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: 534074
# Created Fri Nov 22 02:07:28 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 54 observations of 54
# Arc: 13.01y
# First observation: 2011/09/04
# Last observation: 2024/09/07
# Chi-squared of fit: 36.10 DOF: 102 RMS: 0.14
# Min/Max residuals: -0.43 0.40
# Exact a, adot, b, bdot, g, gdot:
1.368242E-05 2.085549E-02 2.492570E-07 1.817338E-03 2.287625E-02 -9.920203E-04
# 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
4.275417 15.654548 0.567466 0.061835 -0.827580 2455808.934256
# Heliocentric elements and errors
Epoch: 2455808.5000 = 2011/09/04
Mean Anomaly: 234.94058 +/- 0.000
Argument of Peri: 171.86325 +/- 0.000
Long of Asc Node: 335.16619 +/- 0.000
Inclination: 6.54293 +/- 0.000
Eccentricity: 0.07743955 +/- 0.0000
Semi-Major Axis: 42.49839482 +/- 0.0000
Time of Perihelion: 2490962.2069 +/- 0.0
Perihelion: 39.20733845 +/- 0.0000
Aphelion: 45.78945119 +/- 0.0000
Period (y) 277.0556 +/- 0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X 42.93056840 +/- 0.0000
Ecliptic Y 11.44149618 +/- 0.0000
Ecliptic Z 3.25891306 +/- 0.0000
Ecliptic XDOT -0.00080633 +/- 0.0000
Ecliptic YDOT 0.00237246 +/- 0.0000
Ecliptic ZDOT 0.00020811 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 44.54846207 +/- 0.0000
Geocenter to KBO 43.71351461 +/- 0.0000
# Hcoef: 5.86
The following table shows the complete astrometric record for 534074. 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 (534074) followed by the observatory code and reference code for the source of the astrometry.
2011 09 04.43349 00 50 59.314 +10 06 14.36 22.7w 534074 F51 C~1vXi 2011 09 04.44834 00 50 59.253 +10 06 13.88 22.4w 534074 F51 C~1vXi 2011 09 04.46324 00 50 59.213 +10 06 13.64 22.5w 534074 F51 C~1vXi 2011 09 04.47825 00 50 59.151 +10 06 13.37 22.6w 534074 F51 C~1vXi 2011 10 25.28773 00 47 27.522 +09 45 52.02 22.2G 534074 F51 C~2r7W 2012 09 26.50249 00 53 48.501 +10 31 56.72 21.4G 534074 F51 C~2r7W 2012 10 09.35135 00 52 52.497 +10 26 31.24 22.0G 534074 F51 C~2r7W 2012 10 09.36547 00 52 52.433 +10 26 30.80 22.2G 534074 F51 C~2r7W 2012 10 09.37970 00 52 52.361 +10 26 30.54 22.2G 534074 F51 C~2r7W 2012 10 09.39400 00 52 52.310 +10 26 30.16 22.4G 534074 F51 C~2r7W 2012 11 03.41242 00 51 07.798 +10 15 27.29 22.8G 534074 F51 C~2r7W 2012 11 04.25003 00 51 04.615 +10 15 05.88 22.3w 534074 F51 C~1vXi 2012 11 04.26414 00 51 04.568 +10 15 05.71 22.3w 534074 F51 C~1vXi 2012 11 04.27822 00 51 04.513 +10 15 05.36 22.3w 534074 F51 C~1vXi 2012 11 04.29242 00 51 04.452 +10 15 05.01 22.3w 534074 F51 C~1vXi 2013 09 15.54773 00 58 56.673 +11 09 46.62 22.2G 534074 F51 C~2r7W 2013 09 15.56146 00 58 56.628 +11 09 46.50 22.9G 534074 F51 C~2r7W 2013 09 15.57527 00 58 56.553 +11 09 46.32 22.8G 534074 F51 C~2r7W 2014 06 30.58798 01 05 16.292 +11 46 25.97 22.5w 534074 F51 C~1vXi 2014 06 30.59192 01 05 16.297 +11 46 25.87 22.3w 534074 F51 C~1vXi 2014 06 30.59588 01 05 16.296 +11 46 26.03 22.6w 534074 F51 C~1vXi 2014 06 30.59982 01 05 16.311 +11 46 26.11 22.2w 534074 F51 C~1vXi 2014 08 28.44831 01 04 24.386 +11 48 15.08 22.7w 534074 F51 C~1vXi 2014 08 28.47287 01 04 24.317 +11 48 14.66 22.6w 534074 F51 C~1vXi 2014 08 28.48506 01 04 24.277 +11 48 14.35 22.3w 534074 F51 C~1vXi 2014 09 19.44819 01 03 04.756 +11 41 55.16 22.5G 534074 F51 C~2r7W 2014 09 29.51918 01 02 22.197 +11 38 06.96 22.3w 534074 F51 C~1vXi 2014 09 29.53062 01 02 22.144 +11 38 06.73 22.2w 534074 F51 C~1vXi 2014 09 29.54206 01 02 22.109 +11 38 06.51 22.2w 534074 F51 C~1vXi 2014 09 29.55351 01 02 22.043 +11 38 06.11 22.1w 534074 F51 C~1vXi 2014 11 18.25537 00 58 58.265 +11 16 50.06 22.1w 534074 F51 C~1vXi 2014 11 18.26729 00 58 58.251 +11 16 50.30 22.2w 534074 F51 C~1vXi 2014 11 18.29121 00 58 58.136 +11 16 49.80 22.2w 534074 F51 C~1vXi 2015 11 18.23609 01 03 21.345 +11 50 16.39 22.6G 534074 F51 C~2r7W 2015 12 03.24445 01 02 38.619 +11 44 54.78 22.5G 534074 F51 C~2r7W 2015 12 14.31909 01 02 17.570 +11 41 49.81 22.4G 534074 F51 C~2r7W 2016 10 06.50824 01 10 39.611 +12 41 31.22 22.6G 534074 F51 C~2r7W 2016 10 06.52075 01 10 39.542 +12 41 30.96 21.7G 534074 F51 C~2r7W 2016 10 06.53327 01 10 39.505 +12 41 30.64 22.1G 534074 F51 C~2r7W 2016 10 06.54577 01 10 39.449 +12 41 30.38 22.2G 534074 F51 C~2r7W 2017 09 19.54016 01 16 20.951 +13 20 52.12 23.1G 534074 F51 C~2r7W 2017 09 19.55303 01 16 20.895 +13 20 51.90 22.3G 534074 F51 C~2r7W 2017 09 19.56577 01 16 20.860 +13 20 51.74 22.3G 534074 F51 C~2r7W 2017 09 19.57850 01 16 20.793 +13 20 51.32 22.6G 534074 F51 C~2r7W 2017 10 22.46877 01 13 57.095 +13 07 44.82 22.5G 534074 F51 C~2r7W 2017 11 10.29066 01 12 38.337 +12 59 29.97 21.7G 534074 F51 C~2r7W 2018 02 04.26199 01 11 35.541 +12 45 30.12 22.4G 534074 F51 C~2r7W 2023 10 14.344603 01 42 10.620 +16 25 09.74 22.4w 534074 F52 C~7MED 2023 10 14.357520 01 42 10.531 +16 25 09.55 22.3w 534074 F52 C~7MED 2023 10 14.370491 01 42 10.487 +16 25 09.31 22.2w 534074 F52 C~7MED 2023 10 14.383412 01 42 10.423 +16 25 08.83 22.2w 534074 F52 C~7MED 2024 09 07.474792 01 49 19.451 +17 06 54.88 22.2w 534074 F52 C~8Fj4 2024 09 07.487385 01 49 19.431 +17 06 54.95 22.1w 534074 F52 C~8Fj4 2024 09 07.500304 01 49 19.387 +17 06 54.76 22.2w 534074 F52 C~8Fj4
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 0.06 0.00 0.25
2 0.0000 0.00 -0.04 0.00 0.03
3 0.0001 0.00 0.17 0.00 0.05
4 0.0001 0.00 0.06 0.00 0.04
5 0.1392 0.00 -0.43 0.00 -0.26
6 1.0625 0.00 -0.17 0.00 -0.04
7 1.0977 0.00 -0.03 0.00 -0.01
8 1.0977 0.00 -0.05 0.00 -0.08
9 1.0977 0.00 -0.18 0.00 0.03
10 1.0978 0.00 0.02 0.00 0.02
11 1.1663 0.00 0.28 0.00 -0.06
12 1.1686 0.00 -0.05 0.00 -0.05
13 1.1686 0.00 0.06 0.00 0.14
14 1.1686 0.00 0.05 0.00 0.15
15 1.1687 0.00 -0.05 0.00 0.16
16 2.0318 0.00 0.10 0.00 -0.14
17 2.0318 0.00 0.26 0.00 0.02
18 2.0319 0.00 -0.03 0.00 0.13
19 2.8204 0.00 -0.08 0.00 0.01
20 2.8204 0.00 -0.09 0.00 -0.16
21 2.8204 0.00 -0.20 0.00 -0.06
22 2.8204 0.00 -0.05 0.00 -0.05
23 2.9816 0.00 -0.05 0.00 0.06
24 2.9816 0.00 0.07 0.00 -0.05
25 2.9817 0.00 0.04 0.00 -0.21
26 3.0418 0.00 0.11 0.00 -0.27
27 3.0694 0.00 -0.08 0.00 0.12
28 3.0694 0.00 -0.12 0.00 0.16
29 3.0694 0.00 0.11 0.00 0.22
30 3.0695 0.00 -0.12 0.00 0.09
31 3.2055 0.00 -0.09 0.00 -0.17
32 3.2056 0.00 0.29 0.00 0.35
33 3.2056 0.00 -0.24 0.00 0.40
34 4.2048 0.00 0.07 0.00 -0.02
35 4.2459 0.00 -0.15 0.00 -0.09
36 4.2762 0.00 -0.03 0.00 -0.19
37 5.0899 0.00 0.15 0.00 -0.17
38 5.0899 0.00 -0.04 0.00 -0.12
39 5.0899 0.00 0.26 0.00 -0.13
40 5.0900 0.00 0.26 0.00 -0.07
41 6.0427 0.00 0.01 0.00 -0.04
42 6.0428 0.00 -0.04 0.00 -0.00
43 6.0428 0.00 0.22 0.00 0.09
44 6.0428 0.00 -0.00 0.00 -0.08
45 6.1329 0.00 0.01 0.00 -0.16
46 6.1844 0.00 -0.14 0.00 -0.07
47 6.4198 0.00 0.18 0.00 -0.12
48 12.1093 0.00 0.15 0.00 -0.02
49 12.1093 0.00 -0.28 0.00 0.09
50 12.1093 0.00 -0.04 0.00 0.15
51 12.1094 0.00 -0.10 0.00 -0.03
52 13.0104 0.00 -0.19 0.00 -0.06
53 13.0104 0.00 0.11 0.00 0.13
54 13.0104 0.00 0.07 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.
534074 quality flag:3 Type: 5:3EE 5:3EE 5:3EE axisobj 42.552 42.552 42.552 ecceobj 0.076 0.076 0.076 incobj 6.540 6.540 6.540 qmin 37.041 37.041 37.041 qmax 48.090 48.089 48.089 amean 42.329 42.329 42.329 amin 41.934 41.935 41.934 amax 42.757 42.757 42.758 emean 0.096 0.096 0.096 emin 0.065 0.065 0.065 emax 0.125 0.125 0.125 imean 6.803 6.803 6.802 imin 5.592 5.592 5.592 imax 8.169 8.169 8.169 excite_mean 0.153 0.153 0.153 fracstop 1.000 1.000 1.000 cjmean 3.054 3.054 3.054 libcent 0 181.6 181.5 182.3 libamp 0 96.7 96.7 95.5 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 175.5 175.6 175.6 kozaiamp 180.0 180.0 180.0