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: 19CN32
# Created Wed Dec 25 02:11:00 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 16 observations of 16
# Arc: 15.21y
# First observation: 2003/12/23
# Last observation: 2019/03/10
# Chi-squared of fit: 3.62 DOF: 26 RMS: 0.08
# Min/Max residuals: -0.18 0.15
# Exact a, adot, b, bdot, g, gdot:
1.738738E-05 2.959907E-02 1.366959E-06 2.650449E-03 2.720777E-02 4.278995E-03
# Covariance matrix:
4.8955E-13 -6.5130E-14 1.2721E-16 -2.9088E-15 -2.8650E-14 -7.3540E-14
-6.5130E-14 1.6689E-12 -5.9419E-15 1.4331E-13 2.4412E-12 3.6614E-12
1.2721E-16 -5.9419E-15 4.8823E-13 -3.3141E-14 -8.4029E-15 -1.3091E-14
-2.9088E-15 1.4331E-13 -3.3141E-14 1.4999E-14 2.0694E-13 3.1525E-13
-2.8650E-14 2.4412E-12 -8.4029E-15 2.0694E-13 4.0848E-12 5.3077E-12
-7.3540E-14 3.6614E-12 -1.3091E-14 3.1525E-13 5.3077E-12 8.0519E-12
# lat0 lon0 xBary yBary zBary JD0
0.511438 152.582945 0.862839 0.004230 -0.466217 2452996.980153
# Heliocentric elements and errors
Epoch: 2452996.5000 = 2003/12/23
Mean Anomaly: 30.65546 +/- 0.030
Argument of Peri: 320.83330 +/- 0.047
Long of Asc Node: 145.61976 +/- 0.001
Inclination: 5.12865 +/- 0.000
Eccentricity: 0.19435492 +/- 0.0001
Semi-Major Axis: 44.03084322 +/- 0.0105
Time of Perihelion: 2443909.1090 +/- 9.4
Perihelion: 35.47323242 +/- 0.0092
Aphelion: 52.58845401 +/- 0.0131
Period (y) 292.1754 +/- 0.10
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -32.64485290 +/- 0.0024
Ecliptic Y 17.90625021 +/- 0.0013
Ecliptic Z 0.32811435 +/- 0.0000
Ecliptic XDOT -0.00175583 +/- 0.0000
Ecliptic YDOT -0.00245309 +/- 0.0000
Ecliptic ZDOT 0.00027069 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 37.23469045 +/- 0.0022
Geocenter to KBO 36.75412933 +/- 0.0027
# Hcoef: 8.94
The following table shows the complete astrometric record for 19CN32. 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 (19CN32) followed by the observatory code and reference code for the source of the astrometry.
2003 12 23.47941 10 18 56.70 +11 01 52.5 19CN32 T14 C~8Sg4 2003 12 23.53110 10 18 56.60 +11 01 53.1 19CN32 T14 C~8Sg4 2003 12 23.58193 10 18 56.50 +11 01 53.8 19CN32 T14 C~8Sg4 2018 03 18.586708 11 41 15.79 +04 45 11.8 19CN32 T09 C~8Sg4 2018 03 18.602744 11 41 15.73 +04 45 12.3 19CN32 T09 C~8Sg4 2018 04 24.455925 11 38 39.20 +05 01 53.2 19CN32 T09 C~8Sg4 2019 02 04.59733 11 50 04.63 +03 54 00.0 26.0g 19CN32 T09 C~8Sg4 2019 02 04.59943 11 50 04.61 +03 54 00.2 25.8g 19CN32 T09 C~8Sg4 2019 02 04.64154 11 50 04.48 +03 54 01.0 25.6g 19CN32 T09 C~8Sg4 2019 02 05.47125 11 50 01.77 +03 54 22.2 24.2i 19CN32 T09 C~8Sg4 2019 02 05.48460 11 50 01.74 +03 54 22.6 24.2i 19CN32 T09 C~8Sg4 2019 02 05.52237 11 50 01.59 +03 54 23.6 24.4i 19CN32 T09 C~8Sg4 2019 03 08.370670 11 47 55.12 +04 09 41.8 19CN32 T09 C~8Sg4 2019 03 08.412689 11 47 54.92 +04 09 43.2 19CN32 T09 C~8Sg4 2019 03 10.494607 11 47 45.22 +04 10 50.1 19CN32 T09 C~8Sg4 2019 03 10.511780 11 47 45.14 +04 10 50.4 19CN32 T09 C~8Sg4
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 -0.02 0.00 0.05
2 0.0001 0.00 -0.01 0.00 -0.04
3 0.0003 0.00 0.00 0.00 -0.01
4 14.2344 0.00 -0.14 0.00 0.03
5 14.2344 0.00 0.11 0.00 0.03
6 14.3353 0.00 0.07 0.00 0.12
7 15.1187 0.00 0.09 0.00 -0.02
8 15.1187 0.00 -0.10 0.00 0.13
9 15.1189 0.00 0.05 0.00 -0.14
10 15.1211 0.00 -0.07 0.00 -0.09
11 15.1212 0.00 0.15 0.00 -0.03
12 15.1213 0.00 -0.18 0.00 -0.00
13 15.2057 0.00 0.01 0.00 -0.01
14 15.2058 0.00 -0.02 0.00 0.04
15 15.2115 0.00 -0.02 0.00 0.11
16 15.2116 0.00 0.01 0.00 -0.14
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.
19CN32 quality flag:3 Type: 7:4EEE 7:4EEE 7:4EEE axisobj 43.633 43.633 43.633 ecceobj 0.190 0.190 0.190 incobj 5.146 5.146 5.146 qmin 34.424 34.422 34.425 qmax 53.626 53.610 53.640 amean 43.727 43.727 43.727 amin 43.278 43.265 43.255 amax 44.261 44.255 44.267 emean 0.196 0.196 0.196 emin 0.178 0.178 0.178 emax 0.212 0.211 0.212 imean 2.478 2.500 2.454 imin 1.153 1.162 1.144 imax 4.034 4.109 4.020 excite_mean 0.201 0.201 0.201 fracstop 1.000 1.000 1.000 cjmean 3.049 3.049 3.049 libcent 0 181.0 180.4 180.4 libamp 0 88.2 89.7 88.7 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 267.6 267.6 267.8 kozaiamp 70.5 69.8 71.0