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: 14XC48 # Created Fri Apr 26 01:16:52 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 54 observations of 54 # Arc: 6.80y # First observation: 2014/12/12 # Last observation: 2021/09/30 # Chi-squared of fit: 18.04 DOF: 102 RMS: 0.10 # Min/Max residuals: -0.35 0.24 # Exact a, adot, b, bdot, g, gdot: 1.655011E-05 2.767663E-02 -4.988610E-06 -7.543116E-03 2.690523E-02 -3.330078E-03 # Covariance matrix: 1.2851E-13 -6.6203E-14 -1.8715E-14 1.2702E-14 -6.4154E-14 -2.6627E-13 -6.6203E-14 5.9679E-14 1.3177E-14 -1.4002E-14 1.2531E-14 2.6169E-13 -1.8715E-14 1.3177E-14 6.7925E-14 -2.1661E-14 1.9210E-14 7.3632E-14 1.2702E-14 -1.4002E-14 -2.1661E-14 1.2992E-14 -1.9577E-15 -7.1924E-14 -6.4154E-14 1.2531E-14 1.9210E-14 -1.9577E-15 1.3734E-13 1.1075E-13 -2.6627E-13 2.6169E-13 7.3632E-14 -7.1924E-14 1.1075E-13 1.3697E-12 # lat0 lon0 xBary yBary zBary JD0 -24.642712 9.162883 -0.927549 -0.137018 -0.299157 2457003.639138 # Heliocentric elements and errors Epoch: 2457004.5000 = 2014/12/13 Mean Anomaly: 319.63013 +/- 0.015 Argument of Peri: 292.36750 +/- 0.020 Long of Asc Node: 132.92229 +/- 0.000 Inclination: 28.22383 +/- 0.000 Eccentricity: 0.13085252 +/- 0.0000 Semi-Major Axis: 41.24226201 +/- 0.0027 Time of Perihelion: 2467852.9333 +/- 9.2 Perihelion: 35.84560802 +/- 0.0030 Aphelion: 46.63891600 +/- 0.0035 Period (y) 264.8634 +/- 0.03 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 33.52561705 +/- 0.0005 Ecliptic Y 6.34924397 +/- 0.0001 Ecliptic Z -15.49753463 +/- 0.0002 Ecliptic XDOT -0.00107262 +/- 0.0000 Ecliptic YDOT 0.00267528 +/- 0.0000 Ecliptic ZDOT -0.00055628 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 37.47609780 +/- 0.0004 Geocenter to KBO 37.16761755 +/- 0.0005 # Hcoef: 7.18
The following table shows the complete astrometric record for 14XC48. 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 (14XC48) followed by the observatory code and reference code for the source of the astrometry.
2014 12 12.13836 01 13 38.082 -18 57 51.34 23.3r 14XC48 W84 C~4yVS 2014 12 12.13836 01 13 38.08 -18 57 51.3 23.3r 14XC48 W84 C~3cpY 2014 12 15.12668 01 13 32.501 -18 56 35.13 22.8r 14XC48 W84 C~4yVS 2014 12 15.12668 01 13 32.50 -18 56 35.1 22.9r 14XC48 W84 C~3cpZ 2014 12 15.12805 01 13 32.494 -18 56 35.10 22.8i 14XC48 W84 C~4yVS 2014 12 15.12805 01 13 32.49 -18 56 35.1 22.8i 14XC48 W84 C~3cpZ 2014 12 25.08048 01 13 20.404 -18 51 28.49 23.7g 14XC48 W84 C~4yVS 2014 12 29.07605 01 13 18.511 -18 49 04.24 22.5z 14XC48 W84 C~4yVS 2015 08 24.39409 01 28 17.419 -18 00 29.53 22.7r 14XC48 W84 C~4yVS 2015 08 24.39546 01 28 17.425 -18 00 29.59 22.0i 14XC48 W84 C~4yVS 2015 09 04.35956 01 27 43.265 -18 09 43.22 22.8z 14XC48 W84 C~4yVS 2015 10 07.22227 01 25 15.586 -18 33 51.03 22.8r 14XC48 W84 C~4yVS 2015 10 07.22227 01 25 15.59 -18 33 51.0 22.9r 14XC48 W84 C~3cpZ 2015 10 07.22363 01 25 15.580 -18 33 51.04 23.9g 14XC48 W84 C~4yVS 2015 11 06.11335 01 22 42.649 -18 45 38.47 23.9g 14XC48 W84 C~4yVS 2015 11 06.11335 01 22 42.65 -18 45 38.5 23.9g 14XC48 W84 C~3cpZ 2015 11 06.11474 01 22 42.638 -18 45 38.60 22.5i 14XC48 W84 C~4yVS 2015 11 06.11474 01 22 42.64 -18 45 38.6 22.6i 14XC48 W84 C~3cpZ 2015 11 07.14022 01 22 37.738 -18 45 48.82 24.0g 14XC48 W84 C~4yVS 2015 11 07.14022 01 22 37.74 -18 45 48.8 24.0g 14XC48 W84 C~3cpZ 2015 11 07.14158 01 22 37.730 -18 45 48.96 22.7i 14XC48 W84 C~4yVS 2015 11 07.14158 01 22 37.73 -18 45 48.9 22.8i 14XC48 W84 C~3cpZ 2015 11 20.10625 01 21 40.407 -18 46 32.74 22.6z 14XC48 W84 C~4yVS 2015 11 20.10625 01 21 40.41 -18 46 32.7 22.6z 14XC48 W84 C~3cpZ 2016 09 30.28598 01 32 45.418 -18 11 37.55 22.8r 14XC48 W84 C~4yVS 2016 09 30.28598 01 32 45.42 -18 11 37.5 22.9r 14XC48 W84 C~3cpZ 2016 09 30.28736 01 32 45.412 -18 11 37.54 22.7i 14XC48 W84 C~4yVS 2016 09 30.28736 01 32 45.41 -18 11 37.5 22.8i 14XC48 W84 C~3cpZ 2016 09 30.28871 01 32 45.402 -18 11 37.42 23.3g 14XC48 W84 C~4yVS 2016 09 30.28871 01 32 45.40 -18 11 37.4 23.7g 14XC48 W84 C~3cpZ 2016 11 18.22280 01 28 41.211 -18 28 57.16 22.4z 14XC48 W84 C~4yVS 2016 12 05.16148 01 27 39.499 -18 26 23.52 22.6i 14XC48 W84 C~4yVS 2016 12 05.16148 01 27 39.50 -18 26 23.5 22.5i 14XC48 W84 C~3cpZ 2016 12 05.16285 01 27 39.495 -18 26 23.44 22.8r 14XC48 W84 C~4yVS 2016 12 05.16285 01 27 39.49 -18 26 23.4 22.8r 14XC48 W84 C~3cpZ 2016 12 05.16421 01 27 39.474 -18 26 23.68 23.3g 14XC48 W84 C~4yVS 2016 12 05.16421 01 27 39.48 -18 26 23.6 23.7g 14XC48 W84 C~3cpZ 2017 11 10.14149 01 36 16.427 -18 09 41.14 22.5r 14XC48 W84 C~4yVS 2017 11 10.14286 01 36 16.416 -18 09 41.09 22.4i 14XC48 W84 C~4yVS 2017 11 10.14422 01 36 16.405 -18 09 41.12 24.1g 14XC48 W84 C~4yVS 2017 11 23.03402 01 35 18.884 -18 10 05.14 22.4z 14XC48 W84 C~4yVS 2017 11 24.10370 01 35 14.550 -18 10 00.09 22.1z 14XC48 W84 C~4yVS 2017 11 27.06623 01 35 02.998 -18 09 39.35 22.5i 14XC48 W84 C~4yVS 2017 12 08.06381 01 34 26.000 -18 07 09.04 22.6r 14XC48 W84 C~4yVS 2017 12 08.06519 01 34 25.994 -18 07 09.15 23.7g 14XC48 W84 C~4yVS 2018 10 18.30397 01 45 14.481 -17 42 12.92 23.0r 14XC48 W84 C~4yVS 2018 10 18.30896 01 45 14.466 -17 42 12.96 24.3g 14XC48 W84 C~4yVS 2018 10 21.17169 01 44 59.364 -17 43 34.41 22.3z 14XC48 W84 C~4yVS 2018 11 16.02024 01 42 48.383 -17 50 22.99 22.5z 14XC48 W84 C~4yVS 2018 11 16.23330 01 42 47.377 -17 50 23.57 22.5i 14XC48 W84 C~4yVS 2018 11 16.23467 01 42 47.370 -17 50 23.49 22.7i 14XC48 W84 C~4yVS 2021 09 30.413672 02 07 46.947 -16 23 56.66 22.8w 14XC48 F51 C~55TM 2021 09 30.427243 02 07 46.914 -16 23 57.04 22.8w 14XC48 F51 C~55TM 2021 09 30.440784 02 07 46.852 -16 23 58.03 22.6w 14XC48 F51 C~55TM
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 -0.11 0.00 0.08
2 0.0000 0.00 -0.08 0.00 0.04
3 0.0082 0.00 0.08 0.00 -0.01
4 0.0082 0.00 0.07 0.00 0.02
5 0.0082 0.00 0.01 0.00 -0.02
6 0.0082 0.00 -0.05 0.00 -0.02
7 0.0354 0.00 -0.19 0.00 0.04
8 0.0464 0.00 0.07 0.00 0.06
9 0.6989 0.00 -0.15 0.00 -0.08
10 0.6989 0.00 -0.00 0.00 -0.07
11 0.7289 0.00 -0.14 0.00 -0.12
12 0.8188 0.00 0.09 0.00 0.01
13 0.8188 0.00 0.03 0.00 -0.02
14 0.8189 0.00 0.04 0.00 0.02
15 0.9007 0.00 0.13 0.00 0.09
16 0.9007 0.00 0.14 0.00 0.06
17 0.9007 0.00 0.10 0.00 -0.03
18 0.9007 0.00 0.07 0.00 -0.03
19 0.9035 0.00 0.11 0.00 0.13
20 0.9035 0.00 0.08 0.00 0.11
21 0.9035 0.00 0.06 0.00 0.04
22 0.9035 0.00 0.06 0.00 -0.02
23 0.9390 0.00 0.07 0.00 0.03
24 0.9390 0.00 0.03 0.00 -0.01
25 1.8019 0.00 0.03 0.00 -0.02
26 1.8019 0.00 0.00 0.00 -0.07
27 1.8019 0.00 -0.01 0.00 0.03
28 1.8019 0.00 0.02 0.00 -0.01
29 1.8019 0.00 -0.06 0.00 0.19
30 1.8019 0.00 -0.03 0.00 0.17
31 1.9359 0.00 0.04 0.00 -0.05
32 1.9823 0.00 0.03 0.00 -0.03
33 1.9823 0.00 0.02 0.00 -0.05
34 1.9823 0.00 -0.06 0.00 0.04
35 1.9823 0.00 0.02 0.00 0.00
36 1.9823 0.00 -0.14 0.00 -0.18
37 1.9823 0.00 -0.23 0.00 -0.26
38 2.9131 0.00 0.09 0.00 0.14
39 2.9131 0.00 0.02 0.00 0.20
40 2.9131 0.00 -0.04 0.00 0.18
41 2.9484 0.00 -0.07 0.00 0.09
42 2.9513 0.00 -0.10 0.00 -0.19
43 2.9594 0.00 -0.00 0.00 -0.08
44 2.9895 0.00 0.03 0.00 0.02
45 2.9895 0.00 0.00 0.00 -0.12
46 3.8499 0.00 0.06 0.00 -0.03
47 3.8499 0.00 0.24 0.00 0.08
48 3.8577 0.00 0.06 0.00 0.06
49 3.9285 0.00 0.04 0.00 -0.25
50 3.9291 0.00 -0.01 0.00 -0.09
51 3.9291 0.00 -0.02 0.00 -0.01
52 6.8016 0.00 -0.35 0.00 0.03
53 6.8016 0.00 0.12 0.00 0.24
54 6.8016 0.00 0.14 0.00 -0.17
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.
14XC48 quality flag:3 Type: SCATEXTD SCATEXTD SCATEXTD axisobj 41.599 41.599 41.599 ecceobj 0.135 0.135 0.135 incobj 28.182 28.182 28.182 qmin 35.298 35.283 35.285 qmax 47.684 47.701 47.673 amean 41.344 41.345 41.342 amin 41.007 41.017 40.994 amax 41.706 41.707 41.709 emean 0.125 0.126 0.125 emin 0.108 0.108 0.109 emax 0.144 0.144 0.144 imean 26.933 26.933 26.932 imin 26.424 26.416 26.420 imax 27.394 27.406 27.392 excite_mean 0.470 0.470 0.470 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 176.7 176.6 176.7 kozaiamp 180.0 180.0 180.0