.076 47.076 47.076 ecceobj 0.185 0.185 0.185 incobj 24.862 24.862 24.862 qmin 37.544 37.532 37.564 qmax 56.587 56.596 56.585 amean 46.867 46.867 46.867 amin 46.470 46.472 46.470 amax 47.334 47.338 47.332 emean 0.181 0.181 0.181 emin 0.166 0.166 0.166 emax 0.196 0.196 0.196 imean 23.622 23.622 23.622 imin 23.198 23.197 23.200 imax 23.997 24.004 24.002 excite_mean 0.440 0.440 0.440 fracstop 1.000 1.000 1.000 cjmean 2.891 2.891 2.891 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 170.6 170.7 170.5 kozaiamp 180.0 180.0 180.0