Orbit Fit and Astrometric record for 16FX185

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: 16FX185   
# Created Tue Jun 17 01:10:55 2025
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     19 observations of     23
# Arc:   5.15y
# First observation: 2012/01/26
#  Last observation: 2017/03/23
# Chi-squared of fit:   236.18 DOF:     32 RMS:  0.62
# Min/Max residuals:    -1.25    1.88
# Exact a, adot, b, bdot, g, gdot:
  1.360573E-05  1.754887E-02 -1.502001E-05  5.021513E-04  1.934520E-02 -8.341647E-03
# Covariance matrix:
  2.9838E-11 -9.0822E-12  1.3326E-12 -3.6678E-13 -2.4946E-12 -2.7016E-11
 -9.0822E-12  2.7914E-12 -4.1848E-13  1.1255E-13  8.5141E-13  8.3102E-12
  1.3326E-12 -4.1848E-13  3.1766E-13 -4.8370E-14 -1.6702E-13 -1.2453E-12
 -3.6678E-13  1.1255E-13 -4.8370E-14  9.8995E-15  3.2697E-14  3.3583E-13
 -2.4946E-12  8.5141E-13 -1.6702E-13  3.2697E-14  6.5561E-13  2.5098E-12
 -2.7016E-11  8.3102E-12 -1.2453E-12  3.3583E-13  2.5098E-12  2.4790E-11
#      lat0       lon0       xBary       yBary       zBary        JD0
    9.786618 -155.502157    0.965088    0.033747   -0.195603  2455953.157782
# Heliocentric elements and errors
Epoch:              2455952.5000  =  2012/01/26
Mean Anomaly:          331.43160 +/-     0.016
Argument of Peri:      163.25485 +/-     0.021
Long of Asc Node:      124.02452 +/-     0.001
Inclination:             9.91357 +/-     0.000
Eccentricity:         0.53056001 +/-    0.0003
Semi-Major Axis:     76.42447372 +/-    0.0282
Time of Perihelion: 2475318.0785 +/-     124.9
Perihelion:          35.87670450 +/-    0.0249
Aphelion:           116.97224294 +/-    0.0480
Period (y)              668.1237 +/-      0.37
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -46.93186434 +/-    0.0019
Ecliptic Y          -20.32613668 +/-    0.0010
Ecliptic Z            8.78587037 +/-    0.0004
Ecliptic XDOT         0.00209501 +/-    0.0000
Ecliptic YDOT        -0.00176819 +/-    0.0000
Ecliptic ZDOT        -0.00013055 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   51.89394066 +/-    0.0017
Geocenter to KBO     51.69277561 +/-    0.0022
# Hcoef:  6.28

The following table shows the complete astrometric record for 16FX185. 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 (16FX185) followed by the observatory code and reference code for the source of the astrometry.

2012 01  26.657016 13 45 03.69   -00 22 39.0         16FX185   T14  C~8Djz      
2012 01  26.659834 13 45 03.70   -00 22 39.0         16FX185   T14  C~8Djz      
2012 01  26.662575 13 45 03.69   -00 22 39.0         16FX185   T14  C~8Djz      
2016 03  07.58831  13 59 59.99   -01 34 08.8   23.3g 16FX185   T09  C~89TP      
2016 03  07.62208  13 59 59.92   -01 34 08.0   23.9g 16FX185   T09  C~89TP      
2016 03  07.63555  13 59 59.88   -01 34 07.6   24.1g 16FX185   T09  C~89TP      
2016 03  16.45267  13 59 35.84   -01 30 38.9   22.8z 16FX185   T09  C~89TP      
2016 03  16.45608  13 59 35.84   -01 30 38.9   23.0z 16FX185   T09  C~89TP      
2016 03  16.48283  13 59 35.76   -01 30 38.0   22.8z 16FX185   T09  C~89TP      
2016 03  16.53534  13 59 35.59   -01 30 37.0   23.4z 16FX185   T09  C~89TP      
2016 03  16.55995  13 59 35.54   -01 30 36.5   23.4z 16FX185   T09  C~89TP      
2016 03  16.58177  13 59 35.46   -01 30 35.8   23.4z 16FX185   T09  C~89TP      
2016 04  15.46627  13 57 51.61   -01 18 42.1   22.3y 16FX185   T09  C~89TP      
2016 04  15.49615  13 57 51.49   -01 18 41.6   22.8y 16FX185   T09  C~89TP      
2016 04  15.52858  13 57 51.37   -01 18 40.7   22.9y 16FX185   T09  C~89TP      
2016 04  15.53670  13 57 51.34   -01 18 40.4   23.4y 16FX185   T09  C~89TP      
2016 06  08.254890 13 54 49.58   -01 05 54.8         16FX185   T09  C~8COS      
2016 06  08.362536 13 54 49.31   -01 05 54.5         16FX185   T09  C~8COS      
2017 03  23.345591 14 03 25.46   -01 50 01.3         16FX185   W84  C~8Djz      
2017 03  26.337226 14 03 15.64   -01 48 48.4         16FX185   W84  C~8Djz      
2025 04  23.377100 14 37 43.154  -04 46 18.61  22.8G 16FX185   G37  C~8svQ      
2025 04  23.412770 14 37 43.009  -04 46 17.95        16FX185   G37  C~8svQ      
2025 04  23.456250 14 37 42.825  -04 46 16.87        16FX185   G37  C~8svQ      

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 (   1.29)      0.00 (   2.91)
     2   0.0000      0.00 (   1.44)      0.00 (   2.88)
     3   0.0000      0.00 (   1.29)      0.00 (   2.84)
     4   4.1121      0.00    -0.70       0.00    -0.54
     5   4.1122      0.00    -0.45       0.00    -0.53
     6   4.1122      0.00    -0.54       0.00    -0.44
     7   4.1363      0.00    -0.69       0.00    -0.51
     8   4.1363      0.00    -0.54       0.00    -0.59
     9   4.1364      0.00    -0.53       0.00    -0.34
    10   4.1366      0.00    -0.70       0.00    -0.60
    11   4.1366      0.00    -0.33       0.00    -0.70
    12   4.1367      0.00    -0.54       0.00    -0.52
    13   4.2185      0.00    -0.55       0.00    -0.45
    14   4.2186      0.00    -0.62       0.00    -0.62
    15   4.2187      0.00    -0.54       0.00    -0.45
    16   4.2187      0.00    -0.52       0.00    -0.33
    17   4.3658      0.00    -0.36       0.00    -0.56
    18   4.3661      0.00    -0.45       0.00    -0.65
    19   5.1545      0.00 (   1.96)      0.00 (  -1.26)
    20   5.1627      0.00     1.88       0.00    -1.25
    21  13.2395      0.00     0.28       0.00     1.10
    22  13.2396      0.00     0.34       0.00     0.99
    23  13.2397      0.00     0.29       0.00     1.13

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.

16FX185    quality flag:3

Type:       SCATNEAR  SCATNEAR  SCATNEAR

axisobj        76.152    76.151    76.153
ecceobj         0.530     0.530     0.530
incobj          9.915     9.915     9.915
qmin           35.132    34.952    35.093
qmax          124.349   126.138   123.158
amean          77.868    77.976    77.065
amin           75.844    75.546    75.568
amax           80.181    80.962    79.606
emean           0.537     0.540     0.533
emin            0.523     0.523     0.520
emax            0.551     0.558     0.547
imean           8.229     7.841     8.141
imin            7.480     7.068     7.517
imax            8.745     8.558     8.904
excite_mean     0.556     0.557     0.551
fracstop        1.000     1.000     1.000
cjmean          3.071     3.071     3.071

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       195.6     190.3     190.3
kozaiamp        180.0     180.0     180.0