Orbit Fit and Astrometric record for 17OQ146

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: 17OQ146   
# Created Tue May  7 01:17:28 2024
# Orbit generated from Bernstein formalism
# Fitting     20 observations of     20
# Arc:   1.13d
# First observation: 2017/07/23
#  Last observation: 2017/07/24
# WARNING Fitting with energy constraint
# WARNING and with gdot fixed = 0
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# Chi-squared of fit:    11.27 DOF:     36 RMS:  0.13
# Min/Max residuals:    -0.30    0.31
# Exact a, adot, b, bdot, g, gdot:
  1.628057E-05  2.388160E-02 -1.683809E-06 -1.102912E-03  2.446624E-02  0.000000E+00
# Covariance matrix:
  3.3577E-11  5.1566E-08 -2.6667E-14  4.8102E-11  8.6689E-09  0.0000E+00
  5.1566E-08  7.9454E-05 -4.1051E-11  7.4052E-08  1.3344E-05  0.0000E+00
 -2.6667E-14 -4.1051E-11  7.4129E-14 -6.6252E-12 -6.9001E-12  0.0000E+00
  4.8102E-11  7.4052E-08 -6.6252E-12  6.5675E-08  1.2447E-08  0.0000E+00
  8.6689E-09  1.3344E-05 -6.9001E-12  1.2447E-08  2.2431E-06  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  1.9272E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.185694  -42.948655    0.283111   -0.003073   -0.972407  2457957.948981
# Heliocentric elements and errors
Epoch:              2457950.5000  =  2017/07/16
Mean Anomaly:          340.09672 +/-   215.366
Argument of Peri:      204.26988 +/-   282.913
Long of Asc Node:      132.74175 +/-     1.755
Inclination:             2.65452 +/-     1.176
Eccentricity:         0.01199274 +/-    0.5701
Semi-Major Axis:     42.32430872 +/-   21.8444
Time of Perihelion: 2463510.8912 +/-  764168.8
Perihelion:          41.81672430 +/-   32.3725
Aphelion:            42.83189314 +/-   32.7241
Period (y)              275.3550 +/-    213.17
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           30.43385614 +/-    1.8312
Ecliptic Y          -28.72265722 +/-    1.7049
Ecliptic Z           -0.13247438 +/-    0.0081
Ecliptic XDOT         0.00182513 +/-    0.0013
Ecliptic YDOT         0.00195050 +/-    0.0012
Ecliptic ZDOT        -0.00012352 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   41.84767839 +/-    1.7728
Geocenter to KBO     40.87264084 +/-    2.5020
# Hcoef:  9.43

The following table shows the complete astrometric record for 17OQ146. 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 (17OQ146) followed by the observatory code and reference code for the source of the astrometry.

2017 07  23.44818  21 18 14.42   -15 54 07.6   26.1r 17OQ146   568  C~7gvM      
2017 07  23.45447  21 18 14.40   -15 54 07.9   25.2r 17OQ146   568  C~7gvM      
2017 07  23.46701  21 18 14.34   -15 54 08.2   25.4r 17OQ146   568  C~7gvM      
2017 07  23.47014  21 18 14.35   -15 54 08.2   25.7r 17OQ146   568  C~7gvM      
2017 07  23.47955  21 18 14.28   -15 54 08.4   26.0r 17OQ146   568  C~7gvM      
2017 07  23.49643  21 18 14.21   -15 54 09.1   25.5r 17OQ146   568  C~7gvM      
2017 07  23.50898  21 18 14.16   -15 54 09.1   26.0r 17OQ146   568  C~7gvM      
2017 07  23.52152  21 18 14.10   -15 54 09.3   25.5r 17OQ146   568  C~7gvM      
2017 07  23.52779  21 18 14.07   -15 54 09.3   25.7r 17OQ146   568  C~7gvM      
2017 07  23.55048  21 18 13.97   -15 54 09.9   25.1r 17OQ146   568  C~7gvM      
2017 07  23.56304  21 18 13.90   -15 54 10.1   26.2r 17OQ146   568  C~7gvM      
2017 07  23.58502  21 18 13.80   -15 54 10.8   25.6r 17OQ146   568  C~7gvM      
2017 07  23.59130  21 18 13.78   -15 54 10.8   25.8r 17OQ146   568  C~7gvM      
2017 07  23.59757  21 18 13.75   -15 54 10.9   25.5r 17OQ146   568  C~7gvM      
2017 07  23.60385  21 18 13.73   -15 54 10.9   25.2r 17OQ146   568  C~7gvM      
2017 07  23.61953  21 18 13.67   -15 54 11.4   24.9r 17OQ146   568  C~7gvM      
2017 07  24.34315  21 18 10.38   -15 54 26.8   25.2r 17OQ146   568  C~7gvM      
2017 07  24.48162  21 18 09.74   -15 54 30.2   25.1r 17OQ146   568  C~7gvM      
2017 07  24.52993  21 18 09.54   -15 54 31.0   25.6r 17OQ146   568  C~7gvM      
2017 07  24.57788  21 18 09.30   -15 54 31.9   25.6r 17OQ146   568  C~7gvM      

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    -0.17       0.00     0.20
     2   0.0000     -0.37    -0.10      -0.20     0.00
     3   0.0001     -1.28    -0.14      -0.22    -0.02
     4   0.0001     -1.14     0.21      -0.27    -0.06
     5   0.0001     -2.17    -0.15      -0.15     0.06
     6   0.0001     -3.34    -0.15      -0.51    -0.30
     7   0.0002     -4.03     0.04      -0.29    -0.07
     8   0.0002     -4.91     0.03      -0.22     0.00
     9   0.0002     -5.33     0.06      -0.09     0.13
    10   0.0003     -6.88     0.08      -0.23     0.00
    11   0.0003     -7.91    -0.07      -0.11     0.12
    12   0.0004     -9.49    -0.12      -0.34    -0.11
    13   0.0004     -9.77     0.04      -0.25    -0.02
    14   0.0004    -10.21     0.03      -0.22     0.02
    15   0.0004    -10.49     0.19      -0.13     0.11
    16   0.0005    -11.46     0.31      -0.35    -0.10
    17   0.0025    -61.36    -0.08      -0.66     0.18
    18   0.0028    -71.19    -0.20      -1.10    -0.20
    19   0.0030    -74.18     0.20      -0.99    -0.08
    20   0.0031    -77.75    -0.01      -0.80     0.12

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.

17OQ146    quality flag:0

Type:      ERR2LARGE ERR2LARGE ERR2LARGE

axisobj         0.000     0.000     0.000
ecceobj        -1.000    -1.000    -1.000
incobj         -1.000    -1.000    -1.000
qmin            0.000     0.000     0.000
qmax            0.000     0.000     0.000
amean           0.000     0.000     0.000
amin            0.000     0.000     0.000
amax            0.000     0.000     0.000
emean           0.000     0.000     0.000
emin            0.000     0.000     0.000
emax            0.000     0.000     0.000
imean           0.000     0.000     0.000
imin            0.000     0.000     0.000
imax            0.000     0.000     0.000
excite_mean     0.000     0.000     0.000
fracstop        0.000     0.000     0.000
cjmean          0.000     0.000     0.000

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         0.0       0.0       0.0
kozaiamp          0.0       0.0       0.0