Orbit Fit and Astrometric record for 20KS54

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: 20KS54    
# Created Sun Dec 22 02:11:12 2024
# Orbit generated from Bernstein formalism
# Fitting     21 observations of     21
# Arc:  78.97d
# First observation: 2020/05/28
#  Last observation: 2020/08/15
Preliminary a, adot, b, bdot, g, gdot:
   0.000005   0.017595   0.000003  -0.007850   0.023990   0.000000
# Chi-squared of fit:     0.31 DOF:     36 RMS:  0.02
# Min/Max residuals:    -0.04    0.05
# Exact a, adot, b, bdot, g, gdot:
  1.490803E-05  2.346784E-02 -5.097538E-06 -7.845269E-03  2.496701E-02 -1.990743E-03
# Covariance matrix:
  1.9851E-13  1.5185E-11 -4.4359E-15 -3.4046E-13  3.6271E-12  1.8462E-10
  1.5185E-11  1.8888E-07 -9.1816E-11 -1.4155E-09  3.5659E-08  6.2362E-07
 -4.4359E-15 -9.1816E-11  1.7129E-13 -2.3241E-13 -1.7307E-11 -2.9686E-10
 -3.4046E-13 -1.4155E-09 -2.3241E-13  2.5838E-11 -2.6908E-10 -5.0829E-09
  3.6271E-12  3.5659E-08 -1.7307E-11 -2.6908E-10  6.7376E-09  1.1884E-07
  1.8462E-10  6.2362E-07 -2.9686E-10 -5.0829E-09  1.1884E-07  2.3038E-06
#      lat0       lon0       xBary       yBary       zBary        JD0
    2.145281  -71.936263    0.664504    0.028296   -0.758775  2458997.947541
# Heliocentric elements and errors
Epoch:              2458990.5000  =  2020/05/21
Mean Anomaly:          292.21662 +/-    13.223
Argument of Peri:      252.13477 +/-    21.317
Long of Asc Node:      113.42535 +/-     0.117
Inclination:            18.54039 +/-     0.328
Eccentricity:         0.09954207 +/-    0.0555
Semi-Major Axis:     42.03339255 +/-    0.5151
Time of Perihelion: 2477732.2802 +/-    3639.9
Perihelion:          37.84930182 +/-    2.3766
Aphelion:            46.21748328 +/-    2.3988
Period (y)              272.5209 +/-      5.01
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           12.01995401 +/-    0.0408
Ecliptic Y          -38.98683115 +/-    0.1251
Ecliptic Z            1.49918416 +/-    0.0049
Ecliptic XDOT         0.00239707 +/-    0.0001
Ecliptic YDOT         0.00097828 +/-    0.0001
Ecliptic ZDOT        -0.00086810 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   40.82523546 +/-    0.1201
Geocenter to KBO     40.05285635 +/-    0.1317
# Hcoef:  9.97

The following table shows the complete astrometric record for 20KS54. 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 (20KS54) followed by the observatory code and reference code for the source of the astrometry.

2020 05  28.44674  19 17 03.646  -20 05 38.54  26.6r 20KS54    266  C~6c5a      
2020 05  28.50129  19 17 03.441  -20 05 39.05  26.6r 20KS54    266  C~6c5a      
2020 05  28.55756  19 17 03.230  -20 05 39.57  26.6r 20KS54    266  C~6c5a      
2020 05  30.43935  19 16 56.214  -20 05 57.09  26.2r 20KS54    266  C~6c5a      
2020 05  30.53044  19 16 55.860  -20 05 57.96  26.2r 20KS54    266  C~6c5a      
2020 05  30.61862  19 16 55.516  -20 05 58.79  26.2r 20KS54    266  C~6c5a      
2020 06  01.43269  19 16 48.507  -20 06 16.28  26.1r 20KS54    266  C~6c5a      
2020 06  01.47325  19 16 48.345  -20 06 16.69  26.1r 20KS54    266  C~6c5a      
2020 06  01.60571  19 16 47.811  -20 06 17.99  26.1r 20KS54    266  C~6c5a      
2020 06  20.45583  19 15 23.864  -20 09 48.31  25.9r 20KS54    266  C~6c5a      
2020 06  20.52860  19 15 23.502  -20 09 49.21  25.9r 20KS54    266  C~6c5a      
2020 06  20.62233  19 15 23.037  -20 09 50.35  25.9r 20KS54    266  C~6c5a      
2020 06  22.44948  19 15 14.068  -20 10 13.12  26.2r 20KS54    266  C~6c5a      
2020 06  22.52092  19 15 13.709  -20 10 14.02  26.2r 20KS54    266  C~6c5a      
2020 06  22.59118  19 15 13.355  -20 10 14.89  26.2r 20KS54    266  C~6c5a      
2020 06  25.44823  19 14 59.122  -20 10 51.22  25.8r 20KS54    266  C~6c5a      
2020 06  25.53213  19 14 58.692  -20 10 52.29  25.8r 20KS54    266  C~6c5a      
2020 06  25.61487  19 14 58.270  -20 10 53.33  25.8r 20KS54    266  C~6c5a      
2020 08  15.24331  19 10 51.254  -20 22 27.59  25.3r 20KS54    266  C~6c5a      
2020 08  15.34125  19 10 50.856  -20 22 28.89  25.3r 20KS54    266  C~6c5a      
2020 08  15.42111  19 10 50.533  -20 22 29.93  25.3r 20KS54    266  C~6c5a      

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     0.03
     2   0.0001     -2.93    -0.02      -0.13     0.03
     3   0.0003     -5.94    -0.01      -0.25     0.02
     4   0.0055   -106.22     0.03      -4.65    -0.01
     5   0.0057   -111.28     0.03      -4.86    -0.00
     6   0.0059   -116.19     0.03      -5.05    -0.00
     7   0.0109   -216.36    -0.02      -9.45    -0.01
     8   0.0110   -218.68    -0.02      -9.55    -0.02
     9   0.0114   -226.31    -0.03      -9.86    -0.02
    10   0.0630  -1425.89     0.05     -64.82    -0.01
    11   0.0632  -1431.06     0.04     -65.06    -0.01
    12   0.0635  -1437.70     0.04     -65.34    -0.01
    13   0.0685  -1565.87    -0.04     -71.67     0.01
    14   0.0686  -1571.00    -0.03     -71.91     0.01
    15   0.0688  -1576.05    -0.04     -72.13     0.01
    16   0.0767  -1779.47     0.01     -82.43    -0.01
    17   0.0769  -1785.61    -0.00     -82.71    -0.01
    18   0.0771  -1791.64     0.00     -82.98    -0.01
    19   0.2157  -5327.93     0.00    -336.93     0.00
    20   0.2160  -5333.65    -0.00    -337.53     0.00
    21   0.2162  -5338.29     0.00    -338.01     0.00

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.

20KS54    quality flag:1

Type:       SCATEXTD  SCATEXTD  CENTAURR

axisobj        41.550    45.728    39.809
ecceobj         0.101     0.136     0.199
incobj         18.606    17.582    19.537
qmin           37.057    38.912    29.791
qmax           46.692    53.422    61.856
amean          41.732    46.009    41.382
amin           41.401    45.623    39.460
amax           42.086    46.438    46.316
emean           0.094     0.139     0.241
emin            0.080     0.128     0.168
emax            0.110     0.151     0.338
imean          17.014    15.946    15.384
imin           16.333    15.569    11.925
imax           17.723    16.341    18.326
excite_mean     0.307     0.308     0.363
fracstop        1.000     1.000     0.324
cjmean          2.963     3.008     2.920

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       184.3     192.0     176.4
kozaiamp        180.0     179.9     179.9