Orbit Fit and Astrometric record for 16EH362

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: 16EH362   
# Created Tue Jan 21 02:10:51 2025
# Orbit generated from Bernstein formalism
# Fitting     20 observations of     20
# Arc:   4.20y
# First observation: 2015/01/21
#  Last observation: 2019/04/05
Preliminary a, adot, b, bdot, g, gdot:
   0.001435   0.025511   0.000051   0.000514   0.027749   0.000000
# Chi-squared of fit:     7.11 DOF:     34 RMS:  0.11
# Min/Max residuals:    -0.24    0.16
# Exact a, adot, b, bdot, g, gdot:
  1.476944E-05  2.824504E-02 -1.277218E-07  5.851291E-04  3.012586E-02  2.786921E-02
# Covariance matrix:
  9.3555E-13 -7.1538E-13  1.8234E-14 -1.7314E-14 -9.0993E-14 -6.2042E-12
 -7.1538E-13  1.4679E-12 -1.6112E-14  2.9018E-14  1.4126E-12  1.3680E-11
  1.8234E-14 -1.6112E-14  4.3169E-13 -1.7692E-13  2.2310E-15 -1.9463E-13
 -1.7314E-14  2.9018E-14 -1.7692E-13  8.9657E-14  2.0353E-14  3.0528E-13
 -9.0993E-14  1.4126E-12  2.2310E-15  2.0353E-14  2.1709E-12  1.2669E-11
 -6.2042E-12  1.3680E-11 -1.9463E-13  3.0528E-13  1.2669E-11  1.3821E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
   -8.476361  150.591063    0.486536   -0.125582   -0.843709  2457044.103451
# Heliocentric elements and errors
Epoch:              2457040.5000  =  2015/01/18
Mean Anomaly:           15.78720 +/-     0.026
Argument of Peri:      169.70759 +/-     0.009
Long of Asc Node:      233.89138 +/-     0.004
Inclination:             8.30621 +/-     0.000
Eccentricity:         0.78024297 +/-    0.0003
Semi-Major Axis:     68.18544338 +/-    0.0727
Time of Perihelion: 2448021.9147 +/-       2.6
Perihelion:          14.98423063 +/-    0.0244
Aphelion:           121.38665613 +/-    0.1307
Period (y)              563.0484 +/-      0.90
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -29.10807039 +/-    0.0014
Ecliptic Y           16.96458073 +/-    0.0008
Ecliptic Z           -4.89287066 +/-    0.0002
Ecliptic XDOT        -0.00345342 +/-    0.0000
Ecliptic YDOT        -0.00100756 +/-    0.0000
Ecliptic ZDOT        -0.00032064 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   34.04433792 +/-    0.0013
Geocenter to KBO     33.19407764 +/-    0.0016
# Hcoef:  9.46

The following table shows the complete astrometric record for 16EH362. 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 (16EH362) followed by the observatory code and reference code for the source of the astrometry.

2015 01  21.602673 09 58 39.19   +03 19 20.3         16EH362   T09  C~86tJ      
2016 03  04.426185 10 00 46.11   +03 08 11.9         16EH362   T09  C~86tJ      
2016 03  07.28113  10 00 30.91   +03 09 48.7   26.2g 16EH362   T09  C~89T1      
2016 03  07.28866  10 00 30.87   +03 09 48.9   25.6g 16EH362   T09  C~89T1      
2016 03  07.29878  10 00 30.81   +03 09 49.0   26.3g 16EH362   T09  C~89T1      
2016 03  09.299522 10 00 20.35   +03 10 57.2         16EH362   T09  C~86tK      
2017 03  04.31448  10 06 33.90   +02 37 53.4   24.0z 16EH362   T09  C~86tK      
2017 03  04.34002  10 06 33.75   +02 37 54.4   24.1z 16EH362   T09  C~86tK      
2017 03  04.47432  10 06 33.02   +02 37 58.6   24.5i 16EH362   T09  C~86tK      
2017 03  04.49602  10 06 32.91   +02 37 59.5   24.6i 16EH362   T09  C~86tK      
2017 03  06.529560 10 06 22.21   +02 39 07.1         16EH362   T09  C~86tK      
2017 03  22.38749  10 05 04.70   +02 47 59.7   25.2z 16EH362   T09  C~86tK      
2017 03  22.41317  10 05 04.57   +02 48 00.5   24.9z 16EH362   T09  C~86tK      
2017 03  22.43886  10 05 04.44   +02 48 01.4   24.5z 16EH362   T09  C~86tK      
2017 03  22.48627  10 05 04.24   +02 48 02.9   24.4z 16EH362   T09  C~86tK      
2017 03  29.289242 10 04 35.37   +02 51 45.4         16EH362   T09  C~86tK      
2017 03  29.303176 10 04 35.30   +02 51 45.5         16EH362   T09  C~86tK      
2018 01  17.494013 10 15 56.07   +01 49 17.2         16EH362   T09  C~86tK      
2019 04  05.337293 10 14 52.02   +01 58 50.2         16EH362   T09  C~86tK      
2019 04  05.378076 10 14 51.87   +01 58 51.5         16EH362   T09  C~86tK      

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     0.01       0.00     0.09
     2   1.1166   2014.66     0.12      33.45     0.11
     3   1.1244   1767.53    -0.07      45.09     0.12
     4   1.1244   1766.90    -0.05      45.07     0.07
     5   1.1244   1766.02    -0.04      44.85    -0.19
     6   1.1299   1595.41    -0.00      54.36    -0.04
     7   2.1156   7535.32     0.12     143.04     0.05
     8   2.1156   7532.86    -0.11     143.19     0.13
     9   2.1160   7521.13    -0.10     143.31    -0.16
    10   2.1161   7519.26    -0.06     143.58     0.05
    11   2.1216   7345.20     0.09     151.02    -0.20
    12   2.1651   6069.70     0.12     245.36     0.06
    13   2.1651   6067.59    -0.04     245.43    -0.05
    14   2.1652   6065.45    -0.24     245.60    -0.07
    15   2.1653   6062.12     0.00     245.96    -0.06
    16   2.1839   5578.79     0.15     303.81     0.16
    17   2.1840   5577.77     0.09     303.54    -0.23
    18   2.9894  16480.85     0.03     357.08     0.05
    19   4.2019  15374.21     0.00     558.00     0.04
    20   4.2020  15371.64    -0.02     558.44     0.09

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.

16EH362    quality flag:3

Type:       CENTAURR  CENTAURR  CENTAURR

axisobj        68.909    69.056    68.763
ecceobj         0.784     0.784     0.783
incobj          8.298     8.298     8.298
qmin           14.462    14.540    14.396
qmax          128.554   123.207   127.440
amean          65.192    66.612    67.145
amin           61.069    64.126    64.666
amax           71.704    69.056    71.180
emean           0.768     0.774     0.778
emin            0.745     0.763     0.767
emax            0.793     0.784     0.790
imean          10.794     9.942     9.863
imin            8.978     9.099     8.997
imax           13.553    11.792    11.622
excite_mean     0.791     0.794     0.797
fracstop        0.063     0.046     0.044
cjmean          2.314     2.308     2.299

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       224.3     208.2     208.4
kozaiamp         50.0      34.3      36.0