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 Wed Mar 26 01:10:48 2025
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     22 observations of     22
# Arc:  11.94y
# First observation: 2013/03/16
#  Last observation: 2025/02/23
# Chi-squared of fit:    38.75 DOF:     38 RMS:  0.23
# Min/Max residuals:    -0.64    0.52
# Exact a, adot, b, bdot, g, gdot:
  1.530911E-05  2.532073E-02 -6.478180E-06 -1.087961E-02  2.627674E-02 -2.952706E-03
# Covariance matrix:
  4.7264E-13 -1.1278E-13 -4.0473E-14  2.4108E-14  6.1633E-13 -1.6340E-13
 -1.1278E-13  6.0934E-14  2.6755E-14 -2.1115E-14 -7.3601E-14  1.4886E-13
 -4.0473E-14  2.6755E-14  1.4867E-13 -2.8817E-14 -2.0280E-14  7.5286E-14
  2.4108E-14 -2.1115E-14 -2.8817E-14  1.4845E-14 -5.9819E-15 -6.3567E-14
  6.1633E-13 -7.3601E-14 -2.0280E-14 -5.9819E-15  1.4733E-12  6.0573E-14
 -1.6340E-13  1.4886E-13  7.5286E-14 -6.3567E-14  6.0573E-14  4.5161E-13
#      lat0       lon0       xBary       yBary       zBary        JD0
   -5.894923  168.936895   -0.115962   -0.101457   -0.983438  2456367.598908
# Heliocentric elements and errors
Epoch:              2456368.5000  =  2013/03/17
Mean Anomaly:          320.22639 +/-     0.035
Argument of Peri:      246.15932 +/-     0.046
Long of Asc Node:      335.95267 +/-     0.000
Inclination:            23.85758 +/-     0.000
Eccentricity:         0.14299823 +/-    0.0001
Semi-Major Axis:     43.37716348 +/-    0.0095
Time of Perihelion: 2467897.2608 +/-      32.1
Perihelion:          37.17430569 +/-    0.0094
Aphelion:            49.58002127 +/-    0.0118
Period (y)              285.6932 +/-      0.09
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -38.14353705 +/-    0.0017
Ecliptic Y            7.34189663 +/-    0.0004
Ecliptic Z           -3.90884253 +/-    0.0002
Ecliptic XDOT        -0.00009792 +/-    0.0000
Ecliptic YDOT        -0.00266968 +/-    0.0000
Ecliptic ZDOT        -0.00109585 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   39.03994093 +/-    0.0017
Geocenter to KBO     38.05656860 +/-    0.0018
# Hcoef:  7.26

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      
2025 02  23.406800 12 07 16.922  -15 06 59.58  23.2G 16FU58    G37  C~8ie2      
2025 02  23.454440 12 07 16.706  -15 06 58.73        16FU58    G37  C~8ie2      

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    -0.02       0.00    -0.01
     2   0.0002      0.00    -0.02       0.00    -0.11
     3   0.0004      0.00    -0.08       0.00    -0.04
     4   0.1448      0.00    -0.06       0.00    -0.11
     5   0.1448      0.00    -0.17       0.00    -0.02
     6   0.1476      0.00     0.07       0.00     0.02
     7   0.1476      0.00     0.06       0.00     0.05
     8   3.0334      0.00    -0.64       0.00     0.25
     9   3.0334      0.00     0.02       0.00    -0.14
    10   3.0334      0.00     0.52       0.00    -0.33
    11   3.0361      0.00    -0.25       0.00     0.24
    12   3.0361      0.00     0.11       0.00     0.05
    13   3.0361      0.00     0.46       0.00    -0.24
    14   3.0389      0.00    -0.43       0.00     0.21
    15   3.0389      0.00    -0.08       0.00     0.02
    16   3.0389      0.00     0.42       0.00    -0.08
    17   3.0444      0.00    -0.45       0.00     0.37
    18   3.0444      0.00     0.05       0.00     0.08
    19   3.0444      0.00     0.39       0.00    -0.11
    20   3.0692      0.00     0.07       0.00     0.01
    21  11.9434      0.00    -0.08       0.00    -0.22
    22  11.9435      0.00     0.02       0.00     0.14

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        43.217    43.216    43.217
ecceobj         0.140     0.140     0.140
incobj         23.912    23.912    23.912
qmin           36.581    36.586    36.567
qmax           50.512    50.473    50.475
amean          43.380    43.380    43.380
amin           43.026    43.024    43.031
amax           43.789    43.763    43.772
emean           0.138     0.138     0.138
emin            0.123     0.123     0.123
emax            0.154     0.154     0.154
imean          24.917    24.917    24.917
imin           24.461    24.460    24.466
imax           25.255    25.251    25.260
excite_mean     0.443     0.443     0.443
fracstop        1.000     1.000     1.000
cjmean          2.850     2.850     2.850

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       187.0     187.0     187.1
kozaiamp        180.0     180.0     180.0