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: 523983
# Created Fri Nov 22 02:07:23 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 36 observations of 36
# Arc: 21.12y
# First observation: 1999/09/06
# Last observation: 2020/10/20
# Chi-squared of fit: 102.31 DOF: 66 RMS: 0.30
# Min/Max residuals: -0.75 0.63
# Exact a, adot, b, bdot, g, gdot:
1.693501E-05 2.940064E-02 5.026392E-06 5.254137E-03 2.711723E-02 -1.831021E-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
9.362985 9.349903 0.441548 0.145973 -0.886720 2451427.939683
# Heliocentric elements and errors
Epoch: 2451428.5000 = 1999/09/07
Mean Anomaly: 341.21027 +/- 0.000
Argument of Peri: 69.79632 +/- 0.000
Long of Asc Node: 327.27633 +/- 0.000
Inclination: 13.67301 +/- 0.000
Eccentricity: 0.18682567 +/- 0.0000
Semi-Major Axis: 45.62184192 +/- 0.0000
Time of Perihelion: 2457303.0647 +/- 0.0
Perihelion: 37.09851089 +/- 0.0000
Aphelion: 54.14517295 +/- 0.0000
Period (y) 308.1537 +/- 0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X 36.86824563 +/- 0.0000
Ecliptic Y 5.62412754 +/- 0.0000
Ecliptic Z 5.99965198 +/- 0.0000
Ecliptic XDOT -0.00075146 +/- 0.0000
Ecliptic YDOT 0.00289363 +/- 0.0000
Ecliptic ZDOT 0.00049340 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 37.77430034 +/- 0.0000
Geocenter to KBO 36.87699637 +/- 0.0000
# Hcoef: 7.36
The following table shows the complete astrometric record for 523983. 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 (523983) followed by the observatory code and reference code for the source of the astrometry.
1999 09 06.43894 00 19 20.48 +12 17 59.3 22.8R 523983 568 Ca8546 1999 09 06.48649 00 19 20.26 +12 17 58.6 22.8R 523983 568 Ca8546 1999 09 06.52690 00 19 20.06 +12 17 57.8 22.8R 523983 568 Ca8546 1999 09 09.47537 00 19 06.24 +12 16 58.6 22.8R 523983 568 Ca8546 1999 09 09.48697 00 19 06.21 +12 16 58.6 22.8R 523983 568 Ca8546 1999 09 10.47595 00 19 01.51 +12 16 37.7 22.9R 523983 568 Ca8546 1999 09 10.48639 00 19 01.46 +12 16 37.3 22.6R 523983 568 Ca8546 1999 10 08.40856 00 16 42.11 +12 04 09.5 23.2R 523983 568 Ca8546 1999 10 08.43404 00 16 42.00 +12 04 08.8 23.0R 523983 568 Ca8546 1999 11 10.31627 00 14 19.64 +11 46 56.2 23.1R 523983 568 Ca8546 1999 11 10.36475 00 14 19.45 +11 46 54.2 23.1R 523983 568 Ca8546 2000 08 27.55819 00 25 52.53 +13 17 31.9 22.9R 523983 568 Cb9109 2000 08 27.59454 00 25 52.37 +13 17 31.1 23.0R 523983 568 Cb9109 2000 08 29.60300 00 25 43.98 +13 17 03.9 22.7R 523983 568 Cb9109 2000 08 29.63530 00 25 43.83 +13 17 03.5 22.9R 523983 568 Cb9109 2000 12 27.22020 00 19 02.621 +12 27 43.75 22.0R 523983 568 Cl2529 2000 12 28.22887 00 19 03.690 +12 27 36.46 22.1R 523983 568 Cl2529 2002 11 05.32464 00 32 15.67 +14 40 40.9 22.5R 523983 568 Cl8251 2002 11 05.36123 00 32 15.51 +14 40 40.1 523983 568 Cl8251 2002 11 06.39525 00 32 11.33 +14 40 06.5 523983 568 Cl8251 2007 07 12.35358 01 09 50.29 +19 33 25.0 523983 304 Cv1964 2007 07 12.43263 01 09 50.35 +19 33 27.3 523983 304 Cv1964 2008 09 20.37879 01 13 30.88 +20 32 18.4 23.6R 523983 250 S~06AL 2008 09 20.38574 01 13 30.84 +20 32 18.2 523983 250 S~06AL 2008 09 20.39199 01 13 30.81 +20 32 18.1 523983 250 S~06AL 2008 09 20.39893 01 13 30.78 +20 32 18.0 523983 250 S~06AL 2015 10 11.235689 01 59 37.45 +26 13 50.4 523983 W84 C~3n9Q 2015 10 11.237390 01 59 37.43 +26 13 50.3 523983 W84 C~3n9Q 2018 09 13.324640 02 23 33.14 +28 27 16.4 22.8G 523983 705 C~2rXd 2018 09 14.333860 02 23 29.55 +28 27 19.7 23.0G 523983 705 C~2rXd 2018 09 14.447070 02 23 29.13 +28 27 20.1 22.8G 523983 705 C~2rXd 2019 11 27.133010 02 24 26.683 +28 46 31.46 22.7G 523983 G37 C~3TtO 2019 11 27.207700 02 24 26.289 +28 46 29.47 523983 G37 C~3TtO 2020 10 20.307710 02 35 32.061 +29 42 04.64 22.9G 523983 G37 C~4Kn8 2020 10 20.363980 02 35 31.741 +29 42 03.50 523983 G37 C~4Kn8 2020 10 20.443100 02 35 31.271 +29 42 02.25 523983 G37 C~4Kn8
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 0.21 0.00 -0.35
2 0.0001 0.00 0.27 0.00 -0.14
3 0.0002 0.00 0.13 0.00 -0.16
4 0.0083 0.00 -0.10 0.00 -0.16
5 0.0083 0.00 0.30 0.00 0.08
6 0.0111 0.00 0.32 0.00 0.02
7 0.0111 0.00 0.33 0.00 -0.15
8 0.0875 0.00 0.32 0.00 -0.31
9 0.0876 0.00 0.61 0.00 -0.22
10 0.1776 0.00 -0.26 0.00 0.63
11 0.1778 0.00 -0.59 0.00 0.07
12 0.9750 0.00 -0.10 0.00 -0.13
13 0.9751 0.00 -0.20 0.00 -0.45
14 0.9806 0.00 0.14 0.00 -0.26
15 0.9807 0.00 -0.02 0.00 -0.19
16 1.3081 0.00 -0.69 0.00 0.51
17 1.3109 0.00 -0.75 0.00 0.60
18 3.1646 0.00 0.16 0.00 -0.46
19 3.1647 0.00 0.06 0.00 -0.07
20 3.1676 0.00 0.43 0.00 -0.14
21 7.8464 0.00 -0.28 0.00 0.23
22 7.8467 0.00 -0.41 0.00 0.32
23 9.0402 0.00 -0.07 0.00 0.54
24 9.0402 0.00 -0.16 0.00 0.46
25 9.0403 0.00 -0.15 0.00 0.46
26 9.0403 0.00 -0.09 0.00 0.48
27 16.0953 0.00 0.07 0.00 0.13
28 16.0953 0.00 -0.09 0.00 0.06
29 19.0195 0.00 -0.00 0.00 -0.22
30 19.0223 0.00 0.02 0.00 -0.13
31 19.0226 0.00 0.00 0.00 -0.05
32 20.2237 0.00 0.12 0.00 -0.29
33 20.2239 0.00 0.11 0.00 0.10
34 21.1222 0.00 0.01 0.00 -0.03
35 21.1223 0.00 0.14 0.00 -0.23
36 21.1225 0.00 0.02 0.00 -0.13
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.
523983 quality flag:3 Type: SCATEXTD SCATEXTD SCATEXTD axisobj 45.599 45.599 45.599 ecceobj 0.187 0.187 0.187 incobj 13.678 13.678 13.678 qmin 36.362 36.402 36.386 qmax 54.423 54.467 54.398 amean 45.198 45.200 45.199 amin 44.811 44.813 44.811 amax 45.656 45.642 45.666 emean 0.176 0.176 0.176 emin 0.161 0.160 0.161 emax 0.193 0.194 0.193 imean 14.853 14.854 14.855 imin 14.239 14.257 14.253 imax 15.556 15.553 15.560 excite_mean 0.311 0.311 0.311 fracstop 1.000 1.000 1.000 cjmean 2.997 2.997 2.997 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 181.1 180.8 180.9 kozaiamp 180.0 179.9 180.0