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: 535022 # Created Sun Nov 24 02:07:27 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 114 observations of 114 # Arc: 13.19y # First observation: 2011/01/30 # Last observation: 2024/04/09 # Chi-squared of fit: 72.68 DOF: 222 RMS: 0.14 # Min/Max residuals: -0.60 0.44 # Exact a, adot, b, bdot, g, gdot: 1.650238E-05 2.387538E-02 -1.284624E-06 -1.803560E-03 2.448565E-02 -1.052143E-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 -5.744434 149.249797 0.323126 -0.093471 -0.929188 2455591.917476 # Heliocentric elements and errors Epoch: 2455592.5000 = 2011/01/31 Mean Anomaly: 284.05248 +/- 0.000 Argument of Peri: 314.04233 +/- 0.000 Long of Asc Node: 276.71228 +/- 0.000 Inclination: 7.10509 +/- 0.000 Eccentricity: 0.05134478 +/- 0.0000 Semi-Major Axis: 42.18637433 +/- 0.0000 Time of Perihelion: 2476706.3698 +/- 0.0 Perihelion: 40.02032429 +/- 0.0000 Aphelion: 44.35242437 +/- 0.0000 Period (y) 274.0101 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X -35.55559774 +/- 0.0000 Ecliptic Y 21.53067045 +/- 0.0000 Ecliptic Z -4.08782765 +/- 0.0000 Ecliptic XDOT -0.00124810 +/- 0.0000 Ecliptic YDOT -0.00235836 +/- 0.0000 Ecliptic ZDOT -0.00018886 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 41.76701189 +/- 0.0000 Geocenter to KBO 40.84030360 +/- 0.0000 # Hcoef: 6.16
The following table shows the complete astrometric record for 535022. 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 (535022) followed by the observatory code and reference code for the source of the astrometry.
2011 01 30.41671 09 57 25.696 +06 20 44.82 22.2w 535022 F51 C~1vXr 2011 01 30.43279 09 57 25.618 +06 20 44.95 22.5w 535022 F51 C~1vXr 2011 01 30.44758 09 57 25.561 +06 20 45.42 22.4w 535022 F51 C~1vXr 2011 02 04.44855 09 57 02.845 +06 22 30.26 22.5w 535022 F51 C~1vXr 2011 02 04.46284 09 57 02.769 +06 22 30.70 22.3w 535022 F51 C~1vXr 2011 02 04.47720 09 57 02.697 +06 22 30.89 22.4w 535022 F51 C~1vXr 2011 02 04.49160 09 57 02.637 +06 22 31.17 22.4w 535022 F51 C~1vXr 2011 02 05.43580 09 56 58.293 +06 22 51.87 22.5G 535022 F51 C~2rYE 2011 02 05.45098 09 56 58.214 +06 22 52.00 22.1G 535022 F51 C~2rYE 2011 02 05.46543 09 56 58.147 +06 22 52.33 22.3G 535022 F51 C~2rYE 2011 02 05.47975 09 56 58.079 +06 22 52.64 22.1G 535022 F51 C~2rYE 2012 02 13.48192 10 01 23.578 +05 51 41.53 22.9G 535022 F51 C~2rYE 2012 02 14.37198 10 01 19.397 +05 52 02.47 21.9w 535022 F51 C~1vXr 2012 02 14.38614 10 01 19.320 +05 52 03.05 22.1w 535022 F51 C~1vXr 2012 02 14.40033 10 01 19.258 +05 52 03.15 22.2w 535022 F51 C~1vXr 2013 02 10.48963 10 06 36.259 +05 16 23.05 21.9G 535022 F51 C~2rYE 2013 02 21.45737 10 05 44.795 +05 20 51.24 21.7G 535022 F51 C~2rYE 2013 03 04.29985 10 04 54.630 +05 25 32.11 22.3w 535022 F51 C~1vXr 2013 03 04.31408 10 04 54.559 +05 25 32.40 22.2w 535022 F51 C~1vXr 2013 03 04.32832 10 04 54.493 +05 25 32.69 22.1w 535022 F51 C~1vXr 2013 03 04.34258 10 04 54.433 +05 25 33.15 22.1w 535022 F51 C~1vXr 2014 01 11.58820 10 13 43.146 +04 32 37.60 21.7G 535022 F51 C~2rYE 2014 02 23.37101 10 10 39.943 +04 46 52.51 22.8G 535022 F51 C~2rYE 2014 02 23.38227 10 10 39.887 +04 46 52.79 22.3G 535022 F51 C~2rYE 2014 03 06.36611 10 09 49.204 +04 51 41.46 22.8G 535022 F51 C~2rYE 2014 11 25.63111 10 19 49.266 +03 59 16.63 22.8G 535022 F51 C~2rYE 2014 11 27.61454 10 19 50.557 +03 58 48.49 22.1w 535022 F51 C~1vXr 2014 11 27.62483 10 19 50.571 +03 58 48.17 22.4w 535022 F51 C~1vXr 2014 11 27.63512 10 19 50.572 +03 58 47.80 22.3w 535022 F51 C~1vXr 2014 11 27.64543 10 19 50.580 +03 58 48.03 22.3w 535022 F51 C~1vXr 2015 01 16.47922 10 18 28.539 +03 58 46.88 22.1w 535022 F51 C~1vXr 2015 01 16.49064 10 18 28.492 +03 58 47.11 22.3w 535022 F51 C~1vXr 2015 01 16.50209 10 18 28.462 +03 58 47.17 22.3w 535022 F51 C~1vXr 2015 01 16.51350 10 18 28.408 +03 58 47.41 22.4w 535022 F51 C~1vXr 2015 01 18.47278 10 18 21.302 +03 59 14.22 22.2w 535022 F51 C~1vXr 2015 01 18.48570 10 18 21.249 +03 59 14.66 22.2w 535022 F51 C~1vXr 2015 01 18.49860 10 18 21.202 +03 59 14.60 22.2w 535022 F51 C~1vXr 2015 01 18.51155 10 18 21.149 +03 59 14.79 21.8w 535022 F51 C~1vXr 2015 03 14.36329 10 14 18.184 +04 20 16.37 21.9w 535022 F51 C~1vXr 2015 03 14.38753 10 14 18.078 +04 20 17.02 22.4w 535022 F51 C~1vXr 2015 03 14.39965 10 14 18.061 +04 20 17.38 22.2w 535022 F51 C~1vXr 2015 03 15.37624 10 14 13.848 +04 20 43.31 22.8G 535022 F51 C~2rYE 2015 03 15.40094 10 14 13.732 +04 20 43.96 22.3G 535022 F51 C~2rYE 2015 12 09.61268 10 24 48.501 +03 22 07.57 22.7G 535022 F51 C~2rYE 2015 12 09.62205 10 24 48.503 +03 22 07.52 22.8G 535022 F51 C~2rYE 2015 12 09.63146 10 24 48.506 +03 22 07.36 22.7G 535022 F51 C~2rYE 2015 12 23.58367 10 24 33.878 +03 21 08.13 21.5G 535022 F51 C~2rYE 2016 01 04.59966 10 24 07.841 +03 21 46.13 22.1G 535022 F51 C~2rYE 2016 01 04.61169 10 24 07.805 +03 21 46.24 22.4G 535022 F51 C~2rYE 2016 01 04.62375 10 24 07.798 +03 21 46.14 21.8G 535022 F51 C~2rYE 2016 01 04.63581 10 24 07.742 +03 21 46.26 22.4G 535022 F51 C~2rYE 2016 01 14.60702 10 23 37.685 +03 23 18.13 22.6G 535022 F51 C~2rYE 2016 01 14.61823 10 23 37.637 +03 23 18.33 21.5G 535022 F51 C~2rYE 2016 01 14.62950 10 23 37.612 +03 23 18.50 21.7G 535022 F51 C~2rYE 2016 01 14.64070 10 23 37.589 +03 23 18.71 21.9G 535022 F51 C~2rYE 2016 01 17.57315 10 23 27.475 +03 23 55.47 22.0G 535022 F51 C~2rYE 2016 01 17.58526 10 23 27.428 +03 23 55.63 22.2G 535022 F51 C~2rYE 2016 01 17.59728 10 23 27.382 +03 23 55.70 22.3G 535022 F51 C~2rYE 2016 01 17.60929 10 23 27.340 +03 23 55.91 22.1G 535022 F51 C~2rYE 2016 02 06.47802 10 22 07.059 +03 29 47.15 22.2G 535022 F51 C~2rYE 2016 02 15.42310 10 21 26.386 +03 33 12.40 21.9G 535022 F51 C~2rYE 2016 03 07.34623 10 19 49.317 +03 42 19.23 22.5G 535022 F51 C~2rYE 2016 03 07.35789 10 19 49.274 +03 42 19.39 22.5G 535022 F51 C~2rYE 2016 03 07.36956 10 19 49.214 +03 42 19.85 22.7G 535022 F51 C~2rYE 2016 03 31.34607 10 18 11.366 +03 52 59.74 22.2G 535022 F51 C~2rYE 2016 03 31.35831 10 18 11.320 +03 53 00.05 22.1G 535022 F51 C~2rYE 2016 03 31.37055 10 18 11.290 +03 53 00.36 22.3G 535022 F51 C~2rYE 2016 03 31.38283 10 18 11.239 +03 53 00.83 22.2G 535022 F51 C~2rYE 2016 04 29.25235 10 16 59.396 +04 03 06.08 22.6G 535022 F51 C~2rYE 2016 04 29.26434 10 16 59.374 +04 03 06.01 22.7G 535022 F51 C~2rYE 2016 04 29.27636 10 16 59.365 +04 03 06.63 22.5G 535022 F51 C~2rYE 2016 04 29.28836 10 16 59.348 +04 03 06.29 22.8G 535022 F51 C~2rYE 2016 12 13.57137 10 29 44.014 +02 46 45.87 22.0G 535022 F51 C~2rYE 2017 01 03.61753 10 29 09.335 +02 46 39.06 22.3G 535022 F51 C~2rYE 2017 01 03.62894 10 29 09.291 +02 46 39.11 22.8G 535022 F51 C~2rYE 2017 01 03.64029 10 29 09.262 +02 46 39.12 22.7G 535022 F51 C~2rYE 2017 01 03.65167 10 29 09.230 +02 46 39.17 22.4G 535022 F51 C~2rYE 2017 03 22.31175 10 23 49.497 +03 13 43.86 22.2G 535022 F51 C~2rYE 2017 03 22.32438 10 23 49.450 +03 13 44.37 21.9G 535022 F51 C~2rYE 2017 03 22.33704 10 23 49.386 +03 13 44.74 22.7G 535022 F51 C~2rYE 2018 01 13.51422 10 33 43.416 +02 12 39.37 23.2G 535022 F51 C~2rYE 2018 01 13.52596 10 33 43.378 +02 12 39.26 22.5G 535022 F51 C~2rYE 2018 01 13.53775 10 33 43.342 +02 12 39.38 22.1G 535022 F51 C~2rYE 2018 01 13.54963 10 33 43.286 +02 12 39.24 22.7G 535022 F51 C~2rYE 2018 01 20.56164 10 33 19.707 +02 14 05.00 22.1G 535022 F51 C~2rYE 2018 01 20.57366 10 33 19.661 +02 14 05.13 22.2G 535022 F51 C~2rYE 2018 01 20.58567 10 33 19.621 +02 14 05.33 21.9G 535022 F51 C~2rYE 2018 01 20.59768 10 33 19.586 +02 14 05.45 22.1G 535022 F51 C~2rYE 2018 02 21.43875 10 31 03.949 +02 25 00.36 22.5G 535022 F51 C~2rYE 2018 02 21.45158 10 31 03.878 +02 25 00.68 22.4G 535022 F51 C~2rYE 2018 02 21.47737 10 31 03.752 +02 25 01.10 23.0G 535022 F51 C~2rYE 2018 03 11.38587 10 29 41.067 +02 33 06.84 22.9G 535022 F51 C~2rYE 2018 03 20.35714 10 29 02.030 +02 37 17.05 23.4G 535022 F51 C~2rYE 2019 04 07.33445 10 32 57.69 +02 09 44.5 23.4g 535022 T09 C~8Lo7 2019 04 07.35805 10 32 57.61 +02 09 45.0 23.5g 535022 T09 C~8Lo7 2019 04 07.37710 10 32 57.55 +02 09 45.7 23.4g 535022 T09 C~8Lo7 2019 04 08.23806 10 32 54.70 +02 10 07.7 22.4y 535022 T09 C~7gdc 2019 04 08.26980 10 32 54.58 +02 10 08.2 21.9y 535022 T09 C~7gdc 2019 04 08.30006 10 32 54.48 +02 10 09.2 22.1y 535022 T09 C~7gdc 2019 04 08.32999 10 32 54.39 +02 10 09.7 22.0y 535022 T09 C~7gdc 2019 04 08.37381 10 32 54.23 +02 10 10.9 21.7y 535022 T09 C~7gdc 2019 05 08.36005 10 31 48.57 +02 20 26.2 21.9i 535022 T09 C~8Pen 2019 05 08.38956 10 31 48.53 +02 20 26.5 22.0i 535022 T09 C~8Pen 2019 05 08.39224 10 31 48.53 +02 20 26.5 22.1i 535022 T09 C~8Pen 2022 02 24.391720 10 51 07.788 +00 03 03.83 22.2w 535022 F52 C~5V3j 2022 02 24.403948 10 51 07.735 +00 03 04.05 22.1w 535022 F52 C~5V3j 2022 02 24.416186 10 51 07.667 +00 03 04.20 22.2w 535022 F52 C~5V3j 2023 01 22.510331 10 58 28.380 -00 43 48.08 22.3w 535022 F52 C~6mow 2023 01 22.523041 10 58 28.329 -00 43 47.95 21.7w 535022 F52 C~6mow 2023 01 22.535791 10 58 28.275 -00 43 47.86 22.2w 535022 F52 C~6mow 2023 01 22.548501 10 58 28.237 -00 43 47.65 22.2w 535022 F52 C~6mow 2024 04 09.346275 10 58 06.516 -00 47 45.09 22.0w 535022 F51 C~7zZ3 2024 04 09.358823 10 58 06.496 -00 47 44.70 22.0w 535022 F51 C~7zZ3 2024 04 09.371341 10 58 06.442 -00 47 44.44 21.9w 535022 F51 C~7zZ3
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 -0.20 0.00 0.10
2 0.0000 0.00 -0.27 0.00 -0.10
3 0.0001 0.00 -0.12 0.00 0.08
4 0.0138 0.00 0.09 0.00 0.11
5 0.0138 0.00 -0.04 0.00 0.24
6 0.0139 0.00 -0.11 0.00 0.12
7 0.0139 0.00 0.00 0.00 0.09
8 0.0165 0.00 0.15 0.00 0.19
9 0.0165 0.00 0.04 0.00 -0.01
10 0.0166 0.00 0.06 0.00 0.00
11 0.0166 0.00 0.05 0.00 -0.00
12 1.0378 0.00 0.21 0.00 0.09
13 1.0403 0.00 0.15 0.00 -0.20
14 1.0403 0.00 0.01 0.00 0.04
15 1.0403 0.00 0.10 0.00 -0.20
16 2.0317 0.00 -0.23 0.00 -0.20
17 2.0617 0.00 -0.11 0.00 0.01
18 2.0914 0.00 0.17 0.00 0.13
19 2.0914 0.00 0.08 0.00 0.04
20 2.0915 0.00 0.08 0.00 -0.04
21 2.0915 0.00 0.16 0.00 0.04
22 2.9491 0.00 -0.16 0.00 -0.41
23 3.0663 0.00 -0.03 0.00 0.09
24 3.0663 0.00 -0.06 0.00 0.08
25 3.0964 0.00 0.17 0.00 -0.09
26 3.8199 0.00 0.19 0.00 -0.25
27 3.8253 0.00 0.08 0.00 0.16
28 3.8253 0.00 0.21 0.00 -0.02
29 3.8254 0.00 0.15 0.00 -0.25
30 3.8254 0.00 0.20 0.00 0.13
31 3.9618 0.00 -0.10 0.00 0.02
32 3.9619 0.00 -0.18 0.00 0.10
33 3.9619 0.00 0.00 0.00 0.00
34 3.9619 0.00 -0.18 0.00 0.09
35 3.9673 0.00 -0.09 0.00 -0.22
36 3.9673 0.00 -0.16 0.00 0.04
37 3.9674 0.00 -0.13 0.00 -0.21
38 3.9674 0.00 -0.20 0.00 -0.20
39 4.1176 0.00 -0.11 0.00 0.27
40 4.1176 0.00 -0.10 0.00 0.26
41 4.1177 0.00 0.44 0.00 0.30
42 4.1204 0.00 -0.04 0.00 -0.01
43 4.1204 0.00 -0.17 0.00 -0.02
44 4.8575 0.00 -0.02 0.00 -0.00
45 4.8575 0.00 0.08 0.00 0.03
46 4.8575 0.00 0.20 0.00 -0.06
47 4.8957 0.00 0.09 0.00 0.00
48 4.9286 0.00 0.09 0.00 0.05
49 4.9287 0.00 0.04 0.00 0.08
50 4.9287 0.00 0.43 0.00 -0.10
51 4.9287 0.00 0.08 0.00 -0.05
52 4.9560 0.00 -0.15 0.00 -0.03
53 4.9561 0.00 -0.30 0.00 0.04
54 4.9561 0.00 -0.09 0.00 0.08
55 4.9561 0.00 0.14 0.00 0.16
56 4.9642 0.00 0.08 0.00 0.09
57 4.9642 0.00 0.03 0.00 0.09
58 4.9642 0.00 -0.00 0.00 0.00
59 4.9643 0.00 0.02 0.00 0.05
60 5.0186 0.00 -0.07 0.00 0.06
61 5.0431 0.00 0.02 0.00 -0.20
62 5.1004 0.00 -0.23 0.00 -0.03
63 5.1005 0.00 -0.07 0.00 -0.18
64 5.1005 0.00 -0.17 0.00 -0.04
65 5.1661 0.00 0.05 0.00 -0.14
66 5.1662 0.00 0.02 0.00 -0.13
67 5.1662 0.00 0.23 0.00 -0.13
68 5.1662 0.00 0.12 0.00 0.03
69 5.2453 0.00 0.02 0.00 0.13
70 5.2453 0.00 -0.05 0.00 -0.13
71 5.2453 0.00 0.08 0.00 0.30
72 5.2454 0.00 0.08 0.00 -0.23
73 5.8704 0.00 0.00 0.00 0.10
74 5.9280 0.00 0.06 0.00 0.14
75 5.9280 0.00 -0.15 0.00 0.12
76 5.9281 0.00 -0.14 0.00 0.07
77 5.9281 0.00 -0.18 0.00 0.05
78 6.1407 0.00 0.04 0.00 -0.20
79 6.1407 0.00 0.12 0.00 -0.03
80 6.1408 0.00 -0.06 0.00 -0.00
81 6.9544 0.00 -0.06 0.00 0.15
82 6.9544 0.00 -0.07 0.00 -0.08
83 6.9545 0.00 -0.04 0.00 -0.08
84 6.9545 0.00 -0.30 0.00 -0.35
85 6.9737 0.00 -0.09 0.00 0.04
86 6.9737 0.00 -0.11 0.00 0.00
87 6.9738 0.00 -0.05 0.00 0.03
88 6.9738 0.00 0.08 0.00 -0.01
89 7.0610 0.00 0.15 0.00 0.10
90 7.0610 0.00 -0.01 0.00 0.09
91 7.0611 0.00 -0.06 0.00 -0.15
92 7.1101 0.00 -0.19 0.00 -0.04
93 7.1347 0.00 0.05 0.00 -0.60
94 8.1832 0.00 -0.09 0.00 0.07
95 8.1833 0.00 -0.07 0.00 -0.04
96 8.1833 0.00 0.01 0.00 0.17
97 8.1857 0.00 -0.01 0.00 0.20
98 8.1858 0.00 -0.21 0.00 -0.11
99 8.1859 0.00 -0.18 0.00 0.12
100 8.1859 0.00 -0.01 0.00 -0.14
101 8.1861 0.00 -0.20 0.00 -0.05
102 8.2682 0.00 0.12 0.00 0.10
103 8.2682 0.00 -0.02 0.00 -0.03
104 8.2682 0.00 0.02 0.00 -0.07
105 11.0691 0.00 0.10 0.00 0.17
106 11.0691 0.00 0.17 0.00 0.07
107 11.0691 0.00 0.02 0.00 -0.10
108 11.9784 0.00 0.19 0.00 0.04
109 11.9784 0.00 0.07 0.00 0.02
110 11.9784 0.00 -0.10 0.00 -0.04
111 11.9785 0.00 -0.03 0.00 0.02
112 13.1908 0.00 -0.14 0.00 0.09
113 13.1908 0.00 0.25 0.00 0.13
114 13.1908 0.00 0.12 0.00 0.04
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.
535022 quality flag:3 Type: SCATNEAR SCATNEAR SCATNEAR axisobj 42.285 42.285 42.285 ecceobj 0.050 0.050 0.050 incobj 7.095 7.095 7.095 qmin 35.344 37.741 35.485 qmax 49.723 47.328 49.706 amean 42.327 42.324 42.326 amin 41.856 41.879 41.844 amax 42.813 42.803 42.831 emean 0.094 0.077 0.113 emin 0.033 0.033 0.033 emax 0.163 0.106 0.161 imean 8.477 8.786 7.182 imin 5.941 7.126 4.468 imax 9.909 10.063 10.042 excite_mean 0.177 0.172 0.173 fracstop 1.000 1.000 1.000 cjmean 3.044 3.046 3.046 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 185.8 184.4 132.3 kozaiamp 180.0 180.0 179.9