Orbit Fit and Astrometric record for 16GY367

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: 16GY367   
# Created Sun Dec 22 02:10:41 2024
# Orbit generated from Bernstein formalism
# Fitting     20 observations of     20
# Arc:   0.93y
# First observation: 2016/04/02
#  Last observation: 2017/03/06
Preliminary a, adot, b, bdot, g, gdot:
  -0.000008   0.029369   0.000007  -0.005341   0.026817   0.000000
# Chi-squared of fit:    13.93 DOF:     34 RMS:  0.15
# Min/Max residuals:    -0.41    0.26
# Exact a, adot, b, bdot, g, gdot:
  1.645447E-05  2.889008E-02 -3.133454E-06 -5.275863E-03  2.700217E-02 -9.557660E-04
# Covariance matrix:
  2.9688E-13  2.2764E-13  2.3694E-15 -9.0468E-14  2.1335E-13  1.6963E-11
  2.2764E-13  1.2041E-10  4.2024E-13 -1.9741E-11  5.7709E-11  3.8232E-09
  2.3694E-15  4.2024E-13  2.9048E-13 -4.0865E-13  1.9795E-13  1.3320E-11
 -9.0468E-14 -1.9741E-11 -4.0865E-13  3.7865E-12 -9.5375E-12 -6.3026E-10
  2.1335E-13  5.7709E-11  1.9795E-13 -9.5375E-12  2.8466E-11  1.8535E-09
  1.6963E-11  3.8232E-09  1.3320E-11 -6.3026E-10  1.8535E-09  1.2218E-07
#      lat0       lon0       xBary       yBary       zBary        JD0
  -13.542559  145.462348   -0.731157   -0.158093   -0.656977  2457480.831819
# Heliocentric elements and errors
Epoch:              2457480.5000  =  2016/04/02
Mean Anomaly:          354.45989 +/-     4.221
Argument of Peri:      240.85775 +/-     5.627
Long of Asc Node:      274.27960 +/-     0.014
Inclination:            16.62630 +/-     0.003
Eccentricity:         0.13619234 +/-    0.0020
Semi-Major Axis:     43.60146656 +/-    0.0453
Time of Perihelion: 2459098.8250 +/-    1232.9
Perihelion:          37.66328096 +/-    0.0969
Aphelion:            49.53965217 +/-    0.1025
Period (y)              287.9121 +/-      0.45
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -30.63400028 +/-    0.0059
Ecliptic Y           20.19084729 +/-    0.0040
Ecliptic Z           -8.67227231 +/-    0.0017
Ecliptic XDOT        -0.00147984 +/-    0.0000
Ecliptic YDOT        -0.00254441 +/-    0.0000
Ecliptic ZDOT        -0.00049737 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   37.70040576 +/-    0.0052
Geocenter to KBO     37.03406407 +/-    0.0073
# Hcoef:  9.48

The following table shows the complete astrometric record for 16GY367. 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 (16GY367) followed by the observatory code and reference code for the source of the astrometry.

2016 04  02.331030 09 32 50.91   +00 15 08.4         16GY367   T09  C~89Tb      
2016 04  04.244078 09 32 45.62   +00 16 03.3         16GY367   T09  C~89Tb      
2016 04  04.25331  09 32 45.58   +00 16 03.5   25.5g 16GY367   T09  C~8COT      
2016 04  04.25541  09 32 45.58   +00 16 03.7   25.2g 16GY367   T09  C~8COT      
2016 04  04.265999 09 32 45.56   +00 16 03.9         16GY367   T09  C~89Tb      
2016 12  25.449137 09 45 57.01   -01 05 29.6         16GY367   T09  C~89Tb      
2016 12  25.46448  09 45 56.94   -01 05 30.0   25.7r 16GY367   T09  C~8COT      
2016 12  25.47707  09 45 56.89   -01 05 29.7   26.5r 16GY367   T09  C~8COT      
2016 12  25.491694 09 45 56.87   -01 05 29.9         16GY367   T09  C~89Tb      
2017 01  28.41954  09 43 37.18   -01 02 58.4   25.3g 16GY367   T09  C~8COT      
2017 01  28.438146 09 43 37.10   -01 02 58.1         16GY367   T09  C~89Tb      
2017 01  28.452912 09 43 37.02   -01 02 57.9         16GY367   T09  C~89Tb      
2017 01  28.46760  09 43 36.91   -01 02 57.4   26.0g 16GY367   T09  C~8COT      
2017 03  04.39457  09 40 39.44   -00 49 26.4   24.8i 16GY367   T09  C~89Tb      
2017 03  04.39993  09 40 39.43   -00 49 26.3   25.1i 16GY367   T09  C~89Tb      
2017 03  04.40261  09 40 39.42   -00 49 26.1   24.8i 16GY367   T09  C~89Tb      
2017 03  04.41889  09 40 39.34   -00 49 25.6   24.5i 16GY367   T09  C~89Tb      
2017 03  04.42965  09 40 39.29   -00 49 25.8   24.9i 16GY367   T09  C~89Tb      
2017 03  04.43238  09 40 39.28   -00 49 25.3   24.8i 16GY367   T09  C~89Tb      
2017 03  06.416212 09 40 29.86   -00 48 27.3         16GY367   T09  C~89Tb      

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     0.10       0.00     0.01
     2   0.0052    -92.96     0.05      25.87     0.03
     3   0.0053    -93.59    -0.13      25.86    -0.10
     4   0.0053    -93.66    -0.09      26.05     0.06
     5   0.0053    -94.00     0.07      26.14     0.01
     6   0.7313  12741.38     0.22    -709.47     0.10
     7   0.7314  12740.52    -0.02    -710.20    -0.29
     8   0.7314  12739.71    -0.32    -710.16     0.01
     9   0.7314  12739.49     0.06    -710.45     0.04
    10   0.8243  10703.80     0.06   -1253.64    -0.04
    11   0.8244  10702.57     0.26   -1253.75     0.05
    12   0.8244  10701.37     0.19   -1253.96     0.00
    13   0.8245  10699.64    -0.41   -1254.02     0.09
    14   0.9201   7913.38    -0.27   -1359.00    -0.01
    15   0.9201   7913.21    -0.02   -1358.96     0.02
    16   0.9201   7913.00    -0.02   -1358.82     0.15
    17   0.9202   7911.70    -0.04   -1358.74     0.17
    18   0.9202   7911.06     0.17   -1359.17    -0.31
    19   0.9202   7910.75     0.08   -1358.75     0.11
    20   0.9256   7758.04     0.05   -1350.19    -0.10

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.

16GY367    quality flag:3

Type:       SCATEXTD  SCATEXTD  SCATEXTD

axisobj        43.364    43.458    43.337
ecceobj         0.130     0.135     0.130
incobj         16.606    16.616    16.603
qmin           37.081    36.811    37.078
qmax           49.855    50.349    49.904
amean          43.346    43.423    43.332
amin           43.000    43.069    42.984
amax           43.727    43.812    43.725
emean           0.128     0.134     0.127
emin            0.115     0.119     0.112
emax            0.142     0.150     0.142
imean          18.347    18.306    18.370
imin           17.834    17.761    17.874
imax           18.824    18.823    18.873
excite_mean     0.340     0.342     0.340
fracstop        1.000     1.000     1.000
cjmean          2.953     2.952     2.953

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       181.2     189.1     187.5
kozaiamp        180.0     180.0     180.0