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: 592487 # Created Wed Jul 17 01:07:39 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 98 observations of 98 # Arc: 13.11y # First observation: 2010/10/09 # Last observation: 2023/11/19 # Chi-squared of fit: 64.10 DOF: 190 RMS: 0.14 # Min/Max residuals: -0.39 0.49 # Exact a, adot, b, bdot, g, gdot: 1.604898E-05 2.373951E-02 -1.641668E-06 -1.606898E-03 2.401115E-02 1.995226E-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 -5.977381 53.946602 0.611817 -0.081762 -0.780721 2455478.935036 # Heliocentric elements and errors Epoch: 2455478.5000 = 2010/10/09 Mean Anomaly: 42.85149 +/- 0.000 Argument of Peri: 185.09015 +/- 0.000 Long of Asc Node: 177.12983 +/- 0.000 Inclination: 7.06631 +/- 0.000 Eccentricity: 0.09673930 +/- 0.0000 Semi-Major Axis: 45.43743718 +/- 0.0000 Time of Perihelion: 2442162.2300 +/- 0.0 Perihelion: 41.04185123 +/- 0.0000 Aphelion: 49.83302312 +/- 0.0000 Period (y) 306.2873 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 25.33809894 +/- 0.0000 Ecliptic Y 33.76120924 +/- 0.0000 Ecliptic Z -4.33704614 +/- 0.0000 Ecliptic XDOT -0.00206636 +/- 0.0000 Ecliptic YDOT 0.00176697 +/- 0.0000 Ecliptic ZDOT -0.00020593 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 42.43400227 +/- 0.0000 Geocenter to KBO 41.64728903 +/- 0.0000 # Hcoef: 5.90
The following table shows the complete astrometric record for 592487. 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 (592487) followed by the observatory code and reference code for the source of the astrometry.
2010 10 09.43427 03 32 20.163 +12 57 42.02 22.3w 592487 F51 C~1vXq 2010 10 09.45032 03 32 20.113 +12 57 41.54 22.5w 592487 F51 C~1vXq 2010 10 09.46646 03 32 20.060 +12 57 41.33 22.3w 592487 F51 C~1vXq 2010 10 09.48423 03 32 19.996 +12 57 41.03 22.1w 592487 F51 C~1vXq 2010 11 08.48828 03 30 12.095 +12 47 44.74 22.2w 592487 F51 C~1vXq 2010 11 08.50100 03 30 12.030 +12 47 44.40 22.4w 592487 F51 C~1vXq 2010 11 08.51518 03 30 11.974 +12 47 44.30 22.4w 592487 F51 C~1vXq 2010 11 08.52784 03 30 11.906 +12 47 43.94 22.1w 592487 F51 C~1vXq 2011 11 26.47948 03 34 19.111 +12 56 44.96 21.0G 592487 F51 C~2rYD 2012 03 14.23916 03 31 57.306 +12 59 27.29 21.9G 592487 F51 C~2rYD 2012 10 21.55071 03 42 34.189 +13 21 22.14 22.3w 592487 F51 C~1vXq 2012 10 21.56677 03 42 34.111 +13 21 21.64 22.1w 592487 F51 C~1vXq 2012 10 21.58282 03 42 34.067 +13 21 21.39 22.2w 592487 F51 C~1vXq 2012 10 21.59894 03 42 33.979 +13 21 21.24 22.1w 592487 F51 C~1vXq 2012 11 07.37053 03 41 19.380 +13 16 02.39 22.0w 592487 F51 C~1vXq 2012 11 07.38573 03 41 19.314 +13 16 02.04 22.1w 592487 F51 C~1vXq 2012 11 07.41599 03 41 19.177 +13 16 01.91 21.9w 592487 F51 C~1vXq 2012 12 29.41527 03 37 27.322 +13 04 08.84 21.9G 592487 F51 C~2rYD 2013 01 17.20908 03 36 36.717 +13 03 14.51 22.3G 592487 F51 C~2rYD 2013 03 05.23888 03 36 50.774 +13 10 21.51 22.2w 592487 F51 C~1vXq 2013 03 05.24285 03 36 50.802 +13 10 21.93 22.4w 592487 F51 C~1vXq 2013 03 05.24681 03 36 50.807 +13 10 22.11 22.5w 592487 F51 C~1vXq 2013 03 05.25076 03 36 50.807 +13 10 22.00 22.4w 592487 F51 C~1vXq 2013 08 24.58583 03 49 55.381 +13 48 30.48 21.9G 592487 F51 C~2rYD 2013 11 09.51066 03 46 41.774 +13 28 45.09 22.0w 592487 F51 C~1vXq 2013 11 09.52573 03 46 41.701 +13 28 44.88 22.1w 592487 F51 C~1vXq 2013 11 09.54084 03 46 41.631 +13 28 44.69 22.0w 592487 F51 C~1vXq 2013 11 09.55599 03 46 41.546 +13 28 44.30 22.3w 592487 F51 C~1vXq 2013 11 26.33901 03 45 20.595 +13 23 59.67 22.0w 592487 F51 C~1vXq 2013 11 26.35433 03 45 20.516 +13 23 59.46 22.2w 592487 F51 C~1vXq 2013 11 26.36971 03 45 20.440 +13 23 59.17 22.1w 592487 F51 C~1vXq 2014 10 07.41957 03 54 26.392 +13 51 24.88 22.4G 592487 F51 C~2rYD 2014 10 25.52411 03 53 20.428 +13 46 04.97 22.6G 592487 F51 C~2rYD 2014 11 18.34485 03 51 31.143 +13 39 04.75 22.6G 592487 F51 C~2rYD 2014 11 20.47906 03 51 20.761 +13 38 29.85 22.2w 592487 F51 C~1vXq 2014 11 20.49031 03 51 20.689 +13 38 29.55 22.2w 592487 F51 C~1vXq 2014 11 20.50153 03 51 20.622 +13 38 29.41 22.2w 592487 F51 C~1vXq 2014 11 20.51273 03 51 20.599 +13 38 29.18 21.9w 592487 F51 C~1vXr 2014 11 26.30470 03 50 52.444 +13 36 57.58 21.9w 592487 F51 C~1vXr 2014 11 26.31593 03 50 52.386 +13 36 57.43 22.4w 592487 F51 C~1vXr 2014 11 26.32712 03 50 52.333 +13 36 57.30 21.9w 592487 F51 C~1vXr 2014 11 26.33832 03 50 52.287 +13 36 56.97 22.1w 592487 F51 C~1vXr 2015 01 17.30380 03 47 31.277 +13 29 45.69 22.3w 592487 F51 C~1vXr 2015 01 17.31761 03 47 31.246 +13 29 45.78 22.4w 592487 F51 C~1vXr 2015 01 17.33146 03 47 31.214 +13 29 45.84 22.3w 592487 F51 C~1vXr 2015 01 17.34530 03 47 31.163 +13 29 46.00 22.3w 592487 F51 C~1vXr 2015 07 26.58565 03 59 36.191 +14 13 48.37 22.0w 592487 F51 C~1vXr 2015 07 26.59616 03 59 36.248 +14 13 48.33 22.1w 592487 F51 C~1vXr 2015 07 26.60138 03 59 36.240 +14 13 48.34 22.2w 592487 F51 C~1vXr 2015 10 08.47324 03 59 51.546 +14 03 09.75 22.4G 592487 F51 C~2rYD 2015 10 08.48538 03 59 51.524 +14 03 09.75 22.7G 592487 F51 C~2rYD 2015 10 08.49754 03 59 51.463 +14 03 09.26 22.0G 592487 F51 C~2rYD 2015 10 08.50967 03 59 51.434 +14 03 09.12 22.0G 592487 F51 C~2rYD 2015 10 09.48259 03 59 48.467 +14 02 53.02 22.0G 592487 F51 C~2rYE 2015 11 07.37401 03 57 54.074 +13 54 31.47 21.8G 592487 F51 C~2rYE 2015 11 18.35499 03 57 01.889 +13 51 26.94 22.0G 592487 F51 C~2rYE 2015 12 01.46296 03 55 58.175 +13 48 08.74 22.2G 592487 F51 C~2rYE 2015 12 03.31473 03 55 49.287 +13 47 43.16 22.5G 592487 F51 C~2rYE 2015 12 03.32570 03 55 49.234 +13 47 42.86 22.4G 592487 F51 C~2rYE 2015 12 03.33672 03 55 49.200 +13 47 42.76 22.3G 592487 F51 C~2rYE 2015 12 03.34778 03 55 49.145 +13 47 42.64 22.4G 592487 F51 C~2rYE 2015 12 12.44713 03 55 06.492 +13 45 48.99 21.9G 592487 F51 C~2rYE 2015 12 12.45889 03 55 06.432 +13 45 48.84 21.9G 592487 F51 C~2rYE 2015 12 12.47067 03 55 06.385 +13 45 48.74 22.4G 592487 F51 C~2rYE 2015 12 12.48233 03 55 06.331 +13 45 48.41 22.0G 592487 F51 C~2rYE 2016 01 13.33689 03 53 07.500 +13 42 18.99 22.3G 592487 F51 C~2rYE 2016 01 13.34833 03 53 07.483 +13 42 18.64 21.6G 592487 F51 C~2rYE 2016 01 13.35980 03 53 07.473 +13 42 18.88 22.5G 592487 F51 C~2rYE 2016 01 13.37123 03 53 07.438 +13 42 18.72 22.3G 592487 F51 C~2rYE 2016 01 31.28772 03 52 33.685 +13 42 51.23 22.5G 592487 F51 C~2rYE 2016 10 28.58781 04 04 02.414 +14 08 46.90 22.2G 592487 F51 C~2rYE 2016 11 04.44429 04 03 32.400 +14 06 49.94 22.4G 592487 F51 C~2rYE 2017 08 05.60993 04 10 45.896 +14 35 36.86 22.5G 592487 F51 C~2rYE 2017 09 22.52018 04 11 17.607 +14 29 17.37 22.2G 592487 F51 C~2rYE 2017 09 22.53255 04 11 17.612 +14 29 17.17 21.9G 592487 F51 C~2rYE 2017 09 22.54486 04 11 17.577 +14 29 17.05 22.2G 592487 F51 C~2rYE 2017 09 22.55720 04 11 17.563 +14 29 16.78 21.7G 592487 F51 C~2rYE 2017 10 19.61071 04 10 05.602 +14 22 25.48 22.4G 592487 F51 C~2rYE 2017 10 27.42478 04 09 35.231 +14 20 16.29 22.4G 592487 F51 C~2rYE 2017 10 27.43649 04 09 35.192 +14 20 15.87 22.0G 592487 F51 C~2rYE 2017 10 27.44818 04 09 35.127 +14 20 15.84 22.3G 592487 F51 C~2rYE 2017 10 27.45986 04 09 35.079 +14 20 15.33 22.6G 592487 F51 C~2rYE 2017 11 19.38215 04 07 50.785 +14 14 06.75 22.4G 592487 F51 C~2rYE 2017 11 19.39423 04 07 50.721 +14 14 06.38 22.2G 592487 F51 C~2rYE 2017 11 19.40625 04 07 50.670 +14 14 06.45 22.1G 592487 F51 C~2rYE 2017 11 19.41830 04 07 50.605 +14 14 06.06 22.5G 592487 F51 C~2rYE 2017 12 08.45594 04 06 18.211 +14 09 49.52 23.5G 592487 F51 C~2rYE 2017 12 08.46846 04 06 18.141 +14 09 49.23 22.3G 592487 F51 C~2rYE 2017 12 08.48093 04 06 18.097 +14 09 49.29 22.5G 592487 F51 C~2rYE 2017 12 08.49337 04 06 18.032 +14 09 49.20 22.6G 592487 F51 C~2rYE 2020 12 10.48642 04 22 25.389 +14 40 39.70 22.1w 592487 F51 C~4NuM 2020 12 10.49743 04 22 25.342 +14 40 39.52 21.9w 592487 F51 C~4NuM 2020 12 10.51958 04 22 25.214 +14 40 39.44 21.9w 592487 F51 C~4NuM 2021 08 10.597494 04 32 05.617 +15 13 13.03 22.3w 592487 F51 C~4yVJ 2021 08 10.602890 04 32 05.632 +15 13 13.14 22.3w 592487 F51 C~4yVJ 2021 08 10.613769 04 32 05.672 +15 13 13.07 22.5w 592487 F51 C~4yVJ 2023 11 19.87120 04 40 23.89 +15 11 17.9 22.3w 592487 O18 C~7b6c 2023 11 19.87667 04 40 23.86 +15 11 17.7 22.3w 592487 O18 C~7b6c
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 -0.12 0.00 0.10
2 0.0000 0.00 0.00 0.00 -0.08
3 0.0001 0.00 0.08 0.00 0.02
4 0.0001 0.00 0.08 0.00 0.06
5 0.0823 0.00 -0.06 0.00 0.16
6 0.0823 0.00 -0.12 0.00 0.07
7 0.0824 0.00 0.07 0.00 0.25
8 0.0824 0.00 -0.03 0.00 0.14
9 1.1309 0.00 -0.00 0.00 -0.15
10 1.4286 0.00 -0.01 0.00 -0.15
11 2.0345 0.00 -0.13 0.00 0.07
12 2.0346 0.00 -0.29 0.00 -0.13
13 2.0346 0.00 0.06 0.00 -0.07
14 2.0347 0.00 -0.25 0.00 0.09
15 2.0806 0.00 -0.17 0.00 0.03
16 2.0806 0.00 -0.07 0.00 -0.03
17 2.0807 0.00 0.05 0.00 0.40
18 2.2231 0.00 -0.00 0.00 0.15
19 2.2745 0.00 0.49 0.00 0.34
20 2.4033 0.00 -0.14 0.00 -0.31
21 2.4033 0.00 0.14 0.00 0.05
22 2.4033 0.00 0.07 0.00 0.16
23 2.4033 0.00 -0.08 0.00 -0.01
24 2.8752 0.00 0.34 0.00 -0.20
25 3.0858 0.00 0.01 0.00 -0.10
26 3.0858 0.00 -0.00 0.00 -0.04
27 3.0858 0.00 0.04 0.00 0.05
28 3.0859 0.00 -0.14 0.00 -0.07
29 3.1318 0.00 0.03 0.00 -0.09
30 3.1319 0.00 -0.03 0.00 -0.07
31 3.1319 0.00 -0.03 0.00 -0.12
32 3.9945 0.00 0.32 0.00 -0.13
33 4.0441 0.00 0.02 0.00 -0.13
34 4.1093 0.00 0.06 0.00 0.02
35 4.1151 0.00 0.03 0.00 0.19
36 4.1151 0.00 -0.21 0.00 0.08
37 4.1152 0.00 -0.39 0.00 0.12
38 4.1152 0.00 0.10 0.00 0.08
39 4.1311 0.00 0.09 0.00 -0.00
40 4.1311 0.00 0.05 0.00 0.02
41 4.1311 0.00 0.08 0.00 0.06
42 4.1312 0.00 0.22 0.00 -0.10
43 4.2734 0.00 0.05 0.00 -0.14
44 4.2735 0.00 0.06 0.00 -0.05
45 4.2735 0.00 0.05 0.00 0.01
46 4.2735 0.00 -0.25 0.00 0.17
47 4.7944 0.00 -0.22 0.00 -0.02
48 4.7944 0.00 0.09 0.00 -0.08
49 4.7944 0.00 -0.30 0.00 -0.08
50 4.9967 0.00 0.05 0.00 -0.04
51 4.9967 0.00 0.28 0.00 0.16
52 4.9968 0.00 -0.07 0.00 -0.13
53 4.9968 0.00 0.06 0.00 -0.07
54 4.9994 0.00 0.14 0.00 -0.04
55 5.0785 0.00 -0.11 0.00 -0.01
56 5.1086 0.00 0.03 0.00 -0.18
57 5.1445 0.00 -0.26 0.00 0.10
58 5.1496 0.00 -0.24 0.00 -0.00
59 5.1496 0.00 -0.24 0.00 -0.15
60 5.1496 0.00 0.06 0.00 -0.11
61 5.1497 0.00 0.04 0.00 -0.08
62 5.1746 0.00 0.10 0.00 -0.00
63 5.1746 0.00 0.01 0.00 -0.02
64 5.1746 0.00 0.13 0.00 0.02
65 5.1747 0.00 0.12 0.00 -0.18
66 5.2619 0.00 -0.34 0.00 0.13
67 5.2619 0.00 -0.13 0.00 -0.20
68 5.2619 0.00 0.19 0.00 0.06
69 5.2620 0.00 0.14 0.00 -0.09
70 5.3110 0.00 -0.08 0.00 0.01
71 6.0538 0.00 0.13 0.00 0.19
72 6.0726 0.00 0.07 0.00 -0.02
73 6.8232 0.00 0.13 0.00 0.06
74 6.9544 0.00 -0.25 0.00 0.01
75 6.9544 0.00 0.13 0.00 -0.03
76 6.9544 0.00 -0.09 0.00 0.01
77 6.9545 0.00 -0.00 0.00 -0.09
78 7.0285 0.00 0.47 0.00 0.02
79 7.0499 0.00 0.00 0.00 0.14
80 7.0500 0.00 0.15 0.00 -0.08
81 7.0500 0.00 -0.09 0.00 0.08
82 7.0500 0.00 -0.08 0.00 -0.24
83 7.1128 0.00 0.02 0.00 -0.06
84 7.1128 0.00 -0.05 0.00 -0.25
85 7.1129 0.00 0.08 0.00 -0.00
86 7.1129 0.00 -0.00 0.00 -0.21
87 7.1650 0.00 0.00 0.00 -0.01
88 7.1650 0.00 -0.14 0.00 -0.15
89 7.1651 0.00 0.10 0.00 0.05
90 7.1651 0.00 0.02 0.00 0.11
91 10.1713 0.00 0.13 0.00 0.00
92 10.1713 0.00 0.22 0.00 -0.06
93 10.1713 0.00 -0.08 0.00 0.08
94 10.8369 0.00 -0.11 0.00 0.18
95 10.8369 0.00 -0.12 0.00 0.31
96 10.8369 0.00 0.03 0.00 0.27
97 13.1128 0.00 -0.03 0.00 0.10
98 13.1128 0.00 -0.08 0.00 -0.03
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.
592487 quality flag:3 Type: CLASSICAL CLASSICAL CLASSICAL axisobj 45.652 45.652 45.652 ecceobj 0.100 0.100 0.100 incobj 7.060 7.060 7.060 qmin 40.168 40.185 40.184 qmax 50.679 50.702 50.647 amean 45.273 45.273 45.273 amin 44.912 44.912 44.908 amax 45.674 45.677 45.669 emean 0.096 0.096 0.096 emin 0.083 0.083 0.083 emax 0.110 0.110 0.110 imean 7.173 7.173 7.173 imin 6.656 6.656 6.656 imax 7.706 7.705 7.706 excite_mean 0.158 0.158 0.158 fracstop 1.000 1.000 1.000 cjmean 3.086 3.086 3.086 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 181.2 180.9 181.2 kozaiamp 180.0 179.9 180.0