Orbit Fit and Astrometric record for 16SD58

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: 16SD58    
# Created Mon Jul  7 01:11:20 2025
# Orbit generated from Bernstein formalism
# Fitting     20 observations of     20
# Arc:   0.97y
# First observation: 2015/10/10
#  Last observation: 2016/09/28
Preliminary a, adot, b, bdot, g, gdot:
  -0.000002   0.029696  -0.000000  -0.003955   0.028002   0.000000
# Chi-squared of fit:     5.37 DOF:     34 RMS:  0.09
# Min/Max residuals:    -0.22    0.24
# Exact a, adot, b, bdot, g, gdot:
  1.677064E-05  2.980094E-02 -2.018006E-06 -3.965255E-03  2.805060E-02  2.208800E-03
# Covariance matrix:
  2.9389E-13  1.6771E-11  6.9478E-14 -1.9353E-12  4.2707E-12  5.2532E-10
  1.6771E-11  5.9811E-09  2.4887E-11 -6.7450E-10  1.3329E-09  1.8357E-07
  6.9478E-14  2.4887E-11  2.0605E-13 -2.9316E-12  5.5438E-12  7.6386E-10
 -1.9353E-12 -6.7450E-10 -2.9316E-12  7.6620E-11 -1.5044E-10 -2.0705E-08
  4.2707E-12  1.3329E-09  5.5438E-12 -1.5044E-10  2.9886E-10  4.0938E-08
  5.2532E-10  1.8357E-07  7.6386E-10 -2.0705E-08  4.0938E-08  5.6350E-06
#      lat0       lon0       xBary       yBary       zBary        JD0
  -14.241846   28.091240    0.198744   -0.241551   -0.952373  2457306.018909
# Heliocentric elements and errors
Epoch:              2457300.5000  =  2015/10/05
Mean Anomaly:           40.60283 +/-    23.951
Argument of Peri:      193.19030 +/-    32.168
Long of Asc Node:      147.24748 +/-     0.075
Inclination:            15.82886 +/-     0.011
Eccentricity:         0.09372844 +/-    0.0658
Semi-Major Axis:     39.22781806 +/-    0.6347
Time of Perihelion: 2447179.0340 +/-    5965.3
Perihelion:          35.55105589 +/-    2.6444
Aphelion:            42.90458022 +/-    2.6728
Period (y)              245.6968 +/-      5.96
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           31.44010875 +/-    0.0188
Ecliptic Y           16.55776441 +/-    0.0100
Ecliptic Z           -8.77049538 +/-    0.0054
Ecliptic XDOT        -0.00127093 +/-    0.0002
Ecliptic YDOT         0.00261306 +/-    0.0001
Ecliptic ZDOT        -0.00042812 +/-    0.0001
# Distances at JD0 (AU)
Heliocenter to KBO   36.60002172 +/-    0.0168
Geocenter to KBO     35.64985709 +/-    0.0220
# Hcoef:  8.92

The following table shows the complete astrometric record for 16SD58. 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 (16SD58) followed by the observatory code and reference code for the source of the astrometry.

2015 10  10.51812  02 04 33.22   -02 31 53.1   24.5r 16SD58    T09  C~8vIL      
2015 10  10.54879  02 04 33.06   -02 31 54.1   24.5r 16SD58    T09  C~8vIL      
2015 10  10.60093  02 04 32.81   -02 31 55.9   24.2r 16SD58    T09  C~8vIL      
2015 10  14.51991  02 04 13.31   -02 34 09.9   25.2g 16SD58    T09  C~8eVS      
2015 10  14.55055  02 04 13.13   -02 34 11.3   25.2g 16SD58    T09  C~8eVS      
2015 10  14.57894  02 04 13.00   -02 34 12.3   25.4g 16SD58    T09  C~8eVS      
2015 10  14.60271  02 04 12.87   -02 34 12.8   25.2g 16SD58    T09  C~8eVS      
2015 11  06.46299  02 02 15.54   -02 45 15.7   24.3z 16SD58    T09  C~8eVS      
2015 11  06.50498  02 02 15.33   -02 45 16.8   24.5z 16SD58    T09  C~8eVS      
2015 11  06.52457  02 02 15.23   -02 45 17.3   24.0z 16SD58    T09  C~8eVS      
2015 11  10.39623  02 01 55.81   -02 46 43.4   24.6i 16SD58    T09  C~8eVS      
2015 11  10.40854  02 01 55.77   -02 46 43.8   24.2i 16SD58    T09  C~8eVS      
2015 11  10.41958  02 01 55.70   -02 46 44.0   24.2i 16SD58    T09  C~8eVS      
2015 11  10.44606  02 01 55.57   -02 46 44.6   24.0i 16SD58    T09  C~8eVS      
2015 11  10.45724  02 01 55.52   -02 46 44.8   24.3i 16SD58    T09  C~8eVS      
2015 11  10.46823  02 01 55.46   -02 46 45.0   24.0i 16SD58    T09  C~8eVS      
2016 09  27.52266  02 12 11.20   -02 01 25.4   25.1g 16SD58    568  C~2eAJ      
2016 09  27.58184  02 12 10.94   -02 01 27.6   24.7g 16SD58    568  C~2eAJ      
2016 09  28.47127  02 12 07.09   -02 02 00.3   24.9g 16SD58    568  C~2eAJ      
2016 09  28.59154  02 12 06.56   -02 02 04.6   25.0g 16SD58    568  C~2eAJ      

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    -0.04
     2   0.0001     -2.60    -0.06      -0.09     0.05
     3   0.0002     -6.74     0.09      -0.46     0.01
     4   0.0110   -327.39     0.24     -23.29     0.13
     5   0.0110   -330.41    -0.22     -23.66    -0.10
     6   0.0111   -332.59    -0.02     -23.91    -0.22
     7   0.0112   -334.59    -0.04     -23.69     0.11
     8   0.0738  -2213.54    -0.04     -27.31     0.07
     9   0.0739  -2216.88     0.01     -27.23    -0.07
    10   0.0739  -2218.45    -0.00     -27.18    -0.11
    11   0.0845  -2521.17    -0.13      -5.74     0.19
    12   0.0846  -2521.87     0.13      -5.90    -0.06
    13   0.0846  -2522.92    -0.06      -5.72     0.05
    14   0.0847  -2524.96    -0.02      -5.60    -0.01
    15   0.0847  -2525.73     0.08      -5.52    -0.01
    16   0.0847  -2526.64     0.03      -5.40     0.04
    17   0.9665   7071.16     0.00    -705.04    -0.02
    18   0.9666   7066.73     0.00    -705.73    -0.04
    19   0.9691   7001.12    -0.06    -715.99    -0.01
    20   0.9694   6992.16     0.06    -717.21     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.

16SD58    quality flag:1

Type:           3:2E   REMOVED CLASSICAL

axisobj        39.645    44.558    38.742
ecceobj         0.103     0.309     0.082
incobj         15.796    15.835    15.769
qmin           34.755    30.382    34.553
qmax           44.577    58.313    42.695
amean          39.459    44.023    38.476
amin           39.066    42.908    38.179
amax           39.901    44.689    38.814
emean           0.097     0.300     0.081
emin            0.076     0.283     0.060
emax            0.119     0.311     0.101
imean          14.910    14.720    12.712
imin           14.314    14.578     8.942
imax           15.626    14.931    17.732
excite_mean     0.275     0.393     0.235
fracstop        1.000     0.002     1.000
cjmean          2.965     2.920     2.979

libcent 0       179.7    -180.0    -180.0
libamp  0        88.1    -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       178.1     175.7     176.9
kozaiamp        180.0       3.3     180.0