Orbit Fit and Astrometric record for 16RU81

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: 16RU81    
# Created Tue Apr  1 01:10:51 2025
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting      8 observations of      8
# Arc:   5.01y
# First observation: 2013/09/11
#  Last observation: 2018/09/14
# Chi-squared of fit:     1.82 DOF:     10 RMS:  0.08
# Min/Max residuals:    -0.14    0.16
# Exact a, adot, b, bdot, g, gdot:
  1.546434E-05  2.388351E-02 -6.463141E-08  2.865368E-05  2.433978E-02 -1.158122E-03
# Covariance matrix:
  1.4515E-12 -7.8400E-13  9.8553E-16 -5.8301E-16 -3.9049E-13 -4.1980E-12
 -7.8400E-13  1.4543E-12 -1.0837E-14  8.1502E-16  1.9809E-12  1.1377E-11
  9.8553E-16 -1.0837E-14  1.1803E-12 -3.0930E-13 -2.3814E-14 -8.4858E-14
 -5.8301E-16  8.1502E-16 -3.0930E-13  9.5912E-14  3.3589E-16  7.4542E-15
 -3.9049E-13  1.9809E-12 -2.3814E-14  3.3589E-16  3.7517E-12  1.5955E-11
 -4.1980E-12  1.1377E-11 -8.4858E-14  7.4542E-15  1.5955E-11  9.5749E-11
#      lat0       lon0       xBary       yBary       zBary        JD0
   -3.638128   -2.538847    0.158972   -0.063032   -0.992879  2456546.783108
# Heliocentric elements and errors
Epoch:              2456546.5000  =  2013/09/11
Mean Anomaly:          300.21640 +/-     0.105
Argument of Peri:      336.94334 +/-     0.131
Long of Asc Node:       86.36671 +/-     0.012
Inclination:             3.55263 +/-     0.000
Eccentricity:         0.06111555 +/-    0.0004
Semi-Major Axis:     43.28284253 +/-    0.0120
Time of Perihelion: 2473818.8576 +/-      47.2
Perihelion:          40.63758765 +/-    0.0220
Aphelion:            45.92809741 +/-    0.0228
Period (y)              284.7619 +/-      0.12
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           41.94854411 +/-    0.0033
Ecliptic Y           -2.01604525 +/-    0.0001
Ecliptic Z           -2.60705774 +/-    0.0002
Ecliptic XDOT        -0.00001685 +/-    0.0000
Ecliptic YDOT         0.00268847 +/-    0.0000
Ecliptic ZDOT         0.00001162 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   42.07783804 +/-    0.0033
Geocenter to KBO     41.08506667 +/-    0.0033
# Hcoef:  7.49

The following table shows the complete astrometric record for 16RU81. 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 (16RU81) followed by the observatory code and reference code for the source of the astrometry.

2013 09  11.28233  23 56 28.736  -04 20 50.55  24.1g 16RU81    W84  C~52Zi      
2016 09  10.33646  00 11 37.403  -02 41 25.28  23.5i 16RU81    W84  C~52Zi      
2016 11  05.06437  00 07 47.213  -03 04 54.98  23.8i 16RU81    W84  C~52Zi      
2016 11  05.06575  00 07 47.214  -03 04 54.70  23.6r 16RU81    W84  C~52Zi      
2016 11  26.12241  00 06 56.134  -03 08 45.63  23.7r 16RU81    W84  C~52Zi      
2017 10  17.22970  00 13 59.390  -02 25 08.09  23.7i 16RU81    W84  C~52Zi      
2017 10  27.16027  00 13 20.077  -02 28 55.53  22.9z 16RU81    W84  C~52Zi      
2018 09  14.30686  00 21 28.211  -01 36 15.05  23.7r 16RU81    W84  C~52Zi      

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     0.00       0.00     0.02
     2   2.9981      0.00     0.05       0.00    -0.08
     3   3.1507      0.00    -0.09       0.00    -0.14
     4   3.1507      0.00    -0.01       0.00     0.16
     5   3.2083      0.00     0.01       0.00     0.07
     6   4.0984      0.00     0.03       0.00     0.06
     7   4.1256      0.00     0.11       0.00    -0.12
     8   5.0076      0.00    -0.06       0.00     0.06

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.

16RU81    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        43.520    43.519    43.520
ecceobj         0.063     0.063     0.063
incobj          3.554     3.554     3.554
qmin           39.144    39.165    39.144
qmax           47.770    47.815    47.767
amean          43.325    43.325    43.325
amin           42.980    42.980    42.984
amax           43.696    43.693    43.693
emean           0.074     0.074     0.074
emin            0.052     0.052     0.052
emax            0.094     0.094     0.094
imean           1.929     1.929     1.929
imin            0.812     0.812     0.812
imax            3.064     3.064     3.065
excite_mean     0.082     0.082     0.082
fracstop        1.000     1.000     1.000
cjmean          3.085     3.085     3.085

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       161.7     161.7     161.7
kozaiamp        179.9     180.0     180.0