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: 535987
# Created Fri Apr 26 01:08:44 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 75 observations of 75
# Arc: 11.73y
# First observation: 2010/06/01
# Last observation: 2022/02/24
# Chi-squared of fit: 61.25 DOF: 144 RMS: 0.16
# Min/Max residuals: -0.59 0.56
# Exact a, adot, b, bdot, g, gdot:
1.735122E-05 2.404720E-02 -2.058090E-06 -3.069496E-03 2.407936E-02 -5.656272E-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
2.393833 141.280859 -0.958287 -0.013825 0.329474 2455348.767246
# Heliocentric elements and errors
Epoch: 2455348.5000 = 2010/06/01
Mean Anomaly: 310.25844 +/- 0.000
Argument of Peri: 235.49348 +/- 0.000
Long of Asc Node: 340.78913 +/- 0.000
Inclination: 7.69253 +/- 0.000
Eccentricity: 0.23133420 +/- 0.0000
Semi-Major Axis: 46.34249281 +/- 0.0000
Time of Perihelion: 2471270.0159 +/- 0.0
Perihelion: 35.62188944 +/- 0.0000
Aphelion: 57.06309618 +/- 0.0000
Period (y) 315.4840 +/- 0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -32.71230185 +/- 0.0000
Ecliptic Y 24.99752730 +/- 0.0000
Ecliptic Z 1.73455593 +/- 0.0000
Ecliptic XDOT -0.00121873 +/- 0.0000
Ecliptic YDOT -0.00252005 +/- 0.0000
Ecliptic ZDOT -0.00037560 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 41.20668779 +/- 0.0000
Geocenter to KBO 41.52954596 +/- 0.0000
# Hcoef: 6.78
The following table shows the complete astrometric record for 535987. 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 (535987) followed by the observatory code and reference code for the source of the astrometry.
2010 06 01.26648 09 37 51.446 +16 40 24.13 22.5G 535987 F51 C~2rYJ 2011 01 30.55332 09 47 58.688 +15 46 41.53 22.6w 535987 F51 C~1vYB 2011 01 30.57064 09 47 58.614 +15 46 41.81 22.5w 535987 F51 C~1vYB 2011 01 30.58575 09 47 58.541 +15 46 42.45 22.8w 535987 F51 C~1vYB 2011 01 31.53083 09 47 54.001 +15 47 03.95 22.8G 535987 F51 C~2rYJ 2011 05 29.26640 09 42 56.402 +16 04 08.48 23.3G 535987 F51 C~2rYJ 2011 10 29.61219 09 55 36.443 +14 53 54.09 23.0G 535987 F51 C~2rYJ 2012 02 03.58801 09 53 04.047 +15 08 27.34 23.0G 535987 F51 C~2rYJ 2012 02 04.60456 09 52 59.090 +15 08 51.80 22.6G 535987 F51 C~2rYJ 2012 02 15.35343 09 52 06.116 +15 13 09.77 22.9G 535987 F51 C~2rYJ 2014 01 25.43356 10 04 36.458 +13 42 46.93 23.1G 535987 F51 C~2rYJ 2014 02 20.33834 10 02 31.924 +13 53 20.39 22.8G 535987 F51 C~2rYJ 2014 02 26.38102 10 02 02.127 +13 55 46.77 23.2G 535987 F51 C~2rYJ 2014 02 28.30870 10 01 52.737 +13 56 32.10 22.4w 535987 F51 C~1vYB 2014 02 28.32175 10 01 52.675 +13 56 32.52 22.7w 535987 F51 C~1vYB 2014 02 28.33490 10 01 52.613 +13 56 32.77 22.3w 535987 F51 C~1vYB 2014 02 28.34791 10 01 52.546 +13 56 33.19 22.6w 535987 F51 C~1vYB 2014 03 24.28469 10 00 06.121 +14 04 47.20 23.1G 535987 F51 C~2rYJ 2014 11 27.59843 10 12 17.498 +12 48 01.86 23.1G 535987 F51 C~2rYJ 2014 11 29.55452 10 12 18.138 +12 47 59.40 22.9G 535987 F51 C~2rYJ 2015 01 20.42407 10 10 27.116 +12 58 19.25 22.9w 535987 F51 C~1vYB 2015 01 20.44519 10 10 27.033 +12 58 19.86 22.8w 535987 F51 C~1vYB 2015 01 20.45856 10 10 26.964 +12 58 20.18 23.0w 535987 F51 C~1vYB 2015 01 20.47201 10 10 26.910 +12 58 20.36 22.6w 535987 F51 C~1vYB 2015 01 22.44380 10 10 18.682 +12 59 04.02 22.9w 535987 F51 C~1vYB 2015 01 22.45740 10 10 18.612 +12 59 04.52 22.6w 535987 F51 C~1vYB 2015 01 22.47101 10 10 18.542 +12 59 04.84 22.9w 535987 F51 C~1vYB 2015 01 22.48471 10 10 18.486 +12 59 05.15 22.7w 535987 F51 C~1vYB 2015 02 16.34390 10 08 22.062 +13 09 12.12 22.2w 535987 F51 C~1vYB 2015 02 16.35642 10 08 22.004 +13 09 12.37 22.3w 535987 F51 C~1vYB 2015 02 16.36899 10 08 21.921 +13 09 12.75 22.6w 535987 F51 C~1vYB 2015 02 17.38277 10 08 16.908 +13 09 38.15 22.5G 535987 F51 C~2rYJ 2015 02 17.39559 10 08 16.841 +13 09 38.36 22.4G 535987 F51 C~2rYJ 2015 02 17.40846 10 08 16.765 +13 09 38.76 22.8G 535987 F51 C~2rYJ 2015 02 17.42134 10 08 16.708 +13 09 39.06 22.8G 535987 F51 C~2rYJ 2015 03 14.32373 10 06 16.993 +13 19 29.80 22.5G 535987 F51 C~2rYJ 2015 03 15.34050 10 06 12.495 +13 19 50.96 23.0G 535987 F51 C~2rYJ 2016 01 08.47273 10 16 41.033 +12 10 56.98 23.1G 535987 F51 C~2rYJ 2016 01 09.48614 10 16 37.706 +12 11 15.59 22.7G 535987 F51 C~2rYJ 2016 02 11.37713 10 14 18.247 +12 23 41.79 22.8G 535987 F51 C~2rYJ 2016 02 11.38914 10 14 18.179 +12 23 42.43 22.4G 535987 F51 C~2rYJ 2016 02 11.40080 10 14 18.113 +12 23 42.57 22.3G 535987 F51 C~2rYJ 2016 02 11.41241 10 14 18.092 +12 23 42.83 22.3G 535987 F51 C~2rYJ 2016 02 26.51138 10 13 03.534 +12 30 07.76 22.7G 535987 F51 C~2rYJ 2016 03 06.32557 10 12 20.729 +12 33 43.28 23.0G 535987 F51 C~2rYJ 2016 03 06.33726 10 12 20.672 +12 33 43.46 22.7G 535987 F51 C~2rYJ 2016 03 06.34891 10 12 20.619 +12 33 43.91 22.3G 535987 F51 C~2rYJ 2016 03 06.36066 10 12 20.555 +12 33 44.28 23.2G 535987 F51 C~2rYJ 2016 03 08.33125 10 12 11.227 +12 34 30.40 22.5G 535987 F51 C~2rYJ 2016 03 28.27088 10 10 45.645 +12 41 22.36 23.0G 535987 F51 C~2rYJ 2016 05 05.30931 10 09 17.193 +12 47 02.61 22.7G 535987 F51 C~2rYJ 2016 05 05.32146 10 09 17.178 +12 47 02.32 22.8G 535987 F51 C~2rYJ 2016 05 05.34535 10 09 17.163 +12 47 02.46 22.5G 535987 F51 C~2rYJ 2017 01 27.57908 10 20 55.179 +11 33 43.45 23.5G 535987 F51 C~2rYJ 2017 01 27.59138 10 20 55.110 +11 33 43.49 22.1G 535987 F51 C~2rYJ 2017 01 27.60366 10 20 55.046 +11 33 44.18 22.6G 535987 F51 C~2rYJ 2017 01 27.61604 10 20 54.995 +11 33 44.42 22.8G 535987 F51 C~2rYJ 2017 03 05.37160 10 17 58.318 +11 49 16.00 22.9G 535987 F51 C~2rYJ 2017 03 19.42054 10 16 53.512 +11 54 42.50 23.4G 535987 F51 C~2rYJ 2017 10 30.61444 10 27 28.603 +10 43 54.95 22.9G 535987 F51 C~2rYJ 2018 01 15.47118 10 27 16.448 +10 44 17.76 22.6G 535987 F51 C~2rYJ 2018 01 15.48349 10 27 16.407 +10 44 18.08 22.7G 535987 F51 C~2rYJ 2018 01 15.49585 10 27 16.370 +10 44 18.37 22.7G 535987 F51 C~2rYJ 2018 01 15.50829 10 27 16.325 +10 44 18.59 22.9G 535987 F51 C~2rYJ 2018 02 12.40519 10 25 15.933 +10 55 13.21 22.7G 535987 F51 C~2rYJ 2018 02 12.41690 10 25 15.869 +10 55 13.63 22.7G 535987 F51 C~2rYJ 2018 02 12.42861 10 25 15.807 +10 55 14.08 22.0G 535987 F51 C~2rYJ 2018 02 12.44041 10 25 15.776 +10 55 14.45 22.2G 535987 F51 C~2rYJ 2018 03 18.33865 10 22 31.943 +11 09 34.77 22.4G 535987 F51 C~2rYJ 2021 02 15.338140 10 41 47.991 +08 37 02.07 22.3G 535987 G37 C~4fMP 2021 02 15.413830 10 41 47.627 +08 37 04.76 535987 G37 C~4fMP 2021 02 15.498100 10 41 47.198 +08 37 06.77 535987 G37 C~4fMP 2022 02 24.394280 10 46 43.921 +07 53 01.40 22.4w 535987 F52 C~5V3l 2022 02 24.406493 10 46 43.859 +07 53 01.83 22.4w 535987 F52 C~5V3l 2022 02 24.423179 10 46 43.794 +07 53 02.33 22.3w 535987 F52 C~5V3l
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 -0.31 0.00 0.11
2 0.6661 0.00 -0.07 0.00 -0.03
3 0.6661 0.00 0.08 0.00 -0.15
4 0.6662 0.00 0.09 0.00 0.13
5 0.6688 0.00 -0.08 0.00 -0.59
6 0.9911 0.00 0.05 0.00 -0.01
7 1.4109 0.00 0.02 0.00 -0.19
8 1.6764 0.00 0.22 0.00 -0.09
9 1.6792 0.00 -0.22 0.00 0.00
10 1.7087 0.00 0.09 0.00 -0.03
11 3.6528 0.00 -0.12 0.00 -0.01
12 3.7237 0.00 -0.03 0.00 -0.12
13 3.7402 0.00 -0.06 0.00 0.20
14 3.7455 0.00 0.02 0.00 -0.04
15 3.7455 0.00 0.05 0.00 0.07
16 3.7456 0.00 0.10 0.00 0.01
17 3.7456 0.00 0.06 0.00 0.12
18 3.8111 0.00 0.10 0.00 0.20
19 4.4910 0.00 -0.02 0.00 -0.02
20 4.4963 0.00 0.04 0.00 -0.10
21 4.6384 0.00 0.07 0.00 0.11
22 4.6384 0.00 0.16 0.00 0.25
23 4.6384 0.00 -0.03 0.00 0.27
24 4.6385 0.00 0.01 0.00 0.16
25 4.6439 0.00 0.14 0.00 -0.16
26 4.6439 0.00 -0.03 0.00 0.03
27 4.6440 0.00 -0.20 0.00 0.04
28 4.6440 0.00 -0.15 0.00 0.04
29 4.7121 0.00 0.06 0.00 0.17
30 4.7121 0.00 0.14 0.00 0.10
31 4.7121 0.00 -0.16 0.00 0.17
32 4.7149 0.00 0.02 0.00 0.00
33 4.7149 0.00 -0.01 0.00 -0.11
34 4.7150 0.00 -0.18 0.00 -0.04
35 4.7150 0.00 -0.06 0.00 -0.06
36 4.7832 0.00 -0.31 0.00 0.19
37 4.7860 0.00 0.10 0.00 -0.11
38 5.6049 0.00 -0.16 0.00 0.01
39 5.6077 0.00 -0.24 0.00 0.42
40 5.6978 0.00 0.27 0.00 -0.07
41 5.6978 0.00 0.14 0.00 0.26
42 5.6978 0.00 0.01 0.00 0.10
43 5.6979 0.00 0.56 0.00 0.07
44 5.7392 0.00 -0.12 0.00 0.25
45 5.7633 0.00 -0.03 0.00 -0.12
46 5.7634 0.00 -0.03 0.00 -0.22
47 5.7634 0.00 0.02 0.00 -0.05
48 5.7634 0.00 -0.09 0.00 0.04
49 5.7688 0.00 0.02 0.00 -0.28
50 5.8234 0.00 -0.11 0.00 0.02
51 5.9276 0.00 0.16 0.00 0.04
52 5.9276 0.00 0.07 0.00 -0.24
53 5.9277 0.00 0.11 0.00 -0.09
54 6.6593 0.00 0.23 0.00 -0.21
55 6.6593 0.00 0.01 0.00 -0.46
56 6.6594 0.00 -0.13 0.00 -0.05
57 6.6594 0.00 -0.07 0.00 -0.10
58 6.7600 0.00 -0.09 0.00 -0.12
59 6.7985 0.00 -0.10 0.00 0.13
60 7.4151 0.00 0.13 0.00 0.13
61 7.6255 0.00 -0.14 0.00 -0.08
62 7.6255 0.00 -0.08 0.00 -0.00
63 7.6255 0.00 0.05 0.00 0.04
64 7.6256 0.00 0.05 0.00 0.02
65 7.7020 0.00 -0.02 0.00 -0.01
66 7.7020 0.00 -0.11 0.00 0.10
67 7.7020 0.00 -0.18 0.00 0.25
68 7.7021 0.00 0.23 0.00 0.31
69 7.7949 0.00 -0.13 0.00 -0.03
70 10.7107 0.00 -0.01 0.00 -0.57
71 10.7109 0.00 0.09 0.00 0.09
72 10.7111 0.00 -0.16 0.00 -0.14
73 11.7348 0.00 -0.09 0.00 -0.04
74 11.7348 0.00 -0.10 0.00 0.05
75 11.7349 0.00 0.19 0.00 0.09
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.
535987 quality flag:3 Type: SCATNEAR SCATNEAR SCATNEAR axisobj 46.495 46.495 46.495 ecceobj 0.230 0.230 0.230 incobj 7.686 7.686 7.686 qmin 34.961 34.897 34.943 qmax 58.832 58.751 59.022 amean 46.557 46.478 46.611 amin 46.034 45.612 46.166 amax 47.186 47.130 47.209 emean 0.230 0.229 0.231 emin 0.213 0.211 0.213 emax 0.248 0.248 0.250 imean 8.766 8.727 8.740 imin 7.650 7.659 7.645 imax 9.786 9.716 9.743 excite_mean 0.276 0.275 0.277 fracstop 1.000 1.000 1.000 cjmean 3.038 3.038 3.039 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 180.8 183.6 181.6 kozaiamp 180.0 180.0 180.0