Orbit Fit and Astrometric record for 19AP142

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: 19AP142   
# Created Wed Mar 26 01:11:13 2025
# Orbit generated from Bernstein formalism
# Fitting     21 observations of     21
# Arc:   3.92y
# First observation: 2015/04/05
#  Last observation: 2019/03/08
Preliminary a, adot, b, bdot, g, gdot:
   0.002559   0.062959  -0.000238  -0.019216   0.047828   0.000000
# Chi-squared of fit:     8.94 DOF:     36 RMS:  0.12
# Min/Max residuals:    -0.30    0.27
# Exact a, adot, b, bdot, g, gdot:
  1.953370E-05  6.363491E-02 -6.074596E-06 -1.935231E-02  5.082208E-02  1.160823E-02
# Covariance matrix:
  6.9043E-13 -5.0292E-13 -5.4533E-14  1.1075E-13 -2.5550E-13 -1.3718E-12
 -5.0292E-13  7.3711E-13  8.8759E-14 -1.9123E-13  2.3979E-13  2.3486E-12
 -5.4533E-14  8.8759E-14  4.1942E-13 -1.3908E-13  3.9938E-14  3.0355E-13
  1.1075E-13 -1.9123E-13 -1.3908E-13  9.1352E-14 -7.3680E-14 -6.4737E-13
 -2.5550E-13  2.3979E-13  3.9938E-14 -7.3680E-14  3.0629E-13  9.2623E-13
 -1.3718E-12  2.3486E-12  3.0355E-13 -6.4737E-13  9.2623E-13  7.9622E-12
#      lat0       lon0       xBary       yBary       zBary        JD0
   -6.511083  130.450061   -0.899166   -0.048742   -0.428495  2457117.581529
# Heliocentric elements and errors
Epoch:              2457110.5000  =  2015/03/29
Mean Anomaly:          102.53139 +/-     0.012
Argument of Peri:       74.74232 +/-     0.008
Long of Asc Node:      292.83793 +/-     0.000
Inclination:            17.90630 +/-     0.000
Eccentricity:         0.23272218 +/-    0.0000
Semi-Major Axis:     18.34174646 +/-    0.0006
Time of Perihelion: 2448938.7742 +/-       0.9
Perihelion:          14.07321515 +/-    0.0007
Aphelion:            22.61027776 +/-    0.0009
Period (y)               78.5542 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -13.65097121 +/-    0.0001
Ecliptic Y           14.62155546 +/-    0.0002
Ecliptic Z           -2.23135773 +/-    0.0000
Ecliptic XDOT        -0.00293835 +/-    0.0000
Ecliptic YDOT        -0.00184714 +/-    0.0000
Ecliptic ZDOT        -0.00110664 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   20.12753975 +/-    0.0002
Geocenter to KBO     19.67648819 +/-    0.0002
# Hcoef:  9.84

The following table shows the complete astrometric record for 19AP142. 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 (19AP142) followed by the observatory code and reference code for the source of the astrometry.

2015 04  05.080751 08 44 25.277  +11 20 39.95  22.2i 19AP142   W84  C~8iiY      
2015 04  12.009224 08 44 10.406  +11 22 35.47  23.1r 19AP142   W84  C~8iiY      
2016 01  10.256672 09 08 51.125  +08 34 39.32  23.2g 19AP142   W84  C~8iiY      
2016 01  10.257794 09 08 51.110  +08 34 39.25  22.7r 19AP142   W84  C~8iiY      
2017 03  17.087909 09 11 26.930  +07 08 08.92  22.6z 19AP142   W84  C~8iiY      
2018 02  18.239547 09 27 23.539  +04 48 34.42  22.9r 19AP142   W84  C~8eYm      
2018 02  19.231934 09 27 14.290  +04 49 14.48  23.3g 19AP142   W84  C~8eYm      
2018 11  15.56153  09 47 42.02   +02 51 37.2   23.2z 19AP142   T09  C~870S      
2018 11  15.57003  09 47 42.05   +02 51 36.9   23.0z 19AP142   T09  C~870S      
2018 11  15.61124  09 47 42.12   +02 51 34.8   23.0z 19AP142   T09  C~870S      
2018 11  15.62300  09 47 42.14   +02 51 34.2   22.8z 19AP142   T09  C~870S      
2019 01  06.56778  09 45 23.29   +02 31 00.7   23.6g 19AP142   T09  C~870S      
2019 01  06.59117  09 45 23.12   +02 31 00.7   23.7g 19AP142   T09  C~870S      
2019 01  06.60179  09 45 23.06   +02 31 00.7   23.7g 19AP142   T09  C~870S      
2019 01  06.62123  09 45 22.91   +02 31 00.7   23.8g 19AP142   T09  C~870S      
2019 01  06.62334  09 45 22.90   +02 31 00.7   23.7g 19AP142   T09  C~870S      
2019 03  08.26245  09 36 35.50   +03 01 55.7   23.3r 19AP142   T09  C~870S      
2019 03  08.29600  09 36 35.20   +03 01 57.2   23.3r 19AP142   T09  C~870S      
2019 03  08.29809  09 36 35.20   +03 01 57.3   23.3r 19AP142   T09  C~870S      
2019 03  08.31706  09 36 35.05   +03 01 58.0   23.0r 19AP142   T09  C~870S      
2019 03  08.33820  09 36 34.86   +03 01 59.0   23.2r 19AP142   T09  C~870S      

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     0.05       0.00     0.01
     2   0.0190   -241.38    -0.04      53.91     0.03
     3   0.7671  23653.97     0.00   -3698.70     0.06
     4   0.7671  23653.78    -0.05   -3698.83    -0.05
     5   1.9494  27401.17     0.06   -8071.84    -0.07
     6   2.8752  43992.81    -0.02  -12166.18    -0.05
     7   2.8779  43842.13     0.03  -12166.85     0.09
     8   3.6153  64903.32    -0.19  -13756.00    -0.11
     9   3.6153  64903.89    -0.02  -13756.17     0.08
    10   3.6154  64905.69    -0.11  -13757.97     0.03
    11   3.6154  64906.21    -0.13  -13758.48     0.01
    12   3.7577  63142.62     0.06  -15626.34     0.05
    13   3.7577  63139.96     0.02  -15627.10    -0.09
    14   3.7578  63139.02     0.27  -15627.37    -0.08
    15   3.7578  63136.68     0.09  -15628.04    -0.23
    16   3.7578  63136.52     0.17  -15628.08    -0.22
    17   3.9238  54362.53    -0.04  -16100.11     0.21
    18   3.9239  54357.45    -0.30  -16099.93     0.09
    19   3.9239  54357.42    -0.03  -16099.83     0.17
    20   3.9240  54354.90     0.17  -16099.79     0.05
    21   3.9240  54351.66    -0.02  -16099.62     0.03

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.

19AP142    quality flag:3

Type:       CENTAURR  CENTAURR  CENTAURR

axisobj        18.414    18.418    18.410
ecceobj         0.240     0.240     0.240
incobj         17.914    17.915    17.914
qmin           13.699    12.323    13.115
qmax           22.836    24.989    23.898
amean          18.214    18.267    18.504
amin           17.929    17.966    18.101
amax           18.414    18.836    18.733
emean           0.240     0.289     0.260
emin            0.232     0.234     0.238
emax            0.245     0.331     0.283
imean          19.443    18.641    18.825
imin           19.264    17.664    18.388
imax           19.896    19.603    19.507
excite_mean     0.410     0.432     0.415
fracstop        0.002     0.025     0.011
cjmean          3.078     3.061     3.063

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        89.7     168.4     152.6
kozaiamp         17.9     178.9      83.2