Orbit Fit and Astrometric record for 19AQ142

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: 19AQ142   
# Created Sat Feb 22 02:11:11 2025
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     20 observations of     20
# Arc:  10.00y
# First observation: 2014/12/30
#  Last observation: 2024/12/31
# Chi-squared of fit:     7.36 DOF:     34 RMS:  0.11
# Min/Max residuals:    -0.28    0.25
# Exact a, adot, b, bdot, g, gdot:
  1.567833E-05  3.145646E-02 -4.628451E-06 -6.568343E-03  3.010552E-02 -2.473056E-03
# Covariance matrix:
  3.7066E-13 -1.2637E-13 -3.4521E-14  1.9788E-14  1.4938E-14 -2.6617E-13
 -1.2637E-13  6.6483E-14  2.0851E-14 -1.2440E-14  3.8450E-14  1.6738E-13
 -3.4521E-14  2.0851E-14  2.1008E-13 -3.6197E-14  8.8076E-15  5.9139E-14
  1.9788E-14 -1.2440E-14 -3.6197E-14  1.0282E-14 -9.1275E-15 -3.5429E-14
  1.4938E-14  3.8450E-14  8.8076E-15 -9.1275E-15  3.9254E-13  1.2311E-13
 -2.6617E-13  1.6738E-13  5.9139E-14 -3.5429E-14  1.2311E-13  4.7669E-13
#      lat0       lon0       xBary       yBary       zBary        JD0
   -9.657920  139.760788    0.650535   -0.123283   -0.725368  2457021.938845
# Heliocentric elements and errors
Epoch:              2457022.5000  =  2014/12/31
Mean Anomaly:          269.56556 +/-     0.046
Argument of Peri:      320.20497 +/-     0.035
Long of Asc Node:      280.86289 +/-     0.000
Inclination:            15.19309 +/-     0.000
Eccentricity:         0.09657668 +/-    0.0000
Semi-Major Axis:     33.61493458 +/-    0.0027
Time of Perihelion: 2474904.9974 +/-      11.1
Perihelion:          30.36851571 +/-    0.0025
Aphelion:            36.86135344 +/-    0.0030
Period (y)              194.8977 +/-      0.02
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -25.14115098 +/-    0.0005
Ecliptic Y           22.12541890 +/-    0.0004
Ecliptic Z           -5.57274926 +/-    0.0001
Ecliptic XDOT        -0.00160620 +/-    0.0000
Ecliptic YDOT        -0.00239692 +/-    0.0000
Ecliptic ZDOT        -0.00055104 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   33.95100631 +/-    0.0005
Geocenter to KBO     33.21657107 +/-    0.0007
# Hcoef:  8.45

The following table shows the complete astrometric record for 19AQ142. 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 (19AQ142) followed by the observatory code and reference code for the source of the astrometry.

2014 12  30.438067 09 16 32.96   +05 42 15.1         19AQ142   695  C~8eYm      
2014 12  30.445324 09 16 32.91   +05 42 15.2         19AQ142   695  C~8eYm      
2014 12  30.463703 09 16 32.82   +05 42 15.0         19AQ142   695  C~8eYm      
2016 02  03.469552 09 19 56.82   +04 55 13.3         19AQ142   T09  C~8eYm      
2016 02  03.491898 09 19 56.69   +04 55 14.0         19AQ142   T09  C~8eYm      
2018 11  15.56728  09 43 36.74   +02 11 30.2   23.7z 19AQ142   T09  C~870S      
2018 11  15.57003  09 43 36.75   +02 11 30.0   23.6z 19AQ142   T09  C~870S      
2018 11  15.59379  09 43 36.76   +02 11 29.4   23.4z 19AQ142   T09  C~870S      
2018 11  15.61124  09 43 36.78   +02 11 28.8   23.8z 19AQ142   T09  C~870S      
2018 11  15.61997  09 43 36.78   +02 11 28.3   23.8z 19AQ142   T09  C~870S      
2019 01  06.56568  09 42 00.10   +02 00 02.2   24.0g 19AQ142   T09  C~870S      
2019 01  06.58908  09 41 59.99   +02 00 02.2   24.1g 19AQ142   T09  C~870S      
2019 01  06.60853  09 41 59.90   +02 00 02.3   24.0g 19AQ142   T09  C~870S      
2019 01  06.62123  09 41 59.84   +02 00 02.5   24.3g 19AQ142   T09  C~870S      
2019 03  08.28552  09 36 26.06   +02 21 41.8   24.0r 19AQ142   T09  C~870S      
2019 03  08.32553  09 36 25.86   +02 21 43.0   23.7r 19AQ142   T09  C~870S      
2019 03  08.32762  09 36 25.83   +02 21 43.2   23.6r 19AQ142   T09  C~870S      
2024 12  31.427570 10 22 10.850  -03 44 51.76  23.4G 19AQ142   G37  C~8eYm      
2024 12  31.480270 10 22 10.689  -03 44 52.10        19AQ142   G37  C~8eYm      
2024 12  31.532250 10 22 10.522  -03 44 52.69        19AQ142   G37  C~8eYm      

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     0.24       0.00     0.18
     2   0.0000      0.00    -0.02       0.00     0.25
     3   0.0001      0.00    -0.13       0.00    -0.04
     4   1.0952      0.00    -0.01       0.00    -0.19
     5   1.0953      0.00     0.05       0.00     0.02
     6   3.8772      0.00     0.01       0.00     0.03
     7   3.8772      0.00     0.12       0.00    -0.09
     8   3.8772      0.00    -0.07       0.00     0.03
     9   3.8773      0.00    -0.02       0.00    -0.04
    10   3.8773      0.00    -0.14       0.00    -0.28
    11   4.0195      0.00     0.06       0.00     0.05
    12   4.0196      0.00    -0.00       0.00    -0.06
    13   4.0196      0.00    -0.03       0.00    -0.06
    14   4.0197      0.00    -0.07       0.00     0.08
    15   4.1858      0.00    -0.06       0.00     0.00
    16   4.1859      0.00     0.14       0.00    -0.06
    17   4.1859      0.00    -0.15       0.00     0.07
    18  10.0041      0.00     0.04       0.00     0.06
    19  10.0042      0.00     0.07       0.00     0.14
    20  10.0044      0.00    -0.02       0.00    -0.05

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.

19AQ142    quality flag:3

Type:       CENTAURR  CENTAURR  CENTAURR

axisobj        33.485    33.485    33.485
ecceobj         0.094     0.094     0.094
incobj         15.195    15.195    15.195
qmin           27.283    28.069    28.088
qmax           39.675    38.994    38.956
amean          33.366    33.370    33.364
amin           32.286    33.009    32.141
amax           33.748    33.738    33.755
emean           0.133     0.123     0.120
emin            0.067     0.081     0.080
emax            0.181     0.157     0.157
imean          16.002    16.714    16.805
imin           14.099    15.243    14.577
imax           18.032    17.508    17.768
excite_mean     0.307     0.313     0.314
fracstop        0.704     0.303     0.296
cjmean          2.909     2.906     2.906

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       231.3     254.3     251.9
kozaiamp        179.9     179.9      80.0