Orbit Fit and Astrometric record for 17DY166

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: 17DY166   
# Created Wed Jul 17 01:11:32 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     67 observations of     67
# Arc:  18.92y
# First observation: 2000/05/05
#  Last observation: 2019/04/06
# Chi-squared of fit:    22.43 DOF:    128 RMS:  0.10
# Min/Max residuals:    -0.26    0.32
# Exact a, adot, b, bdot, g, gdot:
  1.805330E-05  3.212105E-02  6.191721E-06  9.720940E-03  2.754984E-02 -5.054363E-03
# Covariance matrix:
  4.6497E-13 -4.9191E-14  6.0606E-14 -9.7056E-15 -4.9115E-15 -3.2682E-14
 -4.9191E-14  6.4600E-15 -1.0207E-14  1.6405E-15  2.6904E-15  5.5526E-15
  6.0606E-14 -1.0207E-14  2.8213E-13 -1.9614E-14 -1.1163E-14 -1.1118E-14
 -9.7056E-15  1.6405E-15 -1.9614E-14  1.5967E-15  1.9314E-15  1.8006E-15
 -4.9115E-15  2.6904E-15 -1.1163E-14  1.9314E-15  4.5746E-14  7.1898E-15
 -3.2682E-14  5.5526E-15 -1.1118E-14  1.8006E-15  7.1898E-15  6.1594E-15
#      lat0       lon0       xBary       yBary       zBary        JD0
   -7.370134  155.335895   -0.951944   -0.045703   -0.351607  2451669.715270
# Heliocentric elements and errors
Epoch:              2451670.5000  =  2000/05/06
Mean Anomaly:          351.04845 +/-     0.002
Argument of Peri:        0.17084 +/-     0.000
Long of Asc Node:      179.36867 +/-     0.000
Inclination:            18.47112 +/-     0.000
Eccentricity:         0.42088639 +/-    0.0000
Semi-Major Axis:     61.70414387 +/-    0.0001
Time of Perihelion: 2456072.6594 +/-       1.2
Perihelion:          35.73370968 +/-    0.0003
Aphelion:            87.67457805 +/-    0.0004
Period (y)              484.7075 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -33.42722582 +/-    0.0001
Ecliptic Y           14.30781153 +/-    0.0001
Ecliptic Z           -4.65598798 +/-    0.0000
Ecliptic XDOT        -0.00099845 +/-    0.0000
Ecliptic YDOT        -0.00305063 +/-    0.0000
Ecliptic ZDOT         0.00102263 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   36.65756950 +/-    0.0001
Geocenter to KBO     36.29799672 +/-    0.0001
# Hcoef:  7.41

The following table shows the complete astrometric record for 17DY166. 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 (17DY166) followed by the observatory code and reference code for the source of the astrometry.

2000 05  05.214527 10 17 49.48   +02 41 22.9   23.1r 17DY166   645  C~85J0      
2000 05  05.215357 10 17 49.47   +02 41 23.1   21.7i 17DY166   645  C~85J0      
2000 05  05.217844 10 17 49.48   +02 41 23.1   23.5g 17DY166   645  C~85J0      
2013 04  20.224715 12 02 53.16   +00 23 25.3   22.5z 17DY166   W84  C~85J0      
2013 05  11.121066 12 01 41.43   +00 33 21.2   23.9g 17DY166   W84  C~85J0      
2013 05  11.126357 12 01 41.41   +00 33 21.5   23.9g 17DY166   W84  C~85J0      
2013 05  11.129007 12 01 41.40   +00 33 21.5   23.0r 17DY166   W84  C~85J0      
2013 05  11.131643 12 01 41.39   +00 33 21.6   23.0r 17DY166   W84  C~85J0      
2013 05  11.134302 12 01 41.39   +00 33 21.6   22.9r 17DY166   W84  C~85J0      
2013 05  11.137516 12 01 41.38   +00 33 21.6   22.7i 17DY166   W84  C~85J0      
2013 05  11.141309 12 01 41.37   +00 33 21.8   22.9i 17DY166   W84  C~85J0      
2013 05  11.145127 12 01 41.36   +00 33 21.7   22.5i 17DY166   W84  C~85J0      
2013 05  12.108897 12 01 38.84   +00 33 44.0   23.6g 17DY166   W84  C~85J0      
2013 05  12.111549 12 01 38.83   +00 33 44.1   23.5g 17DY166   W84  C~85J0      
2013 05  12.114192 12 01 38.82   +00 33 44.2   23.7g 17DY166   W84  C~85J0      
2013 05  12.116864 12 01 38.82   +00 33 44.2   22.7r 17DY166   W84  C~85J0      
2013 05  12.119523 12 01 38.80   +00 33 44.3   22.9r 17DY166   W84  C~85J0      
2013 05  12.122175 12 01 38.80   +00 33 44.3   22.6r 17DY166   W84  C~85J0      
2013 05  12.125392 12 01 38.79   +00 33 44.5   22.5i 17DY166   W84  C~85J0      
2013 05  12.129222 12 01 38.78   +00 33 44.4   22.4i 17DY166   W84  C~85J0      
2013 05  12.133033 12 01 38.76   +00 33 44.3   22.3i 17DY166   W84  C~85J0      
2013 06  07.055649 12 01 02.13   +00 40 12.3   23.3g 17DY166   W84  C~85J0      
2013 06  07.057431 12 01 02.12   +00 40 12.3   23.5g 17DY166   W84  C~85J0      
2013 06  07.060180 12 01 02.12   +00 40 12.2   23.8g 17DY166   W84  C~85J0      
2013 06  07.062929 12 01 02.12   +00 40 12.2   23.8g 17DY166   W84  C~85J0      
2013 06  07.065690 12 01 02.12   +00 40 12.3   22.8r 17DY166   W84  C~85J0      
2013 06  07.068442 12 01 02.12   +00 40 12.3   22.8r 17DY166   W84  C~85J0      
2013 06  07.071197 12 01 02.12   +00 40 12.3   22.9r 17DY166   W84  C~85J0      
2013 06  07.074529 12 01 02.12   +00 40 12.3   22.5i 17DY166   W84  C~85J0      
2013 06  07.078460 12 01 02.12   +00 40 12.4   22.4i 17DY166   W84  C~85J0      
2013 06  07.082315 12 01 02.11   +00 40 12.4   22.6i 17DY166   W84  C~85J0      
2015 02  17.380060 12 24 04.20   -00 36 31.1   23.6g 17DY166   W84  C~85J0      
2015 02  17.384021 12 24 04.19   -00 36 30.9   23.0g 17DY166   W84  C~85J0      
2015 02  17.387979 12 24 04.17   -00 36 30.6   22.9r 17DY166   W84  C~85J0      
2015 02  17.390617 12 24 04.16   -00 36 30.5   22.9r 17DY166   W84  C~85J0      
2015 02  18.379247 12 24 00.63   -00 35 58.8   23.5g 17DY166   W84  C~85J0      
2015 02  18.381885 12 24 00.62   -00 35 58.7   23.1g 17DY166   W84  C~85J0      
2015 02  19.376474 12 23 57.00   -00 35 26.1   23.4g 17DY166   W84  C~85J0      
2015 02  19.379120 12 23 56.99   -00 35 25.9   23.8g 17DY166   W84  C~85J0      
2015 02  19.380435 12 23 56.98   -00 35 26.1   23.0r 17DY166   W84  C~85J0      
2015 02  19.383076 12 23 56.97   -00 35 26.1   22.9r 17DY166   W84  C~85J0      
2015 02  19.385075 12 23 56.96   -00 35 25.9   22.9r 17DY166   W84  C~85J0      
2015 04  08.169607 12 20 17.86   -00 05 40.2   22.2z 17DY166   W84  C~85J0      
2016 04  05.440296 12 28 41.45   -00 17 46.7         17DY166   T09  C~85J0      
2016 04  05.564262 12 28 40.83   -00 17 42.1         17DY166   T09  C~85J0      
2017 02  23.52726  12 40 01.63   -00 54 19.7   24.0r 17DY166   T09  C~85J0      
2017 02  23.56764  12 40 01.48   -00 54 18.3   24.3r 17DY166   T09  C~85J0      
2017 02  23.60167  12 40 01.34   -00 54 17.3   24.0r 17DY166   T09  C~85J0      
2017 02  23.63983  12 40 01.21   -00 54 15.7   23.8r 17DY166   T09  C~85J0      
2017 02  23.64192  12 40 01.21   -00 54 15.8   23.7r 17DY166   T09  C~85J0      
2017 03  02.249708 12 39 35.41   -00 50 24.2   23.0g 17DY166   W84  C~85J0      
2017 03  03.273368 12 39 31.18   -00 49 47.3   22.4r 17DY166   W84  C~85J0      
2017 03  04.53892  12 39 25.87   -00 49 01.4   22.5y 17DY166   T09  C~85J0      
2017 03  04.58243  12 39 25.69   -00 48 59.7   22.2y 17DY166   T09  C~85J0      
2017 03  04.63107  12 39 25.48   -00 48 57.7   23.2y 17DY166   T09  C~85J0      
2019 02  27.353615 12 56 04.24   -01 13 29.9         17DY166   309  C~85J0      
2019 02  27.356905 12 56 04.26   -01 13 29.4         17DY166   309  C~85J0      
2019 02  27.360195 12 56 04.25   -01 13 29.6         17DY166   309  C~85J0      
2019 02  27.363485 12 56 04.22   -01 13 29.1         17DY166   309  C~85J0      
2019 03  29.336535 12 53 53.06   -00 54 52.7         17DY166   T09  C~85J0      
2019 04  03.477581 12 53 27.95   -00 51 37.4         17DY166   T09  C~85J0      
2019 04  03.488340 12 53 27.90   -00 51 37.1         17DY166   T09  C~85J0      
2019 04  04.520389 12 53 22.84   -00 50 58.2         17DY166   T09  C~85J0      
2019 04  06.35011  12 53 13.89   -00 49 49.5   22.9i 17DY166   T09  C~85J0      
2019 04  06.44937  12 53 13.40   -00 49 46.2   22.3i 17DY166   T09  C~85J0      
2019 04  06.46047  12 53 13.34   -00 49 45.8   22.3i 17DY166   T09  C~85J0      
2019 04  06.51511  12 53 13.07   -00 49 43.5   22.4i 17DY166   T09  C~85J0      

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     0.03       0.00    -0.15
     2   0.0000      0.00    -0.11       0.00     0.04
     3   0.0000      0.00     0.06       0.00    -0.02
     4  12.9583      0.00     0.02       0.00     0.01
     5  13.0155      0.00     0.07       0.00    -0.05
     6  13.0155      0.00    -0.02       0.00     0.13
     7  13.0155      0.00    -0.06       0.00     0.07
     8  13.0155      0.00    -0.10       0.00     0.11
     9  13.0155      0.00     0.01       0.00     0.05
    10  13.0155      0.00    -0.01       0.00    -0.03
    11  13.0155      0.00     0.00       0.00     0.08
    12  13.0156      0.00     0.01       0.00    -0.11
    13  13.0182      0.00     0.10       0.00    -0.01
    14  13.0182      0.00     0.06       0.00     0.03
    15  13.0182      0.00     0.01       0.00     0.07
    16  13.0182      0.00     0.12       0.00     0.01
    17  13.0182      0.00    -0.07       0.00     0.05
    18  13.0182      0.00     0.03       0.00    -0.01
    19  13.0182      0.00     0.01       0.00     0.12
    20  13.0182      0.00     0.01       0.00    -0.07
    21  13.0183      0.00    -0.13       0.00    -0.26
    22  13.0892      0.00     0.12       0.00     0.11
    23  13.0892      0.00    -0.02       0.00     0.10
    24  13.0892      0.00    -0.01       0.00    -0.02
    25  13.0892      0.00     0.00       0.00    -0.04
    26  13.0893      0.00     0.01       0.00     0.04
    27  13.0893      0.00     0.02       0.00     0.03
    28  13.0893      0.00     0.03       0.00     0.01
    29  13.0893      0.00     0.04       0.00    -0.02
    30  13.0893      0.00     0.06       0.00     0.06
    31  13.0893      0.00    -0.08       0.00     0.03
    32  14.7876      0.00     0.01       0.00    -0.21
    33  14.7876      0.00     0.08       0.00    -0.13
    34  14.7876      0.00    -0.01       0.00     0.04
    35  14.7876      0.00    -0.02       0.00     0.05
    36  14.7903      0.00     0.02       0.00    -0.10
    37  14.7903      0.00     0.02       0.00    -0.08
    38  14.7931      0.00     0.06       0.00     0.07
    39  14.7931      0.00     0.05       0.00     0.19
    40  14.7931      0.00    -0.02       0.00    -0.06
    41  14.7931      0.00    -0.02       0.00    -0.14
    42  14.7931      0.00    -0.06       0.00    -0.01
    43  14.9239      0.00     0.02       0.00     0.00
    44  15.9185      0.00     0.04       0.00    -0.02
    45  15.9188      0.00    -0.10       0.00    -0.07
    46  16.8058      0.00    -0.13       0.00     0.08
    47  16.8059      0.00    -0.09       0.00     0.11
    48  16.8060      0.00    -0.25       0.00    -0.05
    49  16.8061      0.00    -0.04       0.00     0.25
    50  16.8061      0.00     0.08       0.00     0.08
    51  16.8242      0.00    -0.03       0.00    -0.03
    52  16.8270      0.00    -0.07       0.00    -0.10
    53  16.8305      0.00    -0.18       0.00    -0.07
    54  16.8306      0.00    -0.06       0.00     0.04
    55  16.8307      0.00    -0.07       0.00     0.26
    56  18.8149      0.00    -0.20       0.00    -0.21
    57  18.8149      0.00     0.28       0.00     0.17
    58  18.8149      0.00     0.32       0.00    -0.14
    59  18.8149      0.00     0.05       0.00     0.25
    60  18.8970      0.00     0.12       0.00    -0.08
    61  18.9111      0.00    -0.01       0.00    -0.02
    62  18.9111      0.00     0.05       0.00    -0.12
    63  18.9139      0.00    -0.00       0.00    -0.05
    64  18.9189      0.00    -0.09       0.00     0.19
    65  18.9192      0.00    -0.01       0.00    -0.21
    66  18.9192      0.00    -0.08       0.00    -0.23
    67  18.9194      0.00    -0.04       0.00     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.