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: 534314 # Created Fri Apr 26 01:08:41 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 75 observations of 75 # Arc: 10.24y # First observation: 2010/10/15 # Last observation: 2021/01/11 # Chi-squared of fit: 97.38 DOF: 144 RMS: 0.20 # Min/Max residuals: -0.79 0.59 # Exact a, adot, b, bdot, g, gdot: 1.768906E-05 3.249698E-02 1.203596E-06 4.727894E-04 2.876611E-02 -1.471346E-03 # Covariance matrix: 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 # lat0 lon0 xBary yBary zBary JD0 -9.129842 39.305106 0.297251 -0.150482 -0.936262 2455484.865436 # Heliocentric elements and errors Epoch: 2455484.5000 = 2010/10/15 Mean Anomaly: 345.13904 +/- 0.000 Argument of Peri: 296.01799 +/- 0.000 Long of Asc Node: 123.78387 +/- 0.000 Inclination: 8.92121 +/- 0.000 Eccentricity: 0.16842829 +/- 0.0000 Semi-Major Axis: 42.52207415 +/- 0.0000 Time of Perihelion: 2459665.3500 +/- 0.0 Perihelion: 35.36015394 +/- 0.0000 Aphelion: 49.68399435 +/- 0.0000 Period (y) 277.2872 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 27.48424604 +/- 0.0000 Ecliptic Y 22.11168680 +/- 0.0000 Ecliptic Z -5.51590531 +/- 0.0000 Ecliptic XDOT -0.00206063 +/- 0.0000 Ecliptic YDOT 0.00231656 +/- 0.0000 Ecliptic ZDOT 0.00006664 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 35.70347317 +/- 0.0000 Geocenter to KBO 34.76318589 +/- 0.0000 # Hcoef: 7.11
The following table shows the complete astrometric record for 534314. 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 (534314) followed by the observatory code and reference code for the source of the astrometry.
2010 10 15.36467 02 39 16.327 +05 55 24.64 22.5G 534314 F51 C~2rYB 2010 11 02.44091 02 37 41.451 +05 47 07.63 22.6G 534314 F51 C~2rYB 2010 11 02.45583 02 37 41.355 +05 47 07.16 22.9G 534314 F51 C~2rYB 2010 11 02.46984 02 37 41.276 +05 47 06.81 22.4G 534314 F51 C~2rYB 2010 11 02.48245 02 37 41.218 +05 47 06.54 23.0G 534314 F51 C~2rYB 2010 11 30.30534 02 35 17.088 +05 37 35.86 22.5G 534314 F51 C~2rYB 2012 10 18.39206 02 53 15.422 +07 05 37.90 22.6G 534314 F51 C~2rYB 2012 10 18.40720 02 53 15.336 +07 05 37.43 22.8G 534314 F51 C~2rYB 2012 10 18.42240 02 53 15.258 +07 05 37.06 22.6G 534314 F51 C~2rYB 2012 10 18.43767 02 53 15.179 +07 05 36.67 22.6G 534314 F51 C~2rYB 2012 12 07.23226 02 48 55.321 +06 48 02.89 22.6G 534314 F51 C~2rYB 2012 12 28.26548 02 47 36.559 +06 46 11.27 22.5G 534314 F51 C~2rYB 2013 08 22.57882 03 03 11.454 +08 03 26.92 22.7G 534314 F51 C~2rYB 2013 11 04.47268 02 58 58.161 +07 33 49.84 21.7G 534314 F51 C~2rYB 2013 11 24.29673 02 57 10.422 +07 26 49.09 22.4w 534314 F51 C~2VW4 2013 11 24.31002 02 57 10.331 +07 26 48.99 22.6w 534314 F51 C~2VW4 2013 11 24.32334 02 57 10.264 +07 26 48.94 22.8w 534314 F51 C~2VW4 2013 11 24.33666 02 57 10.193 +07 26 48.69 22.5w 534314 F51 C~2VW4 2013 11 27.48545 02 56 53.793 +07 25 54.64 23.3G 534314 F51 C~2rYB 2014 08 31.54603 03 10 13.407 +08 35 14.84 20.6G 534314 F51 C~2rYB 2014 09 09.53174 03 10 01.028 +08 32 20.11 23.1G 534314 F51 C~2rYB 2014 09 23.50849 03 09 25.805 +08 27 01.47 22.2w 534314 F51 C~1vXj 2014 09 23.52116 03 09 25.787 +08 27 00.76 22.3w 534314 F51 C~1vXj 2014 09 23.53385 03 09 25.728 +08 27 00.69 22.3w 534314 F51 C~1vXj 2014 10 07.43672 03 08 33.682 +08 21 06.58 22.6G 534314 F51 C~2rYB 2014 10 25.51656 03 07 06.917 +08 13 13.10 22.8G 534314 F51 C~2rYB 2014 10 29.40788 03 06 46.296 +08 11 34.62 22.3w 534314 F51 C~1vXj 2014 10 29.42083 03 06 46.216 +08 11 34.27 22.4w 534314 F51 C~1vXj 2014 10 29.43372 03 06 46.153 +08 11 33.32 22.1w 534314 F51 C~1vXj 2014 11 22.46121 03 04 34.507 +08 02 39.67 22.4G 534314 F51 C~2rYB 2014 11 24.34518 03 04 24.370 +08 02 05.62 22.2w 534314 F51 C~1vXj 2014 11 24.36028 03 04 24.282 +08 02 05.51 22.4w 534314 F51 C~1vXj 2014 11 24.37539 03 04 24.209 +08 02 05.19 22.4w 534314 F51 C~1vXj 2014 11 24.39050 03 04 24.143 +08 02 04.62 22.5w 534314 F51 C~1vXj 2014 11 26.29746 03 04 13.974 +08 01 31.60 22.3w 534314 F51 C~1vXj 2014 11 26.31989 03 04 13.849 +08 01 31.74 22.3w 534314 F51 C~1vXj 2014 11 26.33108 03 04 13.807 +08 01 31.29 22.3w 534314 F51 C~1vXj 2014 12 12.47350 03 02 54.179 +07 57 57.50 22.5G 534314 F51 C~2rYB 2015 01 10.31289 03 01 17.887 +07 57 14.22 22.8G 534314 F51 C~2rYB 2015 01 15.35694 03 01 09.163 +07 57 54.83 22.7G 534314 F51 C~2rYB 2015 01 22.25005 03 01 01.735 +07 59 13.47 23.1w 534314 F51 C~1vXj 2015 01 22.26541 03 01 01.722 +07 59 13.74 22.8w 534314 F51 C~1vXj 2015 01 22.28083 03 01 01.704 +07 59 13.67 22.9w 534314 F51 C~1vXj 2015 10 09.61785 03 15 39.852 +08 54 41.69 22.9G 534314 F51 C~2rYB 2015 10 09.62237 03 15 39.822 +08 54 41.61 22.6G 534314 F51 C~2rYB 2015 10 09.62687 03 15 39.817 +08 54 41.36 21.8G 534314 F51 C~2rYB 2015 10 09.63140 03 15 39.787 +08 54 41.35 23.0G 534314 F51 C~2rYB 2015 11 07.39098 03 13 14.494 +08 42 45.97 23.0G 534314 F51 C~2rYB 2015 12 02.30729 03 10 58.370 +08 34 48.90 22.3G 534314 F51 C~2rYB 2015 12 02.31992 03 10 58.314 +08 34 48.76 22.2G 534314 F51 C~2rYB 2015 12 02.33260 03 10 58.244 +08 34 48.52 23.0G 534314 F51 C~2rYB 2015 12 02.34541 03 10 58.175 +08 34 48.25 22.6G 534314 F51 C~2rYB 2015 12 03.30762 03 10 53.221 +08 34 34.68 22.7G 534314 F51 C~2rYB 2015 12 03.31862 03 10 53.179 +08 34 34.97 23.1G 534314 F51 C~2rYB 2015 12 03.32958 03 10 53.096 +08 34 34.35 22.6G 534314 F51 C~2rYB 2015 12 03.34061 03 10 53.069 +08 34 34.23 22.5G 534314 F51 C~2rYB 2016 01 03.32374 03 08 44.377 +08 31 15.92 22.7G 534314 F51 C~2rYB 2016 01 03.33755 03 08 44.326 +08 31 15.94 23.1G 534314 F51 C~2rYB 2016 01 03.35151 03 08 44.286 +08 31 16.20 22.4G 534314 F51 C~2rYB 2016 01 13.32941 03 08 20.226 +08 32 02.25 22.5G 534314 F51 C~2rYB 2016 01 14.28118 03 08 18.474 +08 32 09.99 22.0G 534314 F51 C~2rYB 2016 03 06.25350 03 09 15.462 +08 49 57.47 22.7G 534314 F51 C~2rYB 2016 11 29.49345 03 18 25.533 +09 09 39.73 22.4G 534314 F51 C~2rYB 2017 09 24.46703 03 31 05.020 +10 07 34.62 22.8G 534314 F51 C~2rYB 2017 09 24.48064 03 31 04.980 +10 07 34.36 22.4G 534314 F51 C~2rYB 2017 09 24.49430 03 31 04.948 +10 07 34.33 22.4G 534314 F51 C~2rYB 2017 09 24.50790 03 31 04.904 +10 07 33.90 23.2G 534314 F51 C~2rYB 2017 12 07.29201 03 25 03.990 +09 41 46.78 22.2G 534314 F51 C~2rYB 2017 12 20.28527 03 24 01.741 +09 39 45.92 22.3R 534314 G37 C~2VW4 2017 12 20.37174 03 24 01.385 +09 39 45.63 534314 G37 C~2VW4 2018 01 03.37202 03 23 07.855 +09 39 09.08 22.6G 534314 F51 C~2rYB 2018 01 13.38520 03 22 40.485 +09 39 44.84 22.3G 534314 F51 C~2rYB 2021 01 11.158740 03 44 36.315 +11 17 24.55 22.4G 534314 G37 C~4YAl 2021 01 11.218120 03 44 36.133 +11 17 24.88 534314 G37 C~4YAl 2021 01 11.265170 03 44 35.988 +11 17 25.09 534314 G37 C~4YAl
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 -0.17
2 0.0495 0.00 0.19 0.00 0.04
3 0.0495 0.00 -0.02 0.00 -0.05
4 0.0496 0.00 -0.05 0.00 -0.04
5 0.0496 0.00 0.12 0.00 0.02
6 0.1258 0.00 -0.32 0.00 0.06
7 2.0097 0.00 0.19 0.00 -0.01
8 2.0097 0.00 0.06 0.00 -0.07
9 2.0097 0.00 0.06 0.00 -0.02
10 2.0098 0.00 0.06 0.00 0.01
11 2.1461 0.00 -0.04 0.00 -0.02
12 2.2037 0.00 0.59 0.00 -0.79
13 2.8534 0.00 0.13 0.00 0.04
14 3.0557 0.00 0.19 0.00 -0.03
15 3.1100 0.00 0.17 0.00 -0.03
16 3.1100 0.00 -0.13 0.00 0.10
17 3.1101 0.00 -0.06 0.00 0.28
18 3.1101 0.00 -0.06 0.00 0.27
19 3.1187 0.00 -0.16 0.00 -0.45
20 3.8773 0.00 0.21 0.00 -0.24
21 3.9019 0.00 0.06 0.00 0.20
22 3.9402 0.00 -0.31 0.00 0.41
23 3.9402 0.00 0.04 0.00 0.01
24 3.9402 0.00 -0.22 0.00 0.25
25 3.9783 0.00 0.11 0.00 0.07
26 4.0278 0.00 0.25 0.00 0.11
27 4.0384 0.00 -0.16 0.00 0.42
28 4.0385 0.00 -0.30 0.00 0.39
29 4.0385 0.00 -0.19 0.00 -0.24
30 4.1043 0.00 -0.03 0.00 -0.07
31 4.1095 0.00 -0.34 0.00 -0.04
32 4.1095 0.00 -0.42 0.00 0.11
33 4.1095 0.00 -0.28 0.00 0.06
34 4.1096 0.00 -0.04 0.00 -0.24
35 4.1148 0.00 -0.54 0.00 -0.25
36 4.1149 0.00 -0.60 0.00 0.27
37 4.1149 0.00 -0.33 0.00 0.01
38 4.1591 0.00 -0.08 0.00 0.30
39 4.2381 0.00 -0.09 0.00 -0.05
40 4.2519 0.00 -0.11 0.00 -0.06
41 4.2707 0.00 0.15 0.00 0.06
42 4.2708 0.00 0.13 0.00 0.12
43 4.2708 0.00 0.05 0.00 -0.15
44 4.9836 0.00 0.14 0.00 -0.02
45 4.9836 0.00 -0.02 0.00 0.01
46 4.9836 0.00 0.21 0.00 -0.12
47 4.9836 0.00 0.05 0.00 -0.02
48 5.0624 0.00 0.23 0.00 -0.00
49 5.1306 0.00 -0.04 0.00 -0.08
50 5.1306 0.00 0.12 0.00 -0.04
51 5.1306 0.00 0.07 0.00 -0.10
52 5.1307 0.00 0.05 0.00 -0.18
53 5.1333 0.00 0.03 0.00 -0.00
54 5.1333 0.00 0.26 0.00 0.44
55 5.1334 0.00 -0.13 0.00 -0.02
56 5.1334 0.00 0.33 0.00 0.01
57 5.2182 0.00 0.22 0.00 -0.13
58 5.2183 0.00 0.08 0.00 -0.13
59 5.2183 0.00 0.11 0.00 0.10
60 5.2456 0.00 0.06 0.00 -0.12
61 5.2482 0.00 0.07 0.00 0.31
62 5.3905 0.00 -0.20 0.00 -0.03
63 6.1249 0.00 0.32 0.00 -0.20
64 6.9435 0.00 -0.11 0.00 -0.16
65 6.9435 0.00 -0.11 0.00 -0.13
66 6.9435 0.00 0.01 0.00 0.14
67 6.9436 0.00 -0.05 0.00 0.01
68 7.1456 0.00 -0.10 0.00 0.14
69 7.1812 0.00 0.12 0.00 -0.12
70 7.1814 0.00 0.55 0.00 0.14
71 7.2197 0.00 -0.19 0.00 0.14
72 7.2471 0.00 0.12 0.00 -0.17
73 10.2417 0.00 -0.03 0.00 -0.17
74 10.2419 0.00 -0.02 0.00 -0.05
75 10.2420 0.00 -0.03 0.00 0.00
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.
534314 quality flag:3 Type: 5:3EE 5:3EE 5:3EE axisobj 42.688 42.688 42.688 ecceobj 0.171 0.171 0.171 incobj 8.919 8.919 8.919 qmin 34.838 34.838 34.838 qmax 50.153 50.152 50.152 amean 42.328 42.328 42.328 amin 41.945 41.945 41.945 amax 42.741 42.741 42.741 emean 0.158 0.158 0.158 emin 0.141 0.141 0.141 emax 0.175 0.175 0.175 imean 7.654 7.654 7.654 imin 7.037 7.037 7.037 imax 8.413 8.413 8.413 excite_mean 0.207 0.207 0.207 fracstop 1.000 1.000 1.000 cjmean 3.032 3.032 3.032 libcent 0 181.8 181.8 181.8 libamp 0 36.4 36.5 36.4 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 179.4 179.4 179.4 kozaiamp 180.0 180.0 180.0