Orbit Fit and Astrometric record for 14UE241

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: 14UE241   
# Created Fri May  3 01:16:39 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     51 observations of     51
# Arc:   6.15y
# First observation: 2013/09/02
#  Last observation: 2019/10/27
# Chi-squared of fit:    14.47 DOF:     96 RMS:  0.09
# Min/Max residuals:    -0.20    0.38
# Exact a, adot, b, bdot, g, gdot:
  1.397675E-05  2.011276E-02  2.047726E-06  1.704712E-03  2.248199E-02 -1.880238E-03
# Covariance matrix:
  2.2308E-13 -1.0207E-13  5.6337E-15 -6.4792E-15  5.8938E-14 -6.6830E-13
 -1.0207E-13  9.6341E-14 -7.4322E-15  8.1671E-15  2.1218E-14  8.3455E-13
  5.6337E-15 -7.4322E-15  1.0719E-13 -2.8436E-14 -2.9271E-15 -7.2402E-14
 -6.4792E-15  8.1671E-15 -2.8436E-14  1.0614E-14  2.7938E-15  7.9294E-14
  5.8938E-14  2.1218E-14 -2.9271E-15  2.7938E-15  1.1831E-13  2.7636E-13
 -6.6830E-13  8.3455E-13 -7.2402E-14  7.9294E-14  2.7636E-13  8.0968E-12
#      lat0       lon0       xBary       yBary       zBary        JD0
   -5.904153   10.810644    0.521347   -0.088895   -0.860511  2456537.865838
# Heliocentric elements and errors
Epoch:              2456538.5000  =  2013/09/03
Mean Anomaly:          244.38172 +/-     0.039
Argument of Peri:       77.03654 +/-     0.034
Long of Asc Node:       60.48770 +/-     0.002
Inclination:             7.50556 +/-     0.000
Eccentricity:         0.12482715 +/-    0.0001
Semi-Major Axis:     42.55227881 +/-    0.0024
Time of Perihelion: 2489100.1689 +/-      12.4
Perihelion:          37.24059894 +/-    0.0054
Aphelion:            47.86395867 +/-    0.0056
Period (y)              277.5827 +/-      0.02
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           44.40604863 +/-    0.0007
Ecliptic Y            7.95184914 +/-    0.0001
Ecliptic Z           -4.57535061 +/-    0.0001
Ecliptic XDOT        -0.00066833 +/-    0.0000
Ecliptic YDOT         0.00236605 +/-    0.0000
Ecliptic ZDOT         0.00023019 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   45.34389702 +/-    0.0007
Geocenter to KBO     44.48013887 +/-    0.0007
# Hcoef:  6.45

The following table shows the complete astrometric record for 14UE241. 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 (14UE241) followed by the observatory code and reference code for the source of the astrometry.

2013 09  02.36506  00 48 59.384  -01 09 19.33  23.7g 14UE241   W84  C~4yUy      
2013 09  12.34858  00 48 23.088  -01 13 37.47  23.7g 14UE241   W84  C~4yUy      
2013 10  03.10649  00 46 58.363  -01 22 47.54  24.2g 14UE241   W84  C~4yUy      
2013 10  04.15595  00 46 53.923  -01 23 14.63  24.2g 14UE241   W84  C~4yUy      
2013 10  04.15595  00 46 53.92   -01 23 14.6   24.2g 14UE241   W84  C~3coO      
2013 10  11.22093  00 46 23.957  -01 26 12.90  24.2g 14UE241   W84  C~4yUy      
2014 10  28.20419  00 49 21.358  -01 00 01.75  22.5i 14UE241   W84  C~4yUy      
2014 10  28.20419  00 49 21.36   -01 00 01.8   22.5i 14UE241   W84  C~3coO      
2014 11  13.12828  00 48 24.030  -01 04 34.93  23.4r 14UE241   W84  C~4yUy      
2014 11  13.12828  00 48 24.03   -01 04 34.9   23.6r 14UE241   W84  C~3coO      
2014 11  14.08300  00 48 20.970  -01 04 47.96  22.9i 14UE241   W84  C~4yUy      
2014 11  14.08300  00 48 20.97   -01 04 48.0   22.8i 14UE241   W84  C~3coO      
2014 11  17.07321  00 48 11.711  -01 05 25.71  22.5i 14UE241   W84  C~4yUy      
2014 11  17.07321  00 48 11.71   -01 05 25.7   22.5i 14UE241   W84  C~3coO      
2014 11  17.07457  00 48 11.708  -01 05 25.86  22.1z 14UE241   W84  C~4yUy      
2014 11  17.07457  00 48 11.71   -01 05 25.9   22.4z 14UE241   W84  C~3coO      
2014 11  18.12122  00 48 08.592  -01 05 38.12  22.4z 14UE241   W84  C~4yUy      
2014 11  18.12122  00 48 08.59   -01 05 38.1   22.5z 14UE241   W84  C~3coO      
2016 08  26.32136  01 01 39.985  +00 31 02.81  22.9i 14UE241   W84  C~4yUy      
2016 08  26.32136  01 01 39.98   +00 31 02.8   23.0i 14UE241   W84  C~3coO      
2016 08  26.32273  01 01 39.982  +00 31 02.89  23.3r 14UE241   W84  C~4yUy      
2016 08  26.32273  01 01 39.98   +00 31 02.9   24.0r 14UE241   W84  C~3coO      
2016 08  26.32411  01 01 39.973  +00 31 02.87  22.9z 14UE241   W84  C~4yUy      
2016 08  30.353507 01 01 27.80   +00 29 30.1   23.7g 14UE241   W84  C~352R      
2016 08  30.35404  01 01 27.806  +00 29 29.95  23.9g 14UE241   W84  C~4yUy      
2016 08  30.41875  01 01 27.57   +00 29 28.3   22.0z 14UE241   W84  C~3coO      
2016 11  05.17275  00 57 02.337  +00 02 30.08  23.5r 14UE241   W84  C~4yUy      
2016 11  05.17275  00 57 02.34   +00 02 30.1   23.6r 14UE241   W84  C~3coO      
2016 11  06.19836  00 56 58.542  +00 02 11.84  22.5i 14UE241   W84  C~4yUy      
2016 11  06.19836  00 56 58.54   +00 02 11.8   22.6i 14UE241   W84  C~3coO      
2016 11  06.19973  00 56 58.543  +00 02 11.88  23.2g 14UE241   W84  C~4yUy      
2016 11  18.13386  00 56 18.206  -00 00 47.06  22.3z 14UE241   W84  C~4yUy      
2016 11  18.13386  00 56 18.21   -00 00 47.0   22.3z 14UE241   W84  C~3coO      
2017 08  22.336424 01 05 59.42   +01 05 19.3   23.0r 14UE241   W84  C~352R      
2017 08  22.33695  01 05 59.419  +01 05 19.26  22.9r 14UE241   W84  C~4yUy      
2017 08  22.337789 01 05 59.42   +01 05 19.3   22.4i 14UE241   W84  C~352R      
2017 08  22.33832  01 05 59.420  +01 05 19.29  22.3i 14UE241   W84  C~4yUy      
2017 08  22.339167 01 05 59.42   +01 05 19.3   23.7g 14UE241   W84  C~352R      
2017 08  22.33969  01 05 59.417  +01 05 19.27  23.4g 14UE241   W84  C~4yUy      
2017 09  18.286782 01 04 29.76   +00 54 34.1   22.8r 14UE241   W84  C~352R      
2017 09  18.28731  01 04 29.766  +00 54 34.13  22.7r 14UE241   W84  C~4yUy      
2017 09  18.288171 01 04 29.75   +00 54 34.0   22.7i 14UE241   W84  C~352R      
2017 09  18.28870  01 04 29.757  +00 54 34.03  22.8i 14UE241   W84  C~4yUy      
2017 09  18.29007  01 04 29.747  +00 54 33.90  23.9g 14UE241   W84  C~4yUy      
2017 09  24.292037 01 04 05.63   +00 51 56.9   22.4z 14UE241   W84  C~352R      
2017 09  24.29256  01 04 05.633  +00 51 56.78  21.8z 14UE241   W84  C~4yUy      
2018 10  18.20738  01 06 35.284  +01 14 56.35  22.0z 14UE241   W84  C~4yUy      
2019 10  27.37241  01 10 09.18   +01 44 42.6   22.5i 14UE241   T09  C~7bK3      
2019 10  27.39969  01 10 09.05   +01 44 42.4   22.4i 14UE241   T09  C~7bK3      
2019 10  27.40237  01 10 09.05   +01 44 42.2   22.5i 14UE241   T09  C~7bK3      
2019 10  27.52034  01 10 08.55   +01 44 39.5   22.4i 14UE241   T09  C~7bK3      

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     0.10       0.00    -0.15
     2   0.0273      0.00    -0.10       0.00    -0.08
     3   0.0842      0.00    -0.01       0.00     0.03
     4   0.0870      0.00     0.14       0.00     0.09
     5   0.0870      0.00     0.18       0.00     0.06
     6   0.1064      0.00    -0.14       0.00    -0.17
     7   1.1522      0.00    -0.07       0.00     0.04
     8   1.1522      0.00    -0.04       0.00    -0.01
     9   1.1958      0.00     0.05       0.00     0.06
    10   1.1958      0.00     0.05       0.00     0.03
    11   1.1984      0.00    -0.01       0.00    -0.07
    12   1.1984      0.00    -0.01       0.00    -0.03
    13   1.2066      0.00    -0.09       0.00     0.12
    14   1.2066      0.00    -0.08       0.00     0.11
    15   1.2066      0.00    -0.06       0.00    -0.02
    16   1.2066      0.00    -0.03       0.00    -0.06
    17   1.2095      0.00    -0.01       0.00    -0.00
    18   1.2095      0.00     0.02       0.00    -0.02
    19   2.9814      0.00    -0.04       0.00    -0.01
    20   2.9814      0.00     0.04       0.00     0.00
    21   2.9814      0.00     0.02       0.00     0.13
    22   2.9814      0.00     0.05       0.00     0.12
    23   2.9814      0.00    -0.02       0.00     0.13
    24   2.9924      0.00     0.26       0.00     0.12
    25   2.9924      0.00     0.38       0.00    -0.02
    26   2.9926      0.00    -0.05       0.00    -0.15
    27   3.1754      0.00     0.14       0.00     0.08
    28   3.1754      0.00     0.10       0.00     0.06
    29   3.1782      0.00    -0.07       0.00    -0.05
    30   3.1782      0.00    -0.04       0.00    -0.01
    31   3.1782      0.00     0.05       0.00     0.05
    32   3.2109      0.00     0.00       0.00     0.14
    33   3.2109      0.00    -0.06       0.00     0.08
    34   3.9698      0.00    -0.08       0.00    -0.07
    35   3.9698      0.00    -0.07       0.00    -0.10
    36   3.9698      0.00    -0.02       0.00    -0.04
    37   3.9698      0.00    -0.00       0.00    -0.04
    38   3.9698      0.00     0.03       0.00    -0.02
    39   3.9698      0.00     0.01       0.00    -0.03
    40   4.0436      0.00    -0.08       0.00    -0.02
    41   4.0436      0.00     0.04       0.00     0.02
    42   4.0436      0.00    -0.14       0.00    -0.08
    43   4.0436      0.00    -0.01       0.00    -0.04
    44   4.0436      0.00    -0.07       0.00    -0.14
    45   4.0600      0.00    -0.12       0.00     0.07
    46   4.0600      0.00    -0.05       0.00    -0.04
    47   5.1248      0.00    -0.14       0.00     0.03
    48   6.1492      0.00     0.15       0.00    -0.20
    49   6.1493      0.00    -0.06       0.00     0.20
    50   6.1493      0.00     0.11       0.00     0.06
    51   6.1496      0.00     0.10       0.00    -0.04

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.

14UE241    quality flag:2

Type:       SCATNEAR CLASSICAL CLASSICAL

axisobj        42.760    42.760    42.760
ecceobj         0.120     0.120     0.120
incobj          7.502     7.502     7.502
qmin           35.664    35.653    35.614
qmax           49.748    49.818    49.868
amean          42.540    42.540    42.540
amin           42.092    42.154    42.146
amax           42.965    42.946    42.967
emean           0.113     0.113     0.113
emin            0.078     0.078     0.079
emax            0.160     0.160     0.161
imean           5.568     5.567     5.569
imin            3.893     3.894     3.891
imax            6.905     6.899     6.906
excite_mean     0.150     0.149     0.150
fracstop        1.000     1.000     1.000
cjmean          3.056     3.056     3.056

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       180.3     180.0     180.2
kozaiamp        180.0     180.0     179.9