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: 19CP32
# Created Fri Jan 24 02:11:36 2025
# Orbit generated from Bernstein formalism
# Fitting 10 observations of 10
# Arc: 59.00d
# First observation: 2019/02/05
# Last observation: 2019/04/05
Preliminary a, adot, b, bdot, g, gdot:
0.000001 0.014465 -0.000001 -0.000630 0.021503 0.000000
# WARNING MRQMIN stopped after 13 iterations -- oscilliatory solution
# WARNING Fitting with energy constraint
# Chi-squared of fit: 3.39 DOF: 15 RMS: 0.10
# Min/Max residuals: -0.19 0.18
# Exact a, adot, b, bdot, g, gdot:
1.348811E-05 1.752998E-02 -1.290832E-06 -7.023784E-04 2.188075E-02 -9.767049E-03
# Covariance matrix:
2.1551E-11 3.0185E-08 -6.4317E-13 -7.3369E-10 5.3612E-09 5.3586E-08
3.0185E-08 4.3012E-05 -9.1638E-10 -1.0454E-06 7.6381E-06 7.6150E-05
-6.4317E-13 -9.1638E-10 3.8386E-13 1.9985E-11 -1.6277E-10 -1.6333E-09
-7.3369E-10 -1.0454E-06 1.9985E-11 2.5431E-08 -1.8565E-07 -1.8548E-06
5.3612E-09 7.6381E-06 -1.6277E-10 -1.8565E-07 1.3572E-06 1.3793E-05
5.3586E-08 7.6150E-05 -1.6333E-09 -1.8548E-06 1.3793E-05 2.2480E-04
# lat0 lon0 xBary yBary zBary JD0
4.318383 -177.502365 0.720478 0.051402 -0.679856 2458520.059171
# Heliocentric elements and errors
Epoch: 2458520.5000 = 2019/02/06
Mean Anomaly: 298.06311 +/- 88.068
Argument of Peri: 238.77225 +/- 34.348
Long of Asc Node: 63.47186 +/- 4.419
Inclination: 4.82235 +/- 0.204
Eccentricity: 0.50181214 +/- 0.6705
Semi-Major Axis: 46.10911933 +/- 23.2088
Time of Perihelion: 2478195.9911 +/- 23706.7
Perihelion: 22.97100367 +/- 33.0085
Aphelion: 69.24723500 +/- 46.5914
Period (y) 313.1039 +/- 236.40
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -46.24071747 +/- 2.4241
Ecliptic Y -1.30399356 +/- 0.1056
Ecliptic Z 3.44124754 +/- 0.1832
Ecliptic XDOT 0.00131450 +/- 0.0019
Ecliptic YDOT -0.00214021 +/- 0.0008
Ecliptic ZDOT -0.00017987 +/- 0.0001
# Distances at JD0 (AU)
Heliocenter to KBO 46.38692203 +/- 2.4165
Geocenter to KBO 45.70227437 +/- 2.4333
# Hcoef: 8.73
The following table shows the complete astrometric record for 19CP32. 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 (19CP32) followed by the observatory code and reference code for the source of the astrometry.
2019 02 05.55837 12 16 02.18 +02 58 09.3 25.0i 19CP32 T09 C~8Sg4 2019 02 05.58709 12 16 02.12 +02 58 09.6 25.0i 19CP32 T09 C~8Sg4 2019 02 05.60072 12 16 02.07 +02 58 09.9 24.8i 19CP32 T09 C~8Sg4 2019 02 05.62764 12 16 02.00 +02 58 10.5 24.8i 19CP32 T09 C~8Sg4 2019 04 04.44950 12 12 24.82 +03 23 05.7 25.9g 19CP32 T09 C~8Sg4 2019 04 04.47203 12 12 24.73 +03 23 06.2 26.0g 19CP32 T09 C~8Sg4 2019 04 04.49512 12 12 24.61 +03 23 06.8 26.4g 19CP32 T09 C~8Sg4 2019 04 04.51398 12 12 24.54 +03 23 07.2 25.3g 19CP32 T09 C~8Sg4 2019 04 05.53497 12 12 20.34 +03 23 32.7 25.1r 19CP32 T09 C~8Sg4 2019 04 05.55592 12 12 20.24 +03 23 33.4 26.0r 19CP32 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 -0.17 0.00 0.16
2 0.0001 -0.94 0.18 -0.08 -0.02
3 0.0001 -1.75 -0.01 -0.11 -0.09
4 0.0002 -2.95 -0.00 0.03 -0.05
5 0.1585 -3582.33 0.04 78.94 0.09
6 0.1586 -3583.76 0.14 78.86 0.06
7 0.1586 -3585.65 -0.19 78.70 -0.06
8 0.1587 -3586.77 -0.03 78.65 -0.07
9 0.1615 -3654.64 0.14 77.08 -0.05
10 0.1615 -3656.29 -0.10 77.12 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.
19CP32 quality flag:0 Type: ERR2LARGE ERR2LARGE ERR2LARGE axisobj 0.000 0.000 0.000 ecceobj -1.000 -1.000 -1.000 incobj -1.000 -1.000 -1.000 qmin 0.000 0.000 0.000 qmax 0.000 0.000 0.000 amean 0.000 0.000 0.000 amin 0.000 0.000 0.000 amax 0.000 0.000 0.000 emean 0.000 0.000 0.000 emin 0.000 0.000 0.000 emax 0.000 0.000 0.000 imean 0.000 0.000 0.000 imin 0.000 0.000 0.000 imax 0.000 0.000 0.000 excite_mean 0.000 0.000 0.000 fracstop 0.000 0.000 0.000 cjmean 0.000 0.000 0.000 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 0.0 0.0 0.0 kozaiamp 0.0 0.0 0.0