Orbit Fit and Astrometric record for 20KR55

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: 20KR55    
# Created Fri Nov 22 02:11:05 2024
# Orbit generated from Bernstein formalism
# Fitting     21 observations of     21
# Arc:  79.98d
# First observation: 2020/05/26
#  Last observation: 2020/08/14
Preliminary a, adot, b, bdot, g, gdot:
   0.000005   0.019723   0.000006   0.008567   0.025145   0.000000
# Chi-squared of fit:     1.66 DOF:     36 RMS:  0.05
# Min/Max residuals:    -0.10    0.08
# Exact a, adot, b, bdot, g, gdot:
  1.549065E-05  2.615083E-02  5.610251E-06  8.541659E-03  2.621875E-02  1.009249E-04
# Covariance matrix:
  2.1370E-13 -1.9735E-11  8.7715E-15  1.8714E-13 -2.8884E-12  8.0547E-11
 -1.9735E-11  7.5349E-08 -6.3661E-11  3.1463E-10  1.4086E-08  2.1190E-07
  8.7715E-15 -6.3661E-11  1.9267E-13 -1.0902E-12 -1.1969E-11 -1.9272E-10
  1.8714E-13  3.1463E-10 -1.0902E-12  1.1587E-11  6.1277E-11  1.3881E-09
 -2.8884E-12  1.4086E-08 -1.1969E-11  6.1277E-11  2.6396E-09  4.0850E-08
  8.0547E-11  2.1190E-07 -1.9272E-10  1.3881E-09  4.0850E-08  8.4889E-07
#      lat0       lon0       xBary       yBary       zBary        JD0
    2.682833  -73.343867    0.671353    0.035124   -0.752306  2458995.943811
# Heliocentric elements and errors
Epoch:              2458990.5000  =  2020/05/21
Mean Anomaly:          352.48384 +/-    19.448
Argument of Peri:       17.47562 +/-    23.405
Long of Asc Node:      277.66840 +/-     0.086
Inclination:            18.26183 +/-     0.180
Eccentricity:         0.09230912 +/-    0.0107
Semi-Major Axis:     42.81843800 +/-    0.6025
Time of Perihelion: 2461127.1730 +/-    5528.6
Perihelion:          38.86590587 +/-    0.7146
Aphelion:            46.77097013 +/-    0.8029
Period (y)              280.1912 +/-      5.91
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           10.49840953 +/-    0.0214
Ecliptic Y          -37.42111793 +/-    0.0715
Ecliptic Z            1.78553995 +/-    0.0035
Ecliptic XDOT         0.00261536 +/-    0.0000
Ecliptic YDOT         0.00081613 +/-    0.0001
Ecliptic ZDOT         0.00089123 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   38.90687372 +/-    0.0690
Geocenter to KBO     38.14064710 +/-    0.0747
# Hcoef: 10.22

The following table shows the complete astrometric record for 20KR55. 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 (20KR55) followed by the observatory code and reference code for the source of the astrometry.

2020 05  26.44301  19 10 50.199  -19 44 17.96  25.9r 20KR55    266  C~6c5c      
2020 05  26.50149  19 10 49.970  -19 44 17.91  25.9r 20KR55    266  C~6c5c      
2020 05  26.55599  19 10 49.756  -19 44 17.85  25.9r 20KR55    266  C~6c5c      
2020 05  29.44698  19 10 38.350  -19 44 15.19  26.1r 20KR55    266  C~6c5c      
2020 05  29.53371  19 10 37.991  -19 44 15.15  26.1r 20KR55    266  C~6c5c      
2020 05  29.61905  19 10 37.637  -19 44 15.09  26.1r 20KR55    266  C~6c5c      
2020 05  31.44139  19 10 30.137  -19 44 14.20  26.2r 20KR55    266  C~6c5c      
2020 05  31.52961  19 10 29.760  -19 44 14.19  26.2r 20KR55    266  C~6c5c      
2020 05  31.61814  19 10 29.381  -19 44 14.16  26.2r 20KR55    266  C~6c5c      
2020 06  21.45390  19 08 50.033  -19 44 40.53  26.1r 20KR55    266  C~6c5c      
2020 06  21.53376  19 08 49.608  -19 44 40.74  26.1r 20KR55    266  C~6c5c      
2020 06  21.61261  19 08 49.189  -19 44 40.93  26.1r 20KR55    266  C~6c5c      
2020 06  24.43648  19 08 34.317  -19 44 48.86  26.2r 20KR55    266  C~6c5c      
2020 06  24.52599  19 08 33.833  -19 44 49.13  26.2r 20KR55    266  C~6c5c      
2020 06  24.61708  19 08 33.342  -19 44 49.37  26.2r 20KR55    266  C~6c5c      
2020 08  12.26680  19 04 22.438  -19 48 18.19  26.0r 20KR55    266  C~6c5c      
2020 08  12.34843  19 04 22.082  -19 48 18.56  26.0r 20KR55    266  C~6c5c      
2020 08  12.42950  19 04 21.730  -19 48 18.90  26.0r 20KR55    266  C~6c5c      
2020 08  14.24286  19 04 14.131  -19 48 26.71  25.9r 20KR55    266  C~6c5c      
2020 08  14.33285  19 04 13.750  -19 48 27.11  25.9r 20KR55    266  C~6c5c      
2020 08  14.42134  19 04 13.376  -19 48 27.48  25.9r 20KR55    266  C~6c5c      

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     0.06       0.00    -0.09
     2   0.0002     -3.20     0.06       0.44    -0.10
     3   0.0003     -6.20     0.07       0.87    -0.10
     4   0.0082   -165.73    -0.03      22.99     0.02
     5   0.0085   -170.76    -0.02      23.64     0.02
     6   0.0087   -175.71    -0.02      24.31     0.02
     7   0.0137   -280.72    -0.06      37.97     0.08
     8   0.0139   -286.00    -0.06      38.63     0.08
     9   0.0142   -291.31    -0.06      39.30     0.08
    10   0.0712  -1687.10     0.07     180.62     0.00
    11   0.0714  -1693.08     0.07     181.12     0.00
    12   0.0716  -1698.98     0.06     181.63    -0.00
    13   0.0794  -1908.43    -0.04     198.53     0.01
    14   0.0796  -1915.24    -0.04     199.07     0.00
    15   0.0799  -1922.16    -0.05     199.64     0.01
    16   0.2131  -5465.55    -0.01     398.60    -0.05
    17   0.2133  -5470.58    -0.01     398.79    -0.05
    18   0.2135  -5475.56     0.00     399.01    -0.05
    19   0.2185  -5583.08     0.01     403.22     0.04
    20   0.2187  -5588.48     0.00     403.42     0.04
    21   0.2190  -5593.77    -0.00     403.64     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.

20KR55    quality flag:1

Type:       SCATEXTD  SCATEXTD  SCATEXTD

axisobj        42.268    45.459    40.119
ecceobj         0.083     0.167     0.088
incobj         18.348    17.768    18.983
qmin           37.213    36.785    36.238
qmax           48.007    55.258    44.479
amean          42.448    45.789    40.287
amin           42.075    45.376    39.960
amax           42.838    46.272    40.617
emean           0.093     0.177     0.081
emin            0.066     0.161     0.067
emax            0.121     0.194     0.096
imean          19.780    19.177    20.703
imin           19.152    18.644    19.994
imax           20.386    19.647    21.413
excite_mean     0.351     0.373     0.363
fracstop        1.000     1.000     1.000
cjmean          2.933     2.950     2.904

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       176.3     169.2     178.4
kozaiamp        179.9     179.9     180.0