Orbit Fit and Astrometric record for 20KP11

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: 20KP11    
# Created Sun Dec 22 02:11:11 2024
# Orbit generated from Bernstein formalism
# Fitting     65 observations of     65
# Arc:   3.29y
# First observation: 2020/05/26
#  Last observation: 2023/09/10
Preliminary a, adot, b, bdot, g, gdot:
  -0.000033   0.014723  -0.000000  -0.006000   0.019487   0.000000
# Chi-squared of fit:     5.26 DOF:    124 RMS:  0.05
# Min/Max residuals:    -0.16    0.15
# Exact a, adot, b, bdot, g, gdot:
  1.225487E-05  1.486790E-02 -4.956182E-06 -6.063229E-03  1.975646E-02  1.774218E-03
# Covariance matrix:
  6.7540E-14 -1.6565E-14 -6.4575E-16  2.7716E-15  3.3757E-14 -1.5172E-13
 -1.6565E-14  1.0318E-13  2.3486E-14 -6.9073E-14  6.8352E-14  3.7501E-12
 -6.4575E-16  2.3486E-14  5.4438E-14 -4.3540E-14  1.6056E-14  1.1279E-12
  2.7716E-15 -6.9073E-14 -4.3540E-14  8.2633E-14 -4.5954E-14 -3.3364E-12
  3.3757E-14  6.8352E-14  1.6056E-14 -4.5954E-14  9.8547E-14  2.4931E-12
 -1.5172E-13  3.7501E-12  1.1279E-12 -3.3364E-12  2.4931E-12  1.8117E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
    1.902829  -73.592993    0.667956    0.024980   -0.755727  2458995.952801
# Heliocentric elements and errors
Epoch:              2458990.5000  =  2020/05/21
Mean Anomaly:          136.45080 +/-     0.236
Argument of Peri:       27.78935 +/-     0.229
Long of Asc Node:      110.28200 +/-     0.000
Inclination:            22.12505 +/-     0.001
Eccentricity:         0.15669123 +/-    0.0004
Semi-Major Axis:     45.73745180 +/-    0.0068
Time of Perihelion: 2416167.2175 +/-      73.4
Perihelion:          38.57079400 +/-    0.0177
Aphelion:            52.90410959 +/-    0.0185
Period (y)              309.3258 +/-      0.07
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           13.86757105 +/-    0.0002
Ecliptic Y          -49.44934247 +/-    0.0008
Ecliptic Z            1.68051189 +/-    0.0000
Ecliptic XDOT         0.00206191 +/-    0.0000
Ecliptic YDOT         0.00032299 +/-    0.0000
Ecliptic ZDOT        -0.00083185 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   51.38454162 +/-    0.0007
Geocenter to KBO     50.61634777 +/-    0.0008
# Hcoef:  7.97

The following table shows the complete astrometric record for 20KP11. 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 (20KP11) followed by the observatory code and reference code for the source of the astrometry.

2020 05  26.452    19 10 11.068  -20 32 33.53  25.8R 20KP11    266  C~4Al3      
2020 05  26.510    19 10 10.887  -20 32 33.95  25.8R 20KP11    266  C~4Al3      
2020 05  29.44698  19 10 01.709  -20 32 55.27  25.3r 20KP11    266  C~6VL7      
2020 05  29.53371  19 10 01.425  -20 32 55.93  25.3r 20KP11    266  C~5Zeg      
2020 05  29.61905  19 10 01.144  -20 32 56.56  25.3r 20KP11    266  C~5Zeg      
2020 05  31.44139  19 09 55.214  -20 33 10.35  25.3r 20KP11    266  C~5Zeg      
2020 05  31.52961  19 09 54.916  -20 33 11.03  25.3r 20KP11    266  C~5Zeg      
2020 05  31.61814  19 09 54.617  -20 33 11.71  25.3r 20KP11    266  C~6VL7      
2020 06  21.45390  19 08 36.555  -20 36 13.41  25.4r 20KP11    266  C~5Zeg      
2020 06  21.53376  19 08 36.223  -20 36 14.17  25.4r 20KP11    266  C~5Zeg      
2020 06  21.61261  19 08 35.895  -20 36 14.92  25.4r 20KP11    266  C~6VL7      
2020 06  24.43648  19 08 24.271  -20 36 42.37  25.1r 20KP11    266  C~5Zeg      
2020 06  24.52739  19 08 23.887  -20 36 43.26  25.1r 20KP11    266  C~5Zeg      
2020 06  24.61708  19 08 23.510  -20 36 44.12  25.1r 20KP11    266  C~6VL7      
2020 08  12.26680  19 05 06.975  -20 45 09.89  25.7r 20KP11    266  C~6VL7      
2020 08  12.34843  19 05 06.693  -20 45 10.71  25.7r 20KP11    266  C~5Zeg      
2020 08  12.42950  19 05 06.415  -20 45 11.52  25.7r 20KP11    266  C~6VL7      
2020 08  14.24286  19 05 00.393  -20 45 29.62  25.1r 20KP11    266  C~5Zeg      
2020 08  14.33285  19 05 00.092  -20 45 30.52  25.1r 20KP11    266  C~5Zeg      
2020 08  14.42134  19 04 59.796  -20 45 31.39  25.1r 20KP11    266  C~6VL7      
2020 10  26.270819 19 04 08.895  -20 53 18.97        20KP11    250  S~5zHA      
2020 10  26.277138 19 04 08.904  -20 53 19.01        20KP11    250  S~5zHA      
2020 10  26.283457 19 04 08.910  -20 53 19.02        20KP11    250  S~5zHA      
2020 10  26.289777 19 04 08.918  -20 53 18.97        20KP11    250  S~5zHA      
2020 10  26.296096 19 04 08.929  -20 53 18.92        20KP11    250  S~5zHA      
2020 11  06.260646 19 04 37.915  -20 53 31.42        20KP11    250  S~5zHA      
2020 11  06.266965 19 04 37.930  -20 53 31.40        20KP11    250  S~5zHA      
2020 11  06.273285 19 04 37.942  -20 53 31.36        20KP11    250  S~5zHA      
2020 11  06.279604 19 04 37.957  -20 53 31.30        20KP11    250  S~5zHA      
2020 11  06.285924 19 04 37.973  -20 53 31.26        20KP11    250  S~5zHA      
2021 03  04.218589 19 13 51.431  -20 44 50.03        20KP11    250  S~5zHA      
2021 03  04.224908 19 13 51.449  -20 44 49.99        20KP11    250  S~5zHA      
2021 03  04.231228 19 13 51.461  -20 44 49.93        20KP11    250  S~5zHA      
2021 03  04.237547 19 13 51.476  -20 44 49.88        20KP11    250  S~5zHA      
2021 03  04.243867 19 13 51.493  -20 44 49.86        20KP11    250  S~5zHA      
2021 06  09.44201  19 13 13.474  -20 48 48.69  25.5r 20KP11    266  C~6Ion      
2021 06  09.52741  19 13 13.155  -20 48 49.47  25.5r 20KP11    266  C~6Ion      
2021 06  09.61426  19 13 12.831  -20 48 50.24  25.5r 20KP11    266  C~6Ion      
2021 06  17.43605  19 12 43.011  -20 50 03.61  25.5r 20KP11    266  C~6Ion      
2021 06  17.50053  19 12 42.752  -20 50 04.24  25.5r 20KP11    266  C~6Ion      
2021 06  17.57953  19 12 42.435  -20 50 05.00  25.5r 20KP11    266  C~6Ion      
2021 07  05.35106  19 11 28.852  -20 53 07.42  24.9r 20KP11    266  C~6Ion      
2021 07  05.43951  19 11 28.469  -20 53 08.37  24.9r 20KP11    266  C~6Ion      
2021 07  05.52517  19 11 28.098  -20 53 09.28  24.9r 20KP11    266  C~6Ion      
2021 09  06.23258  19 07 48.622  -21 03 43.37  26.3r 20KP11    266  C~6Ion      
2021 09  06.31281  19 07 48.463  -21 03 44.01  26.3r 20KP11    266  C~6Ion      
2021 09  06.39352  19 07 48.304  -21 03 44.65  26.3r 20KP11    266  C~6Ion      
2022 06  29.45229  19 15 44.146  -21 06 16.05  25.0r 20KP11    266  C~7uln      
2022 06  29.51531  19 15 43.878  -21 06 16.73  25.0r 20KP11    266  C~7uln      
2022 06  29.57696  19 15 43.615  -21 06 17.39  25.0r 20KP11    266  C~7uln      
2022 06  30.45132  19 15 39.953  -21 06 26.87  24.9r 20KP11    266  C~7uln      
2022 06  30.51472  19 15 39.682  -21 06 27.55  24.9r 20KP11    266  C~7uln      
2022 06  30.57688  19 15 39.416  -21 06 28.22  24.9r 20KP11    266  C~7uln      
2022 10  20.21696  19 11 24.551  -21 21 51.49  24.2V 20KP11    266  C~7uln      
2022 10  20.26058  19 11 24.616  -21 21 51.56  24.2V 20KP11    266  C~7uln      
2022 10  20.29842  19 11 24.672  -21 21 51.63  24.2V 20KP11    266  C~7uln      
2022 10  21.20926  19 11 26.121  -21 21 53.27  24.4V 20KP11    266  C~7uln      
2022 10  21.25420  19 11 26.191  -21 21 53.34  24.4V 20KP11    266  C~7uln      
2022 10  21.29846  19 11 26.261  -21 21 53.41  24.4V 20KP11    266  C~7uln      
2023 09  09.22891  19 15 18.114  -21 32 33.24  23.9V 20KP11    266  C~7uln      
2023 09  09.32430  19 15 17.929  -21 32 33.96  23.9V 20KP11    266  C~7uln      
2023 09  09.41985  19 15 17.746  -21 32 34.66  23.9V 20KP11    266  C~7uln      
2023 09  10.22905  19 15 16.282  -21 32 40.74  23.7V 20KP11    266  C~7uln      
2023 09  10.32490  19 15 16.104  -21 32 41.45  23.7V 20KP11    266  C~7uln      
2023 09  10.42059  19 15 15.927  -21 32 42.14  23.7V 20KP11    266  C~7uln      

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    -0.07       0.00     0.02
     2   0.0002     -2.57    -0.08      -0.11     0.02
     3   0.0082   -133.11     0.00      -5.83     0.02
     4   0.0084   -137.15     0.00      -6.00     0.02
     5   0.0087   -141.15    -0.01      -6.16     0.02
     6   0.0137   -225.49     0.02      -9.88     0.00
     7   0.0139   -229.72     0.02     -10.06     0.01
     8   0.0141   -233.98     0.03     -10.23     0.00
     9   0.0712  -1344.02    -0.03     -60.66     0.01
    10   0.0714  -1348.74    -0.02     -60.87     0.01
    11   0.0716  -1353.40    -0.03     -61.07     0.01
    12   0.0794  -1518.71     0.01     -69.17     0.00
    13   0.0796  -1524.16     0.01     -69.42     0.00
    14   0.0798  -1529.52     0.02     -69.65     0.00
    15   0.2130  -4327.98     0.05    -255.63     0.01
    16   0.2133  -4332.00     0.04    -256.00     0.01
    17   0.2135  -4335.97     0.05    -256.37     0.00
    18   0.2185  -4421.97    -0.01    -264.89     0.01
    19   0.2187  -4426.27    -0.00    -265.31     0.01
    20   0.2189  -4430.50    -0.01    -265.71     0.01
    21   0.4184  -5192.21     0.15    -651.01    -0.11
    22   0.4184  -5192.09     0.08    -651.06    -0.13
    23   0.4184  -5192.00    -0.03    -651.08    -0.12
    24   0.4184  -5191.89    -0.11    -651.04    -0.05
    25   0.4185  -5191.73    -0.15    -651.01     0.02
    26   0.4485  -4789.19     0.13    -708.57    -0.11
    27   0.4485  -4788.98     0.08    -708.57    -0.08
    28   0.4485  -4788.80    -0.02    -708.55    -0.03
    29   0.4485  -4788.59    -0.07    -708.51     0.04
    30   0.4486  -4788.36    -0.11    -708.50     0.08
    31   0.7714   2979.57     0.15   -1110.81    -0.03
    32   0.7715   2979.83     0.11   -1110.80    -0.01
    33   0.7715   2980.00    -0.01   -1110.76     0.04
    34   0.7715   2980.22    -0.10   -1110.74     0.07
    35   0.7715   2980.46    -0.16   -1110.75     0.07
    36   1.0376   2421.48    -0.01   -1280.99     0.05
    37   1.0379   2416.95    -0.02   -1281.21     0.04
    38   1.0381   2412.34    -0.01   -1281.41     0.04
    39   1.0595   1988.33     0.01   -1302.25     0.00
    40   1.0597   1984.65     0.01   -1302.43    -0.00
    41   1.0599   1980.14     0.01   -1302.63    -0.00
    42   1.1086    934.07     0.04   -1356.88     0.01
    43   1.1088    928.63     0.05   -1357.17     0.01
    44   1.1090    923.35     0.05   -1357.44     0.01
    45   1.2807  -2204.48    -0.02   -1620.81     0.02
    46   1.2809  -2206.77    -0.01   -1621.18     0.02
    47   1.2812  -2209.05    -0.01   -1621.56     0.02
    48   2.0917   4383.22     0.00   -2587.53    -0.03
    49   2.0919   4379.41     0.01   -2587.72    -0.03
    50   2.0921   4375.67     0.00   -2587.91    -0.03
    51   2.0945   4323.61     0.01   -2590.72    -0.01
    52   2.0946   4319.76     0.02   -2590.90    -0.01
    53   2.0948   4315.98     0.01   -2591.09    -0.01
    54   2.4005    664.14    -0.00   -3060.96    -0.04
    55   2.4006    665.04     0.00   -3061.14    -0.03
    56   2.4007    665.80    -0.01   -3061.31    -0.04
    57   2.4032    685.70     0.01   -3065.40     0.06
    58   2.4033    686.66     0.00   -3065.59     0.07
    59   2.4034    687.62     0.01   -3065.78     0.06
    60   3.2875   3820.16    -0.03   -4105.67    -0.01
    61   3.2878   3817.51    -0.04   -4106.05    -0.01
    62   3.2881   3814.89    -0.03   -4106.42    -0.01
    63   3.2903   3793.84     0.01   -4109.84    -0.00
    64   3.2905   3791.29     0.02   -4110.22    -0.00
    65   3.2908   3788.75     0.01   -4110.59    -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.

20KP11    quality flag:3

Type:       SCATEXTD  SCATEXTD  SCATEXTD

axisobj        45.253    45.272    45.233
ecceobj         0.163     0.164     0.162
incobj         22.225    22.226    22.225
qmin           36.940    36.906    36.887
qmax           54.394    54.542    54.488
amean          45.481    45.503    45.483
amin           45.072    45.063    45.069
amax           45.977    45.968    45.964
emean           0.167     0.169     0.169
emin            0.149     0.152     0.151
emax            0.185     0.187     0.186
imean          20.546    20.533    20.505
imin           20.046    20.068    20.071
imax           21.045    21.037    20.986
excite_mean     0.389     0.389     0.389
fracstop        1.000     1.000     1.000
cjmean          2.932     2.931     2.932

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       169.4     169.0     169.3
kozaiamp        180.0     180.0     180.0