Orbit Fit and Astrometric record for 19ES9

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: 19ES9     
# Created Sun Nov 24 02:10:56 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     27 observations of     27
# Arc:  10.98y
# First observation: 2008/03/14
#  Last observation: 2019/03/08
# Chi-squared of fit:    16.84 DOF:     48 RMS:  0.14
# Min/Max residuals:    -0.40    0.27
# Exact a, adot, b, bdot, g, gdot:
  1.551797E-05  2.603368E-02  6.108179E-06  8.539865E-03  2.585841E-02  1.485942E-03
# Covariance matrix:
  2.9171E-13 -6.3369E-14  4.1959E-15 -1.2040E-14 -4.3773E-14 -1.2856E-13
 -6.3369E-14  1.1796E-13 -1.3293E-14  3.8182E-14  2.0747E-13  4.0762E-13
  4.1959E-15 -1.3293E-14  2.8067E-13 -3.1194E-14 -2.5063E-14 -4.7267E-14
 -1.2040E-14  3.8182E-14 -3.1194E-14  1.5885E-14  7.2275E-14  1.3578E-13
 -4.3773E-14  2.0747E-13 -2.5063E-14  7.2275E-14  9.1949E-13  7.7090E-13
 -1.2856E-13  4.0762E-13 -4.7267E-14  1.3578E-13  7.7090E-13  1.4495E-12
#      lat0       lon0       xBary       yBary       zBary        JD0
   -3.261316  160.369213   -0.228683   -0.055034   -0.966988  2454539.763034
# Heliocentric elements and errors
Epoch:              2454540.5000  =  2008/03/15
Mean Anomaly:           20.86300 +/-     0.023
Argument of Peri:      322.18892 +/-     0.031
Long of Asc Node:      170.29603 +/-     0.000
Inclination:            18.45399 +/-     0.000
Eccentricity:         0.14087095 +/-    0.0001
Semi-Major Axis:     45.48376775 +/-    0.0071
Time of Perihelion: 2448047.3229 +/-       7.3
Perihelion:          39.07642637 +/-    0.0073
Aphelion:            51.89110912 +/-    0.0091
Period (y)              306.7558 +/-      0.07
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -37.35439346 +/-    0.0013
Ecliptic Y           13.07562893 +/-    0.0005
Ecliptic Z           -2.19982530 +/-    0.0001
Ecliptic XDOT        -0.00111595 +/-    0.0000
Ecliptic YDOT        -0.00252605 +/-    0.0000
Ecliptic ZDOT         0.00089366 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   39.63784853 +/-    0.0013
Geocenter to KBO     38.67213593 +/-    0.0014
# Hcoef:  8.34

The following table shows the complete astrometric record for 19ES9. 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 (19ES9) followed by the observatory code and reference code for the source of the astrometry.

2008 03  14.262280 10 42 34.21   +04 39 32.2         19ES9     T14  C~8Mhh      
2008 03  14.270789 10 42 34.17   +04 39 32.9         19ES9     T14  C~8Mhh      
2008 03  14.279216 10 42 34.12   +04 39 33.0         19ES9     T14  C~8Mhh      
2008 03  14.300866 10 42 34.04   +04 39 33.9         19ES9     T14  C~8Mhh      
2008 03  14.309374 10 42 34.00   +04 39 33.9         19ES9     T14  C~8Mhh      
2014 03  05.516731 11 20 32.26   +03 52 42.0         19ES9     T14  C~8Mhh      
2017 03  23.207255 11 37 29.846  +03 39 55.73  24.2V 19ES9     W84  C~8Mhh      
2017 03  24.208417 11 37 25.351  +03 40 29.60  24.3V 19ES9     W84  C~8Mhh      
2018 03  18.463065 11 43 55.51   +03 29 09.7         19ES9     T09  C~8Mhh      
2018 03  18.50571  11 43 55.30   +03 29 11.2   24.5i 19ES9     T09  C~8Mhh      
2018 03  18.57604  11 43 54.95   +03 29 13.7   24.1i 19ES9     T09  C~8Mhh      
2018 03  18.57871  11 43 54.95   +03 29 13.7   23.8i 19ES9     T09  C~8Mhh      
2018 04  24.355370 11 41 23.94   +03 48 03.7         19ES9     T09  C~8Mhh      
2018 04  24.445224 11 41 23.64   +03 48 05.8         19ES9     T09  C~8Mhh      
2019 02  02.656217 11 52 52.38   +02 57 28.8         19ES9     T09  C~8Mhh      
2019 02  04.63313  11 52 46.46   +02 58 21.9   25.3g 19ES9     T09  C~8Mhh      
2019 02  04.66250  11 52 46.38   +02 58 22.7   24.7g 19ES9     T09  C~8Mhh      
2019 02  05.473907 11 52 43.89   +02 58 44.8         19ES9     T09  C~8Mhh      
2019 02  05.511564 11 52 43.76   +02 58 45.9         19ES9     T09  C~8Mhh      
2019 03  02.43427  11 51 09.12   +03 11 48.3   24.4y 19ES9     T09  C~8Mhh      
2019 03  02.53236  11 51 08.70   +03 11 51.6   23.7y 19ES9     T09  C~8Mhh      
2019 03  02.53504  11 51 08.71   +03 11 51.5   24.3y 19ES9     T09  C~8Mhh      
2019 03  02.61357  11 51 08.35   +03 11 54.1   24.2y 19ES9     T09  C~8Mhh      
2019 03  08.35114  11 50 43.17   +03 15 11.3   24.2r 19ES9     T09  C~8Mhh      
2019 03  08.36022  11 50 43.12   +03 15 11.7   24.2r 19ES9     T09  C~8Mhh      
2019 03  08.37278  11 50 43.07   +03 15 12.2   24.2r 19ES9     T09  C~8Mhh      
2019 03  08.40431  11 50 42.93   +03 15 13.4   24.2r 19ES9     T09  C~8Mhh      

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     0.01       0.00    -0.20
     2   0.0000      0.00    -0.01       0.00     0.21
     3   0.0000      0.00    -0.18       0.00     0.02
     4   0.0001      0.00     0.11       0.00     0.19
     5   0.0001      0.00     0.10       0.00    -0.10
     6   5.9747      0.00    -0.08       0.00    -0.29
     7   9.0238      0.00    -0.08       0.00     0.06
     8   9.0265      0.00     0.03       0.00     0.03
     9  10.0101      0.00     0.27       0.00    -0.03
    10  10.0102      0.00     0.09       0.00     0.00
    11  10.0104      0.00    -0.29       0.00     0.08
    12  10.0104      0.00    -0.10       0.00    -0.01
    13  10.1111      0.00     0.07       0.00    -0.04
    14  10.1114      0.00     0.13       0.00    -0.16
    15  10.8895      0.00     0.12       0.00     0.00
    16  10.8949      0.00     0.00       0.00     0.04
    17  10.8950      0.00     0.18       0.00     0.04
    18  10.8972      0.00     0.20       0.00    -0.10
    19  10.8973      0.00     0.05       0.00    -0.04
    20  10.9656      0.00    -0.40       0.00     0.27
    21  10.9658      0.00    -0.21       0.00     0.22
    22  10.9658      0.00     0.11       0.00     0.03
    23  10.9661      0.00    -0.11       0.00    -0.04
    24  10.9818      0.00     0.02       0.00    -0.17
    25  10.9818      0.00    -0.12       0.00    -0.08
    26  10.9818      0.00    -0.01       0.00    -0.02
    27  10.9819      0.00     0.03       0.00     0.09

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.