Orbit Fit and Astrometric record for 17EO50

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: 17EO50    
# Created Sun Nov 24 02:10:50 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     65 observations of     65
# Arc:   6.87y
# First observation: 2013/04/03
#  Last observation: 2020/02/14
# Chi-squared of fit:    23.88 DOF:    124 RMS:  0.11
# Min/Max residuals:    -0.31    0.29
# Exact a, adot, b, bdot, g, gdot:
  1.596354E-05  2.494635E-02 -2.473710E-06 -3.301298E-03  2.489587E-02 -1.212958E-03
# Covariance matrix:
  1.2680E-12 -5.1871E-13 -1.1396E-13  5.6536E-14 -1.9628E-13 -1.9626E-12
 -5.1871E-13  2.7995E-13  6.8939E-14 -3.5283E-14  3.3152E-14  1.2143E-12
 -1.1396E-13  6.8939E-14  3.8149E-13 -9.1102E-14  7.3557E-15  3.2226E-13
  5.6536E-14 -3.5283E-14 -9.1102E-14  2.4394E-14 -2.2961E-15 -1.6572E-13
 -1.9628E-13  3.3152E-14  7.3557E-15 -2.2961E-15  1.1959E-13  9.2841E-14
 -1.9626E-12  1.2143E-12  3.2226E-13 -1.6572E-13  9.2841E-14  5.6959E-12
#      lat0       lon0       xBary       yBary       zBary        JD0
   -7.746991  143.518572   -0.765300   -0.086924   -0.639540  2456385.532368
# Heliocentric elements and errors
Epoch:              2456386.5000  =  2013/04/04
Mean Anomaly:          337.03631 +/-     0.078
Argument of Peri:      252.48170 +/-     0.091
Long of Asc Node:      278.82498 +/-     0.001
Inclination:            10.57965 +/-     0.000
Eccentricity:         0.06710278 +/-    0.0000
Semi-Major Axis:     43.46780687 +/-    0.0028
Time of Perihelion: 2463063.6194 +/-      24.7
Perihelion:          40.55099612 +/-    0.0032
Aphelion:            46.38461762 +/-    0.0035
Period (y)              286.5892 +/-      0.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -32.97536644 +/-    0.0005
Ecliptic Y           23.43440888 +/-    0.0003
Ecliptic Z           -5.41463222 +/-    0.0001
Ecliptic XDOT        -0.00149179 +/-    0.0000
Ecliptic YDOT        -0.00231309 +/-    0.0000
Ecliptic ZDOT        -0.00034162 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   40.81502195 +/-    0.0004
Geocenter to KBO     40.16738422 +/-    0.0006
# Hcoef:  7.13

The following table shows the complete astrometric record for 17EO50. 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 (17EO50) followed by the observatory code and reference code for the source of the astrometry.

2013 04  03.031590 09 33 08.77   +06 21 14.0         17EO50    W84  C~81By      
2015 04  17.040437 09 43 02.969  +05 08 35.16  23.3r 17EO50    W84  C~8HKi      
2016 12  23.46867  10 00 46.97   +03 13 55.2   22.7z 17EO50    T09  C~7n3f      
2016 12  23.51848  10 00 46.86   +03 13 55.0   23.2z 17EO50    T09  C~7n3f      
2016 12  23.58951  10 00 46.68   +03 13 55.0   23.3z 17EO50    T09  C~7n3f      
2016 12  23.63426  10 00 46.58   +03 13 55.0   23.4z 17EO50    T09  C~7n3f      
2016 12  25.51058  10 00 42.12   +03 13 54.7   23.4r 17EO50    T09  C~7n3f      
2016 12  25.58308  10 00 41.94   +03 13 54.7   23.1i 17EO50    T09  C~7n3f      
2016 12  25.60907  10 00 41.87   +03 13 54.5   23.4i 17EO50    T09  C~7n3f      
2017 01  02.54073  10 00 19.80   +03 14 15.3   23.1i 17EO50    T09  C~7n3f      
2017 01  02.54410  10 00 19.79   +03 14 15.1   22.8i 17EO50    T09  C~7n3f      
2017 01  02.56030  10 00 19.73   +03 14 15.1   23.0i 17EO50    T09  C~7n3f      
2017 01  02.64649  10 00 19.45   +03 14 15.8   23.6g 17EO50    T09  C~7n3f      
2017 01  02.64928  10 00 19.45   +03 14 15.8   23.7g 17EO50    T09  C~7n3f      
2017 01  21.42316  09 59 10.10   +03 17 21.8   22.6z 17EO50    T09  C~7n3f      
2017 01  21.42903  09 59 10.08   +03 17 21.8   22.7z 17EO50    T09  C~7n3f      
2017 01  21.46362  09 59 09.93   +03 17 22.3   22.7z 17EO50    T09  C~7n3f      
2017 01  21.46896  09 59 09.91   +03 17 22.3   22.6z 17EO50    T09  C~7n3f      
2017 01  21.47486  09 59 09.88   +03 17 22.3   22.7z 17EO50    T09  C~7n3f      
2017 01  21.50089  09 59 09.78   +03 17 22.8   22.7z 17EO50    T09  C~7n3f      
2017 01  21.52708  09 59 09.66   +03 17 23.1   22.8z 17EO50    T09  C~7n3f      
2017 01  21.58938  09 59 09.40   +03 17 24.1   23.1z 17EO50    T09  C~7n3f      
2017 01  23.35517  09 59 01.88   +03 17 50.8   23.5r 17EO50    T09  C~7n3f      
2017 01  23.37982  09 59 01.77   +03 17 51.1   23.4r 17EO50    T09  C~7n3f      
2017 01  23.38883  09 59 01.74   +03 17 51.3   23.4r 17EO50    T09  C~7n3f      
2017 01  23.40271  09 59 01.67   +03 17 51.4   23.3r 17EO50    T09  C~7n3f      
2017 01  23.42310  09 59 01.60   +03 17 51.9   23.5r 17EO50    T09  C~7n3f      
2017 01  23.44005  09 59 01.51   +03 17 52.1   23.6r 17EO50    T09  C~7n3f      
2017 01  23.45653  09 59 01.44   +03 17 52.3   23.4r 17EO50    T09  C~7n3f      
2017 01  23.50979  09 59 01.22   +03 17 53.1   23.0i 17EO50    T09  C~7n3f      
2017 01  23.54000  09 59 01.07   +03 17 53.6   23.0i 17EO50    T09  C~7n3f      
2017 01  23.55094  09 59 01.04   +03 17 53.8   23.0i 17EO50    T09  C~7n3f      
2017 01  23.57255  09 59 00.94   +03 17 54.0   22.9i 17EO50    T09  C~7n3f      
2017 01  23.58131  09 59 00.89   +03 17 54.3   23.0i 17EO50    T09  C~7n3f      
2017 01  30.42829  09 58 30.49   +03 19 51.3   23.2i 17EO50    T09  C~7n3f      
2017 01  30.45035  09 58 30.40   +03 19 51.6   23.1i 17EO50    T09  C~7n3f      
2017 01  30.52066  09 58 30.05   +03 19 53.0   22.8z 17EO50    T09  C~7n3f      
2017 01  30.58347  09 58 29.76   +03 19 54.1   22.8z 17EO50    T09  C~7n3f      
2017 01  30.60540  09 58 29.66   +03 19 54.6   22.6z 17EO50    T09  C~7n3f      
2017 02  21.31699  09 56 46.63   +03 27 56.5   23.1z 17EO50    T09  C~7n3f      
2017 02  21.34253  09 56 46.49   +03 27 56.8   22.9z 17EO50    T09  C~7n3f      
2017 02  21.36806  09 56 46.37   +03 27 57.5   22.8z 17EO50    T09  C~7n3f      
2017 02  21.39368  09 56 46.24   +03 27 58.1   22.8z 17EO50    T09  C~7n3f      
2017 02  21.41563  09 56 46.14   +03 27 58.6   23.0z 17EO50    T09  C~7n3f      
2017 02  23.46231  09 56 36.37   +03 28 50.3   23.2r 17EO50    T09  C~7n3f      
2017 02  23.47596  09 56 36.30   +03 28 50.6   23.1r 17EO50    T09  C~7n3f      
2017 02  23.48959  09 56 36.23   +03 28 51.1   23.4r 17EO50    T09  C~7n3f      
2017 02  23.50705  09 56 36.15   +03 28 51.6   23.2r 17EO50    T09  C~7n3f      
2017 03  04.25993  09 55 55.19   +03 32 39.5   22.7z 17EO50    T09  C~7n3f      
2017 03  04.28551  09 55 55.08   +03 32 40.1   23.0z 17EO50    T09  C~7n3f      
2017 03  04.44888  09 55 54.32   +03 32 44.3   23.1i 17EO50    T09  C~7n3f      
2017 03  04.47080  09 55 54.23   +03 32 45.0   23.2i 17EO50    T09  C~7n3f      
2019 02  05.36641  10 08 32.38   +02 02 01.4   23.5i 17EO50    T09  C~81By      
2019 02  05.40928  10 08 32.16   +02 02 01.9   23.0i 17EO50    T09  C~81By      
2019 02  05.42270  10 08 32.11   +02 02 02.2   22.9i 17EO50    T09  C~81By      
2019 03  01.180214 10 06 39.348  +02 11 29.90  23.8g 17EO50    W84  C~8HKi      
2019 03  01.182757 10 06 39.338  +02 11 29.87  22.9r 17EO50    W84  C~8HKi      
2019 03  01.185058 10 06 39.326  +02 11 29.94  23.3i 17EO50    W84  C~8HKi      
2019 03  01.186455 10 06 39.322  +02 11 30.12  22.6i 17EO50    W84  C~8HKi      
2019 03  03.325025 10 06 29.31   +02 12 27.1         17EO50    T09  C~81By      
2019 03  25.020785 10 04 56.287  +02 22 23.52  23.4r 17EO50    W84  C~8HKi      
2019 03  25.023312 10 04 56.275  +02 22 23.70  22.8i 17EO50    W84  C~8HKi      
2019 04  11.005239 10 04 01.049  +02 29 41.10  23.3r 17EO50    W84  C~8HKi      
2019 05  02.987347 10 03 22.507  +02 37 06.85  22.7i 17EO50    W84  C~8HKi      
2020 02  14.276162 10 13 04.88   +01 25 12.7         17EO50    W84  C~81By      

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     0.00       0.00     0.08
     2   2.0370      0.00     0.10       0.00     0.17
     3   3.7247      0.00    -0.06       0.00     0.05
     4   3.7248      0.00     0.05       0.00    -0.10
     5   3.7250      0.00    -0.11       0.00    -0.04
     6   3.7251      0.00    -0.00       0.00    -0.01
     7   3.7303      0.00     0.04       0.00     0.20
     8   3.7305      0.00     0.11       0.00     0.18
     9   3.7305      0.00     0.05       0.00    -0.03
    10   3.7522      0.00     0.05       0.00     0.12
    11   3.7523      0.00     0.06       0.00    -0.10
    12   3.7523      0.00    -0.07       0.00    -0.18
    13   3.7525      0.00    -0.16       0.00     0.10
    14   3.7525      0.00    -0.03       0.00     0.09
    15   3.8039      0.00    -0.14       0.00     0.15
    16   3.8040      0.00    -0.06       0.00     0.06
    17   3.8041      0.00    -0.09       0.00     0.05
    18   3.8041      0.00    -0.04       0.00    -0.02
    19   3.8041      0.00    -0.11       0.00    -0.11
    20   3.8042      0.00     0.07       0.00     0.01
    21   3.8042      0.00    -0.04       0.00    -0.08
    22   3.8044      0.00     0.08       0.00     0.01
    23   3.8092      0.00    -0.09       0.00     0.07
    24   3.8093      0.00    -0.13       0.00    -0.02
    25   3.8093      0.00     0.01       0.00     0.04
    26   3.8094      0.00    -0.13       0.00    -0.07
    27   3.8094      0.00     0.16       0.00     0.11
    28   3.8095      0.00    -0.08       0.00     0.04
    29   3.8095      0.00    -0.05       0.00    -0.01
    30   3.8097      0.00     0.16       0.00    -0.04
    31   3.8097      0.00    -0.10       0.00    -0.01
    32   3.8098      0.00     0.18       0.00     0.02
    33   3.8098      0.00     0.10       0.00    -0.12
    34   3.8099      0.00    -0.07       0.00     0.05
    35   3.8286      0.00     0.06       0.00     0.03
    36   3.8287      0.00     0.25       0.00    -0.08
    37   3.8289      0.00    -0.10       0.00     0.02
    38   3.8290      0.00    -0.07       0.00    -0.05
    39   3.8291      0.00    -0.05       0.00     0.05
    40   3.8885      0.00     0.15       0.00     0.29
    41   3.8886      0.00    -0.09       0.00    -0.05
    42   3.8887      0.00    -0.03       0.00     0.01
    43   3.8887      0.00    -0.11       0.00    -0.03
    44   3.8888      0.00    -0.00       0.00    -0.08
    45   3.8944      0.00     0.13       0.00    -0.08
    46   3.8944      0.00     0.08       0.00    -0.13
    47   3.8945      0.00     0.02       0.00     0.03
    48   3.8945      0.00     0.08       0.00     0.08
    49   3.9185      0.00    -0.20       0.00    -0.09
    50   3.9186      0.00    -0.07       0.00    -0.17
    51   3.9190      0.00    -0.08       0.00    -0.31
    52   3.9191      0.00     0.10       0.00    -0.19
    53   5.8435      0.00     0.08       0.00     0.10
    54   5.8436      0.00    -0.20       0.00    -0.26
    55   5.8436      0.00    -0.01       0.00    -0.23
    56   5.9087      0.00     0.03       0.00     0.11
    57   5.9087      0.00     0.06       0.00     0.01
    58   5.9087      0.00     0.05       0.00     0.02
    59   5.9087      0.00     0.09       0.00     0.16
    60   5.9146      0.00     0.00       0.00    -0.01
    61   5.9740      0.00    -0.01       0.00     0.01
    62   5.9740      0.00    -0.04       0.00     0.12
    63   6.0205      0.00    -0.01       0.00    -0.09
    64   6.0806      0.00    -0.16       0.00     0.08
    65   6.8672      0.00     0.20       0.00     0.21

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.

17EO50    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        43.335    43.334    43.335
ecceobj         0.063     0.063     0.063
incobj         10.583    10.583    10.583
qmin           39.969    39.982    39.958
qmax           46.969    46.977    46.966
amean          43.358    43.358    43.358
amin           43.028    43.027    43.015
amax           43.715    43.712    43.715
emean           0.061     0.061     0.061
emin            0.048     0.048     0.048
emax            0.075     0.075     0.075
imean          12.329    12.329    12.329
imin           11.707    11.706    11.709
imax           12.826    12.827    12.826
excite_mean     0.222     0.222     0.222
fracstop        1.000     1.000     1.000
cjmean          3.034     3.034     3.034

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       185.2     185.3     185.2
kozaiamp        179.9     179.9     180.0