Orbit Fit and Astrometric record for 16FU58

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: 16FU58    
# Created Fri Apr 26 01:17:49 2024
# Orbit generated from Bernstein formalism
# Fitting     16 observations of     20
# Arc:   3.07y
# First observation: 2013/03/16
#  Last observation: 2016/04/10
Preliminary a, adot, b, bdot, g, gdot:
   0.000018   0.025516   0.000015  -0.010990   0.026109   0.000000
# Chi-squared of fit:    13.17 DOF:     26 RMS:  0.16
# Min/Max residuals:    -0.43    0.33
# Exact a, adot, b, bdot, g, gdot:
  1.521791E-05  2.532699E-02 -6.475922E-06 -1.088260E-02  2.627825E-02 -2.860848E-03
# Covariance matrix:
  4.9185E-13  7.8462E-13  1.0273E-14 -4.1476E-13  8.5398E-13  1.2304E-11
  7.8462E-13  6.7793E-11  2.0480E-12 -3.1792E-11  1.8165E-11  9.3507E-10
  1.0273E-14  2.0480E-12  2.8751E-13 -1.0356E-12  5.1084E-13  2.8239E-11
 -4.1476E-13 -3.1792E-11 -1.0356E-12  1.4962E-11 -8.5511E-12 -4.3880E-10
  8.5398E-13  1.8165E-11  5.1084E-13 -8.5511E-12  6.3865E-12  2.5176E-10
  1.2304E-11  9.3507E-10  2.8239E-11 -4.3880E-10  2.5176E-10  1.2906E-08
#      lat0       lon0       xBary       yBary       zBary        JD0
   -5.894923  168.936895   -0.115962   -0.101457   -0.983438  2456367.598908
# Heliocentric elements and errors
Epoch:              2456360.5000  =  2013/03/09
Mean Anomaly:          320.83440 +/-     0.846
Argument of Peri:      245.13364 +/-     1.293
Long of Asc Node:      335.95346 +/-     0.001
Inclination:            23.85879 +/-     0.001
Eccentricity:         0.14039133 +/-    0.0032
Semi-Major Axis:     43.35594888 +/-    0.0279
Time of Perihelion: 2467704.6960 +/-     244.9
Perihelion:          37.26914969 +/-    0.1408
Aphelion:            49.44274806 +/-    0.1424
Period (y)              285.4837 +/-      0.28
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -38.14139893 +/-    0.0036
Ecliptic Y            7.34148214 +/-    0.0007
Ecliptic Z           -3.90861756 +/-    0.0004
Ecliptic XDOT        -0.00010735 +/-    0.0000
Ecliptic YDOT        -0.00266834 +/-    0.0000
Ecliptic ZDOT        -0.00109708 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   39.03768645 +/-    0.0035
Geocenter to KBO     38.05427918 +/-    0.0037
# Hcoef:  7.20

The following table shows the complete astrometric record for 16FU58. 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 (16FU58) followed by the observatory code and reference code for the source of the astrometry.

2013 03  16.09813  11 10 05.99   -01 02 55.6   23.0r 16FU58    W84  C~6hUh      
2013 03  16.16725  11 10 05.64   -01 02 53.9         16FU58    W84  C~6hUh      
2013 03  16.23751  11 10 05.28   -01 02 52.0         16FU58    W84  C~6hUh      
2013 05  07.978391 11 06 44.61   -00 42 48.2   22.9r 16FU58    W84  C~6hUh      
2013 05  07.999016 11 06 44.56   -00 42 47.8   23.0r 16FU58    W84  C~6hUh      
2013 05  09.003079 11 06 42.60   -00 42 33.1   22.9r 16FU58    W84  C~6hUh      
2013 05  09.007708 11 06 42.59   -00 42 33.0         16FU58    W84  C~6hUh      
2016 03  28.03411  11 22 22.50   -04 24 24.0   23.7V 16FU58    W84  C~1qoJ      
2016 03  28.04105  11 22 22.51   -04 24 24.2         16FU58    W84  C~1qoJ      
2016 03  28.04799  11 22 22.51   -04 24 24.2         16FU58    W84  C~1qoJ      
2016 03  29.03545  11 22 17.73   -04 23 56.4         16FU58    W84  C~1qoJ      
2016 03  29.04239  11 22 17.72   -04 23 56.4         16FU58    W84  C~1qoJ      
2016 03  29.04933  11 22 17.71   -04 23 56.5         16FU58    W84  C~1qoJ      
2016 03  30.05844  11 22 12.85   -04 23 28.2         16FU58    W84  C~1qoJ      
2016 03  30.06538  11 22 12.84   -04 23 28.2         16FU58    W84  C~1qoJ      
2016 03  30.07232  11 22 12.84   -04 23 28.1         16FU58    W84  C~1qoJ      
2016 04  01.06296  11 22 03.42   -04 22 32.7         16FU58    W84  C~1qoJ      
2016 04  01.06990  11 22 03.42   -04 22 32.8         16FU58    W84  C~1qoJ      
2016 04  01.07684  11 22 03.41   -04 22 32.8         16FU58    W84  C~1qoJ      
2016 04  10.125956 11 21 22.92   -04 18 25.1   23.5g 16FU58    W84  C~5bmN      

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    -0.01
     2   0.0002     -5.50     0.04      -0.48    -0.11
     3   0.0004    -11.21    -0.04      -0.84    -0.07
     4   0.1448  -3252.29     0.00     -68.13    -0.05
     5   0.1448  -3253.13    -0.13     -68.05    -0.01
     6   0.1476  -3285.95     0.07     -66.00     0.12
     7   0.1476  -3286.12     0.05     -65.97     0.15
     8   3.0334  14902.03    -0.43   -6850.27    -0.06
     9   3.0334  14902.25     0.33   -6850.40    -0.16
    10   3.0334  14902.25 (   0.87)  -6850.40 (  -0.14)
    11   3.0361  14825.14    -0.08   -6852.44     0.08
    12   3.0361  14825.00     0.32   -6852.50     0.04
    13   3.0361  14824.90 (   0.77)  -6852.65 (  -0.09)
    14   3.0389  14746.49    -0.25   -6854.69    -0.02
    15   3.0389  14746.35     0.15   -6854.75    -0.06
    16   3.0389  14746.31 (   0.64)  -6854.66 (   0.05)
    17   3.0444  14594.12    -0.36   -6858.12     0.13
    18   3.0444  14594.16     0.21   -6858.21     0.05
    19   3.0444  14594.02 (   0.60)  -6858.27 (   0.00)
    20   3.0692  13936.27     0.12   -6864.40    -0.01

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.

16FU58    quality flag:3

Type:       SCATEXTD  SCATEXTD  SCATEXTD

axisobj        43.198    43.251    43.154
ecceobj         0.138     0.145     0.132
incobj         23.913    23.909    23.916
qmin           36.669    36.390    36.841
qmax           50.323    50.706    50.000
amean          43.351    43.416    43.313
amin           42.979    43.052    42.969
amax           43.756    43.800    43.682
emean           0.135     0.142     0.131
emin            0.120     0.127     0.116
emax            0.151     0.158     0.145
imean          24.913    24.928    24.898
imin           24.459    24.468    24.457
imax           25.269    25.282    25.211
excite_mean     0.442     0.445     0.441
fracstop        1.000     1.000     1.000
cjmean          2.850     2.848     2.851

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       188.3     187.6     186.2
kozaiamp        179.9     180.0     180.0