Orbit Fit and Astrometric record for 17DJ171

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: 17DJ171   
# Created Sun Nov 24 02:10:50 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     25 observations of     25
# Arc:  17.05y
# First observation: 2002/03/20
#  Last observation: 2019/04/06
# Chi-squared of fit:    10.26 DOF:     44 RMS:  0.11
# Min/Max residuals:    -0.32    0.31
# Exact a, adot, b, bdot, g, gdot:
  1.582006E-05  2.488689E-02  3.719637E-06  5.789657E-03  2.528567E-02 -3.097331E-03
# Covariance matrix:
  4.8852E-13 -5.7403E-14  4.2692E-15 -6.1656E-15 -2.2317E-14 -5.9995E-14
 -5.7403E-14  4.4444E-14 -6.7757E-15  9.8043E-15  3.4656E-15  9.5511E-14
  4.2692E-15 -6.7757E-15  4.7180E-13 -3.2516E-14 -8.6915E-16 -1.5343E-14
 -6.1656E-15  9.8043E-15 -3.2516E-14  4.5388E-15  1.0601E-15  2.2199E-14
 -2.2317E-14  3.4656E-15 -8.6915E-16  1.0601E-15  3.3652E-13  9.1861E-15
 -5.9995E-14  9.5511E-14 -1.5343E-14  2.2199E-14  9.1861E-15  2.1626E-13
#      lat0       lon0       xBary       yBary       zBary        JD0
   -1.135240  167.834236   -0.206490   -0.019385   -0.974920  2452353.794788
# Heliocentric elements and errors
Epoch:              2452354.5000  =  2002/03/21
Mean Anomaly:          306.54842 +/-     0.022
Argument of Peri:       61.67428 +/-     0.029
Long of Asc Node:      172.87124 +/-     0.000
Inclination:            13.13742 +/-     0.000
Eccentricity:         0.12975096 +/-    0.0000
Semi-Major Axis:     43.34569074 +/-    0.0044
Time of Perihelion: 2467831.0917 +/-      14.9
Perihelion:          37.72154584 +/-    0.0041
Aphelion:            48.96983565 +/-    0.0052
Period (y)              285.3823 +/-      0.04
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -39.64831478 +/-    0.0009
Ecliptic Y            8.34132353 +/-    0.0002
Ecliptic Z           -0.78339355 +/-    0.0000
Ecliptic XDOT        -0.00026066 +/-    0.0000
Ecliptic YDOT        -0.00270336 +/-    0.0000
Ecliptic ZDOT         0.00063362 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   40.52389463 +/-    0.0009
Geocenter to KBO     39.54819304 +/-    0.0009
# Hcoef:  8.28

The following table shows the complete astrometric record for 17DJ171. 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 (17DJ171) followed by the observatory code and reference code for the source of the astrometry.

2002 03  20.294045 11 13 28.27   +03 45 47.7         17DJ171   T14  C~89Ua      
2002 03  20.328210 11 13 28.12   +03 45 48.9         17DJ171   T14  C~89Ua      
2002 03  20.363013 11 13 27.96   +03 45 49.8         17DJ171   T14  C~89Ua      
2016 04  04.442534 12 36 20.52   +00 05 34.5         17DJ171   T09  C~89Ua      
2016 04  04.44255  12 36 20.51   +00 05 34.4   25.4g 17DJ171   T09  C~8COu      
2016 04  04.48066  12 36 20.33   +00 05 35.8   25.5g 17DJ171   T09  C~8COu      
2016 04  04.51309  12 36 20.16   +00 05 36.8   25.7g 17DJ171   T09  C~8COu      
2016 04  04.515201 12 36 20.17   +00 05 36.9         17DJ171   T09  C~89Ua      
2017 02  21.53656  12 45 36.54   -00 35 08.9   23.8z 17DJ171   T09  C~89Ua      
2017 02  21.53924  12 45 36.53   -00 35 08.9   23.5z 17DJ171   T09  C~89Ua      
2017 02  21.56076  12 45 36.45   -00 35 08.4   23.7z 17DJ171   T09  C~89Ua      
2017 02  21.56614  12 45 36.43   -00 35 08.1   23.5z 17DJ171   T09  C~89Ua      
2017 02  21.58766  12 45 36.38   -00 35 07.6   23.9z 17DJ171   T09  C~89Ua      
2017 02  21.60643  12 45 36.29   -00 35 07.3   23.8z 17DJ171   T09  C~89Ua      
2017 02  21.60910  12 45 36.28   -00 35 06.8   23.3z 17DJ171   T09  C~89Ua      
2017 02  23.54421  12 45 29.62   -00 34 08.8   24.2r 17DJ171   T09  C~89Ua      
2017 02  23.56973  12 45 29.53   -00 34 08.1   24.7r 17DJ171   T09  C~89Ua      
2017 02  23.61219  12 45 29.38   -00 34 06.9   23.9r 17DJ171   T09  C~89Ua      
2017 02  23.64192  12 45 29.27   -00 34 05.9   24.0r 17DJ171   T09  C~89Ua      
2017 02  23.64401  12 45 29.26   -00 34 06.1   24.1r 17DJ171   T09  C~89Ua      
2017 04  27.380876 12 40 53.66   -00 00 19.4         17DJ171   T09  C~89Ua      
2019 04  06.350099 12 55 04.86   -00 46 12.7         17DJ171   T09  C~89Ua      
2019 04  06.44937  12 55 04.36   -00 46 09.3   23.6i 17DJ171   T09  C~8COu      
2019 04  06.47397  12 55 04.25   -00 46 08.7   23.7i 17DJ171   T09  C~8COu      
2019 04  06.515104 12 55 04.06   -00 46 07.2         17DJ171   T09  C~89Ua      

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     0.00
     2   0.0001      0.00     0.03       0.00     0.10
     3   0.0002      0.00     0.01       0.00    -0.13
     4  14.0428      0.00     0.07       0.00     0.03
     5  14.0428      0.00    -0.07       0.00    -0.07
     6  14.0429      0.00    -0.05       0.00     0.07
     7  14.0430      0.00    -0.28       0.00    -0.01
     8  14.0430      0.00     0.02       0.00     0.02
     9  14.9274      0.00     0.05       0.00     0.15
    10  14.9274      0.00     0.04       0.00     0.07
    11  14.9275      0.00    -0.04       0.00    -0.06
    12  14.9275      0.00    -0.06       0.00     0.08
    13  14.9276      0.00     0.31       0.00    -0.06
    14  14.9276      0.00    -0.07       0.00    -0.32
    15  14.9276      0.00    -0.08       0.00     0.10
    16  14.9329      0.00    -0.02       0.00     0.20
    17  14.9330      0.00     0.01       0.00     0.13
    18  14.9331      0.00     0.05       0.00     0.04
    19  14.9332      0.00     0.00       0.00     0.14
    20  14.9332      0.00    -0.03       0.00    -0.12
    21  15.1050      0.00     0.16       0.00    -0.08
    22  17.0460      0.00     0.09       0.00    -0.05
    23  17.0463      0.00    -0.22       0.00     0.05
    24  17.0464      0.00    -0.08       0.00    -0.17
    25  17.0465      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.