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: 19CE32
# Created Mon Jun 30 01:11:10 2025
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 18 observations of 18
# Arc: 7.12y
# First observation: 2018/03/10
# Last observation: 2025/04/23
# Chi-squared of fit: 6.21 DOF: 30 RMS: 0.10
# Min/Max residuals: -0.25 0.26
# Exact a, adot, b, bdot, g, gdot:
1.779637E-05 3.197124E-02 1.862238E-06 3.519519E-03 2.860803E-02 -8.667421E-04
# Covariance matrix:
4.5536E-13 -6.8404E-13 4.5386E-14 -8.3128E-14 4.1025E-13 -3.1590E-12
-6.8404E-13 1.2985E-12 -8.7995E-14 1.6131E-13 -7.7627E-13 6.1292E-12
4.5386E-14 -8.7995E-14 1.2204E-13 -3.6138E-14 5.8251E-14 -4.2319E-13
-8.3128E-14 1.6131E-13 -3.6138E-14 3.8486E-14 -1.0295E-13 7.7426E-13
4.1025E-13 -7.7627E-13 5.8251E-14 -1.0295E-13 1.0251E-12 -3.9385E-12
-3.1590E-12 6.1292E-12 -4.2319E-13 7.7426E-13 -3.9385E-12 2.9429E-11
# lat0 lon0 xBary yBary zBary JD0
2.504384 175.297288 0.105336 0.043248 -0.986477 2458187.977768
# Heliocentric elements and errors
Epoch: 2458188.5000 = 2018/03/11
Mean Anomaly: 350.30377 +/- 0.058
Argument of Peri: 34.71850 +/- 0.082
Long of Asc Node: 154.03076 +/- 0.001
Inclination: 6.73561 +/- 0.000
Eccentricity: 0.15804835 +/- 0.0001
Semi-Major Axis: 42.52937730 +/- 0.0103
Time of Perihelion: 2460917.0515 +/- 39.4
Perihelion: 35.80767931 +/- 0.0106
Aphelion: 49.25107529 +/- 0.0134
Period (y) 277.3587 +/- 0.10
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -35.78117023 +/- 0.0012
Ecliptic Y 3.04194966 +/- 0.0001
Ecliptic Z 1.52747125 +/- 0.0001
Ecliptic XDOT -0.00014728 +/- 0.0000
Ecliptic YDOT -0.00306195 +/- 0.0000
Ecliptic ZDOT 0.00033273 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 35.94273489 +/- 0.0012
Geocenter to KBO 34.95528055 +/- 0.0012
# Hcoef: 7.86
The following table shows the complete astrometric record for 19CE32. 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 (19CE32) followed by the observatory code and reference code for the source of the astrometry.
2018 03 10.476967 11 46 43.09 +04 10 02.7 19CE32 T09 C~8Mhg 2018 03 18.476736 11 46 02.40 +04 14 45.3 19CE32 T09 C~8Mhg 2018 03 18.605414 11 46 01.73 +04 14 49.8 19CE32 T09 C~8Mhg 2018 04 24.412197 11 43 12.01 +04 33 28.1 19CE32 T09 C~8Mhg 2018 04 24.45861 11 43 11.81 +04 33 29.2 22.8z 19CE32 T09 C~8Mhg 2018 04 24.49606 11 43 11.68 +04 33 30.2 23.2z 19CE32 T09 C~8Mhg 2019 02 04.56598 11 56 15.95 +03 18 42.1 24.2g 19CE32 T09 C~8Mhg 2019 02 04.58875 11 56 15.87 +03 18 42.7 24.3g 19CE32 T09 C~8Mhg 2019 02 04.60152 11 56 15.82 +03 18 43.1 24.5g 19CE32 T09 C~8Mhg 2019 02 28.544850 11 54 37.18 +03 31 18.8 19CE32 T09 C~8Mhg 2019 03 02.53504 11 54 27.67 +03 32 28.3 22.8y 19CE32 T09 C~8Mhg 2019 03 02.57800 11 54 27.46 +03 32 29.6 22.6y 19CE32 T09 C~8Mhg 2019 03 02.61357 11 54 27.28 +03 32 30.8 23.1y 19CE32 T09 C~8Mhg 2019 03 02.61624 11 54 27.28 +03 32 31.0 22.8y 19CE32 T09 C~8Mhg 2019 03 10.513873 11 53 48.36 +03 37 09.8 19CE32 T09 C~8Mhg 2019 03 11.491782 11 53 43.44 +03 37 44.4 19CE32 T09 C~8Mhg 2025 04 23.272080 12 32 30.529 +00 41 55.73 23.6G 19CE32 G37 C~8swX 2025 04 23.348080 12 32 30.182 +00 41 58.37 19CE32 G37 C~8swX
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 0.03
2 0.0219 0.00 0.08 0.00 -0.05
3 0.0223 0.00 0.02 0.00 -0.06
4 0.1230 0.00 0.15 0.00 -0.01
5 0.1232 0.00 -0.20 0.00 0.01
6 0.1233 0.00 -0.03 0.00 0.15
7 0.9065 0.00 -0.03 0.00 -0.07
8 0.9065 0.00 -0.05 0.00 -0.09
9 0.9066 0.00 -0.15 0.00 -0.04
10 0.9721 0.00 0.00 0.00 -0.07
11 0.9776 0.00 -0.00 0.00 0.21
12 0.9777 0.00 0.01 0.00 0.01
13 0.9778 0.00 -0.08 0.00 -0.03
14 0.9778 0.00 0.11 0.00 0.08
15 0.9994 0.00 0.11 0.00 0.05
16 1.0021 0.00 0.03 0.00 -0.11
17 7.1206 0.00 -0.02 0.00 -0.25
18 7.1208 0.00 0.03 0.00 0.26
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.
19CE32 quality flag:3 Type: 5:3EE 5:3EE 5:3EE axisobj 42.226 42.226 42.227 ecceobj 0.150 0.150 0.150 incobj 6.753 6.753 6.753 qmin 34.960 34.961 34.960 qmax 49.997 49.988 50.008 amean 42.328 42.328 42.329 amin 41.931 41.931 41.931 amax 42.747 42.745 42.749 emean 0.156 0.156 0.156 emin 0.141 0.141 0.141 emax 0.171 0.171 0.171 imean 5.960 5.960 5.960 imin 5.394 5.394 5.394 imax 6.744 6.744 6.745 excite_mean 0.187 0.187 0.187 fracstop 1.000 1.000 1.000 cjmean 3.041 3.041 3.041 libcent 0 180.1 180.0 180.1 libamp 0 43.0 43.1 42.9 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 183.8 183.8 183.9 kozaiamp 180.0 180.0 179.9