Orbit Fit and Astrometric record for 17DO162

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: 17DO162   
# Created Fri Apr  4 01:11:04 2025
# Orbit generated from Bernstein formalism
# Fitting     22 observations of     22
# Arc:   0.90y
# First observation: 2016/04/02
#  Last observation: 2017/02/23
Preliminary a, adot, b, bdot, g, gdot:
  -0.000044   0.023449  -0.000001   0.001882   0.023595   0.000000
# Chi-squared of fit:     7.60 DOF:     38 RMS:  0.10
# Min/Max residuals:    -0.23    0.24
# Exact a, adot, b, bdot, g, gdot:
  1.432279E-05  2.331426E-02  1.222213E-06  1.900161E-03  2.403289E-02 -2.085038E-03
# Covariance matrix:
  2.5206E-13  3.8361E-12  1.1220E-16  2.0339E-13  1.6889E-12  1.4554E-10
  3.8361E-12  4.1643E-10 -7.9262E-14  1.9616E-11  1.4991E-10  1.4237E-08
  1.1220E-16 -7.9262E-14  1.7981E-13 -2.2405E-13 -2.2426E-14 -2.5311E-12
  2.0339E-13  1.9616E-11 -2.2405E-13  1.3633E-12  7.1528E-12  6.7378E-10
  1.6889E-12  1.4991E-10 -2.2426E-14  7.1528E-12  5.5598E-11  5.1769E-09
  1.4554E-10  1.4237E-08 -2.5311E-12  6.7378E-10  5.1769E-09  4.8858E-07
#      lat0       lon0       xBary       yBary       zBary        JD0
    2.925143 -175.076051   -0.136280    0.050468   -0.984956  2457480.904541
# Heliocentric elements and errors
Epoch:              2457480.5000  =  2016/04/02
Mean Anomaly:          297.60457 +/-     3.262
Argument of Peri:      103.97889 +/-     6.188
Long of Asc Node:      153.49905 +/-     0.010
Inclination:             5.43928 +/-     0.002
Eccentricity:         0.09235380 +/-    0.0290
Semi-Major Axis:     44.17482871 +/-    0.2242
Time of Perihelion: 2476067.5726 +/-     961.2
Perihelion:          40.09511525 +/-    1.2969
Aphelion:            48.25454216 +/-    1.3040
Period (y)              293.6098 +/-      2.23
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -42.37669112 +/-    0.0128
Ecliptic Y           -3.78991194 +/-    0.0011
Ecliptic Z            2.12346479 +/-    0.0007
Ecliptic XDOT         0.00047543 +/-    0.0001
Ecliptic YDOT        -0.00263185 +/-    0.0000
Ecliptic ZDOT         0.00020407 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   42.59878503 +/-    0.0128
Geocenter to KBO     41.60963892 +/-    0.0129
# Hcoef:  8.48

The following table shows the complete astrometric record for 17DO162. 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 (17DO162) followed by the observatory code and reference code for the source of the astrometry.

2016 04  02.403752 12 22 42.96   +00 43 44.2         17DO162   T09  C~83F2      
2016 04  02.525980 12 22 42.41   +00 43 47.7         17DO162   T09  C~83F2      
2016 04  04.35736  12 22 34.45   +00 44 40.4   25.6g 17DO162   T09  C~89UX      
2016 04  04.36800  12 22 34.40   +00 44 40.7   25.4g 17DO162   T09  C~89UX      
2016 04  04.39588  12 22 34.27   +00 44 41.4   25.6g 17DO162   T09  C~89UX      
2016 04  04.41508  12 22 34.20   +00 44 41.9   25.3g 17DO162   T09  C~89UX      
2016 04  04.41948  12 22 34.17   +00 44 42.1   25.1g 17DO162   T09  C~89UX      
2016 06  05.330622 12 19 27.70   +01 03 07.2         17DO162   T09  C~83F2      
2016 06  05.356114 12 19 27.67   +01 03 07.3         17DO162   T09  C~83F2      
2017 01  23.62432  12 31 45.11   -00 11 26.6   24.4i 17DO162   T09  C~7zpm      
2017 01  23.63041  12 31 45.10   -00 11 26.1   24.6i 17DO162   T09  C~7zpm      
2017 01  23.63574  12 31 45.09   -00 11 25.9   24.8i 17DO162   T09  C~7zpm      
2017 01  23.64653  12 31 45.07   -00 11 25.9   24.4i 17DO162   T09  C~7zpm      
2017 01  23.65191  12 31 45.06   -00 11 25.9   24.7i 17DO162   T09  C~7zpm      
2017 01  28.60076  12 31 37.34   -00 10 09.5   24.2z 17DO162   T09  C~7zpm      
2017 01  28.60612  12 31 37.34   -00 10 09.5   24.3z 17DO162   T09  C~7zpm      
2017 01  28.61691  12 31 37.30   -00 10 09.3   24.0z 17DO162   T09  C~7zpm      
2017 01  28.62228  12 31 37.29   -00 10 09.1   24.3z 17DO162   T09  C~7zpm      
2017 01  28.64799  12 31 37.25   -00 10 08.8   24.3z 17DO162   T09  C~7zpm      
2017 02  23.53583  12 30 27.16   -00 00 37.7   25.0r 17DO162   T09  C~7zpm      
2017 02  23.57406  12 30 27.01   -00 00 36.5   25.2r 17DO162   T09  C~7zpm      
2017 02  23.64828  12 30 26.74   -00 00 34.5   24.9r 17DO162   T09  C~7zpm      

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     0.21       0.00     0.01
     2   0.0003     -8.96     0.12      -0.06    -0.06
     3   0.0053   -139.46    -0.06       1.01     0.08
     4   0.0054   -140.27    -0.10       0.99     0.06
     5   0.0055   -142.34    -0.15       0.86    -0.07
     6   0.0055   -143.50     0.07       0.90    -0.02
     7   0.0055   -143.99    -0.11       0.91    -0.02
     8   0.1750  -3149.90     0.04     -92.63     0.01
     9   0.1751  -3150.36    -0.01     -92.72     0.00
    10   0.8110   8783.57     0.17     184.81    -0.23
    11   0.8110   8783.23    -0.01     185.21     0.14
    12   0.8110   8783.01    -0.10     185.33     0.24
    13   0.8111   8782.74    -0.10     185.21     0.08
    14   0.8111   8782.60    -0.10     185.15    -0.01
    15   0.8246   8645.76     0.06     209.39     0.01
    16   0.8246   8645.76     0.23     209.39    -0.01
    17   0.8247   8645.13    -0.05     209.34    -0.11
    18   0.8247   8644.91    -0.10     209.46    -0.01
    19   0.8248   8644.24     0.06     209.50    -0.08
    20   0.8956   7450.80     0.16     316.95    -0.08
    21   0.8957   7448.26    -0.08     317.16     0.02
    22   0.8959   7443.74    -0.13     317.39     0.03

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.

17DO162    quality flag:2

Type:      CLASSICAL  SCATNEAR CLASSICAL

axisobj        43.697    44.419    43.527
ecceobj         0.088     0.168     0.042
incobj          5.461     5.459     5.463
qmin           39.461    34.284    41.232
qmax           48.659    55.520    46.504
amean          43.931    44.554    43.751
amin           43.581    44.047    43.393
amax           44.304    45.158    44.100
emean           0.083     0.207     0.037
emin            0.067     0.156     0.020
emax            0.099     0.230     0.055
imean           5.045     6.305     5.003
imin            4.368     4.267     4.401
imax            5.768     8.465     5.684
excite_mean     0.121     0.235     0.095
fracstop        1.000     1.000     1.000
cjmean          3.083     3.041     3.088

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       178.4     178.3     178.0
kozaiamp        180.0     180.0     180.0