Orbit Fit and Astrometric record for 15KG465

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: 15KG465   
# Created Sun Oct 19 01:11:02 2025
# Orbit generated from Bernstein formalism
# Fitting     22 observations of     22
# Arc:  61.91d
# First observation: 2015/03/22
#  Last observation: 2015/05/23
Preliminary a, adot, b, bdot, g, gdot:
  -0.000000   0.037529  -0.000001   0.007717   0.028727   0.000000
# Chi-squared of fit:     9.62 DOF:     38 RMS:  0.12
# Min/Max residuals:    -0.39    0.24
# Exact a, adot, b, bdot, g, gdot:
  1.968073E-05  3.421515E-02  4.427989E-06  7.753369E-03  2.806390E-02 -1.012896E-02
# Covariance matrix:
  2.7078E-13  2.4622E-11 -1.1082E-14 -3.2468E-13  5.1675E-12  2.1425E-10
  2.4622E-11  1.0814E-07 -3.6184E-11 -2.7788E-09  1.7689E-08 -1.1432E-07
 -1.1082E-14 -3.6184E-11  2.6257E-13 -6.9361E-13 -6.0619E-12 -8.1049E-13
 -3.2468E-13 -2.7788E-09 -6.9361E-13  9.3225E-11 -4.3315E-10  8.8081E-09
  5.1675E-12  1.7689E-08 -6.0619E-12 -4.3315E-10  2.9481E-09 -3.8186E-09
  2.1425E-10 -1.1432E-07 -8.1049E-13  8.8081E-09 -3.8186E-09  4.1980E-06
#      lat0       lon0       xBary       yBary       zBary        JD0
   12.510415 -143.801485    0.566676    0.176827   -0.796396  2457104.051198
# Heliocentric elements and errors
Epoch:              2457100.5000  =  2015/03/19
Mean Anomaly:          350.64338 +/-     1.902
Argument of Peri:       89.46270 +/-     5.562
Long of Asc Node:      172.54284 +/-     0.305
Inclination:            17.71279 +/-     0.096
Eccentricity:         0.61241248 +/-    0.0622
Semi-Major Axis:     83.40376478 +/-   10.4638
Time of Perihelion: 2464331.4198 +/-     555.0
Perihelion:          32.32625847 +/-    6.5869
Aphelion:           134.48127109 +/-   17.6522
Period (y)              761.7048 +/-    143.34
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -29.06788735 +/-    0.0543
Ecliptic Y          -20.56925934 +/-    0.0397
Ecliptic Z            7.71889200 +/-    0.0149
Ecliptic XDOT         0.00287867 +/-    0.0002
Ecliptic YDOT        -0.00203294 +/-    0.0001
Ecliptic ZDOT         0.00052448 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   36.43648994 +/-    0.0489
Geocenter to KBO     35.63296702 +/-    0.0689
# Hcoef:  7.69

The following table shows the complete astrometric record for 15KG465. 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 (15KG465) followed by the observatory code and reference code for the source of the astrometry.

2015 03  22.55042  14 31 56.12   -01 45 12.9   23.0i 15KG465   T09  C~94qT      
2015 03  22.59857  14 31 55.95   -01 45 11.3   23.1i 15KG465   T09  C~94qT      
2015 03  22.61243  14 31 55.91   -01 45 10.6   23.1i 15KG465   T09  C~94qT      
2015 03  22.62345  14 31 55.86   -01 45 10.2   23.2i 15KG465   T09  C~94qT      
2015 03  22.62615  14 31 55.84   -01 45 10.2   23.2i 15KG465   T09  C~94qT      
2015 03  28.293480 14 31 34.687  -01 41 45.85  23.4r 15KG465   W84  C~98Nt      
2015 05  17.35118  14 27 39.08   -01 16 07.7   24.1g 15KG465   T09  C~94qT      
2015 05  17.36919  14 27 39.00   -01 16 07.3   24.3g 15KG465   T09  C~94qT      
2015 05  17.43321  14 27 38.68   -01 16 06.1   24.3g 15KG465   T09  C~94qT      
2015 05  17.43532  14 27 38.67   -01 16 06.0   24.9g 15KG465   T09  C~94qT      
2015 05  19.48967  14 27 29.08   -01 15 23.7   22.5y 15KG465   T09  C~94qT      
2015 05  19.50316  14 27 29.01   -01 15 23.7   22.7y 15KG465   T09  C~94qT      
2015 05  19.51464  14 27 28.96   -01 15 23.3   23.0y 15KG465   T09  C~94qT      
2015 05  19.52272  14 27 28.91   -01 15 23.2   23.4y 15KG465   T09  C~94qT      
2015 05  19.52882  14 27 28.90   -01 15 23.0   22.5y 15KG465   T09  C~94qT      
2015 05  19.53152  14 27 28.89   -01 15 22.7   22.8y 15KG465   T09  C~94qT      
2015 05  19.54227  14 27 28.81   -01 15 23.0   22.7y 15KG465   T09  C~94qT      
2015 05  23.40482  14 27 11.25   -01 14 09.5   22.9z 15KG465   T09  C~94qT      
2015 05  23.41833  14 27 11.18   -01 14 09.3   22.8z 15KG465   T09  C~94qT      
2015 05  23.42124  14 27 11.16   -01 14 09.2   22.8z 15KG465   T09  C~94qT      
2015 05  23.43904  14 27 11.09   -01 14 09.0   22.8z 15KG465   T09  C~94qT      
2015 05  23.45689  14 27 11.00   -01 14 08.5   22.9z 15KG465   T09  C~94qT      

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    -0.08       0.00    -0.01
     2   0.0001     -2.93     0.03       0.70    -0.11
     3   0.0002     -3.72     0.11       1.17     0.13
     4   0.0002     -4.56    -0.03       1.31     0.08
     5   0.0002     -4.84    -0.14       1.21    -0.06
     6   0.0157   -370.82     0.13      92.87    -0.01
     7   0.1528  -4211.25    -0.00     413.94     0.10
     8   0.1528  -4212.51     0.09     413.93     0.15
     9   0.1530  -4217.45    -0.04     413.53    -0.05
    10   0.1530  -4217.62    -0.06     413.57    -0.00
    11   0.1586  -4367.46     0.01     407.37     0.05
    12   0.1587  -4368.46     0.01     407.04    -0.23
    13   0.1587  -4369.30     0.01     407.17    -0.05
    14   0.1587  -4370.04    -0.14     407.03    -0.17
    15   0.1587  -4370.25     0.10     407.17    -0.01
    16   0.1587  -4370.49     0.06     407.40     0.24
    17   0.1588  -4371.53    -0.20     406.73    -0.39
    18   0.1693  -4644.64     0.14     391.63     0.12
    19   0.1694  -4645.70     0.03     391.48     0.04
    20   0.1694  -4646.02    -0.08     391.48     0.05
    21   0.1694  -4647.07     0.12     391.33    -0.00
    22   0.1695  -4648.51    -0.06     391.37     0.13

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.

15KG465    quality flag:0

Type:      ERR2LARGE ERR2LARGE ERR2LARGE

axisobj         0.000     0.000     0.000
ecceobj        -1.000    -1.000    -1.000
incobj         -1.000    -1.000    -1.000
qmin            0.000     0.000     0.000
qmax            0.000     0.000     0.000
amean           0.000     0.000     0.000
amin            0.000     0.000     0.000
amax            0.000     0.000     0.000
emean           0.000     0.000     0.000
emin            0.000     0.000     0.000
emax            0.000     0.000     0.000
imean           0.000     0.000     0.000
imin            0.000     0.000     0.000
imax            0.000     0.000     0.000
excite_mean     0.000     0.000     0.000
fracstop        0.000     0.000     0.000
cjmean          0.000     0.000     0.000

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         0.0       0.0       0.0
kozaiamp          0.0       0.0       0.0