Orbit Fit and Astrometric record for 14UP250

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: 14UP250   
# Created Sun Nov 24 02:10:05 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     37 observations of     37
# Arc:   5.79y
# First observation: 2014/10/28
#  Last observation: 2020/08/12
# Chi-squared of fit:    17.42 DOF:     68 RMS:  0.12
# Min/Max residuals:    -0.44    0.38
# Exact a, adot, b, bdot, g, gdot:
  1.219535E-05  1.645708E-02 -5.007735E-06 -6.176316E-03  2.049998E-02  6.589459E-03
# Covariance matrix:
  1.0596E-13 -5.7594E-14 -6.3474E-15  1.2311E-14 -2.1006E-14 -4.0658E-13
 -5.7594E-14  7.9630E-14  1.2181E-14 -2.3756E-14  1.5471E-14  7.8486E-13
 -6.3474E-15  1.2181E-14  9.0320E-14 -2.7888E-14  6.7012E-15  1.4453E-13
  1.2311E-14 -2.3756E-14 -2.7888E-14  2.0186E-14 -1.1930E-14 -2.8076E-13
 -2.1006E-14  1.5471E-14  6.7012E-15 -1.1930E-14  2.2256E-13  3.9183E-13
 -4.0658E-13  7.8486E-13  1.4453E-13 -2.8076E-13  3.9183E-13  9.2737E-12
#      lat0       lon0       xBary       yBary       zBary        JD0
    3.071166    3.261731   -0.513245    0.045859   -0.851380  2456958.663308
# Heliocentric elements and errors
Epoch:              2456958.5000  =  2014/10/28
Mean Anomaly:           61.59434 +/-     0.020
Argument of Peri:       67.76900 +/-     0.013
Long of Asc Node:      191.79193 +/-     0.000
Inclination:            20.90382 +/-     0.000
Eccentricity:         0.36229267 +/-    0.0002
Semi-Major Axis:     52.21293290 +/-    0.0085
Time of Perihelion: 2433380.6696 +/-       9.6
Perihelion:          33.29656991 +/-    0.0096
Aphelion:            71.12929588 +/-    0.0140
Period (y)              377.2900 +/-      0.09
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           49.45099868 +/-    0.0011
Ecliptic Y            3.33419088 +/-    0.0001
Ecliptic Z            2.61318691 +/-    0.0001
Ecliptic XDOT         0.00079200 +/-    0.0000
Ecliptic YDOT         0.00224203 +/-    0.0000
Ecliptic ZDOT        -0.00077643 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   49.63186253 +/-    0.0011
Geocenter to KBO     48.78031998 +/-    0.0011
# Hcoef:  6.06

The following table shows the complete astrometric record for 14UP250. 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 (14UP250) followed by the observatory code and reference code for the source of the astrometry.

2014 10  28.16253  00 07 04.907  +04 06 53.27  22.8r 14UP250   W84  C~4yUz      
2014 10  28.16253  00 07 04.91   +04 06 53.3   22.9r 14UP250   W84  C~3coQ      
2014 10  28.16391  00 07 04.899  +04 06 53.33  24.0g 14UP250   W84  C~4yUz      
2014 10  28.16809  00 07 04.886  +04 06 53.08  22.7i 14UP250   W84  C~4yUz      
2014 10  28.16809  00 07 04.89   +04 06 53.1   22.8i 14UP250   W84  C~3coQ      
2014 10  29.16670  00 07 01.829  +04 06 27.10  22.9r 14UP250   W84  C~4yUz      
2014 10  29.16670  00 07 01.83   +04 06 27.1   23.0r 14UP250   W84  C~3coQ      
2014 10  29.17083  00 07 01.814  +04 06 27.06  22.1i 14UP250   W84  C~4yUz      
2014 10  29.17083  00 07 01.81   +04 06 27.0   22.3i 14UP250   W84  C~3coQ      
2014 11  13.03961  00 06 22.117  +04 00 31.63  23.6g 14UP250   W84  C~4yUz      
2014 11  13.04097  00 06 22.097  +04 00 31.64  22.3i 14UP250   W84  C~4yUz      
2014 11  14.04307  00 06 19.861  +04 00 10.08  23.2r 14UP250   W84  C~4yUz      
2014 11  14.04307  00 06 19.86   +04 00 10.1   23.1r 14UP250   W84  C~3coQ      
2016 09  11.19680  00 17 49.333  +04 33 54.83  22.4z 14UP250   W84  C~4yUz      
2016 09  11.19680  00 17 49.33   +04 33 54.8   22.4z 14UP250   W84  C~3coQ      
2016 09  11.24154  00 17 49.177  +04 33 53.53  22.7i 14UP250   W84  C~4yUz      
2016 09  11.24154  00 17 49.18   +04 33 53.5   23.0i 14UP250   W84  C~3coQ      
2016 09  22.13414  00 17 09.067  +04 29 00.28  22.8r 14UP250   W84  C~4yUz      
2016 09  22.13414  00 17 09.07   +04 29 00.3   22.9r 14UP250   W84  C~3coQ      
2016 09  22.13551  00 17 09.031  +04 29 00.18  24.1g 14UP250   W84  C~4yUz      
2016 12  05.06192  00 13 40.055  +03 59 56.28  22.6i 14UP250   W84  C~4yUz      
2016 12  05.06192  00 13 40.05   +03 59 56.3   22.8i 14UP250   W84  C~3coQ      
2016 12  05.07978  00 13 40.043  +03 59 56.07  22.8r 14UP250   W84  C~4yUz      
2016 12  05.07978  00 13 40.04   +03 59 56.1   22.6r 14UP250   W84  C~3coQ      
2017 08  22.31356  00 22 47.891  +04 44 14.64  23.5i 14UP250   W84  C~4yUz      
2017 08  22.31495  00 22 47.893  +04 44 14.58  23.7g 14UP250   W84  C~4yUz      
2017 09  27.17044  00 20 44.815  +04 29 20.86  22.7z 14UP250   W84  C~4yUz      
2017 10  22.17470  00 19 14.009  +04 17 49.15  22.7r 14UP250   W84  C~4yUz      
2017 10  22.17608  00 19 14.015  +04 17 49.22  22.6i 14UP250   W84  C~4yUz      
2017 10  22.17745  00 19 13.996  +04 17 49.02  23.5g 14UP250   W84  C~4yUz      
2019 11  01.25065  00 26 22.22   +04 18 51.5   23.8g 14UP250   T09  C~7bK3      
2019 11  01.25344  00 26 22.22   +04 18 51.5   24.2g 14UP250   T09  C~7bK3      
2019 11  01.31285  00 26 22.04   +04 18 50.0   23.8g 14UP250   T09  C~7bK3      
2019 11  01.40287  00 26 21.76   +04 18 48.0   24.0g 14UP250   T09  C~7bK3      
2019 11  01.48029  00 26 21.51   +04 18 45.3   24.2g 14UP250   T09  C~7bK3      
2020 08  12.351140 00 34 31.527  +04 53 55.17  23.1G 14UP250   G37  C~443e      
2020 08  12.421940 00 34 31.389  +04 53 54.03        14UP250   G37  C~443e      

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     0.07       0.00     0.09
     2   0.0000      0.00     0.03       0.00     0.06
     3   0.0000      0.00    -0.03       0.00     0.15
     4   0.0000      0.00     0.04       0.00     0.03
     5   0.0000      0.00    -0.02       0.00     0.01
     6   0.0027      0.00     0.04       0.00    -0.00
     7   0.0027      0.00     0.02       0.00    -0.00
     8   0.0028      0.00    -0.07       0.00     0.00
     9   0.0028      0.00    -0.01       0.00     0.06
    10   0.0435      0.00     0.18       0.00    -0.03
    11   0.0435      0.00    -0.07       0.00     0.01
    12   0.0462      0.00    -0.04       0.00    -0.02
    13   0.0462      0.00    -0.02       0.00    -0.04
    14   1.8728      0.00    -0.02       0.00     0.00
    15   1.8728      0.00     0.02       0.00     0.03
    16   1.8729      0.00     0.18       0.00    -0.13
    17   1.8729      0.00     0.14       0.00    -0.10
    18   1.9027      0.00     0.13       0.00     0.02
    19   1.9027      0.00     0.08       0.00     0.00
    20   1.9027      0.00    -0.38       0.00    -0.06
    21   2.1051      0.00    -0.16       0.00    -0.03
    22   2.1051      0.00    -0.08       0.00    -0.05
    23   2.1052      0.00    -0.06       0.00    -0.01
    24   2.1052      0.00    -0.01       0.00    -0.04
    25   2.8177      0.00    -0.11       0.00     0.04
    26   2.8177      0.00    -0.01       0.00     0.01
    27   2.9158      0.00     0.18       0.00    -0.10
    28   2.9843      0.00     0.01       0.00    -0.07
    29   2.9843      0.00     0.17       0.00     0.03
    30   2.9843      0.00    -0.04       0.00    -0.13
    31   5.0105      0.00    -0.15       0.00     0.18
    32   5.0105      0.00    -0.02       0.00     0.25
    33   5.0107      0.00     0.08       0.00     0.19
    34   5.0109      0.00     0.12       0.00     0.38
    35   5.0111      0.00    -0.01       0.00    -0.44
    36   5.7911      0.00    -0.16       0.00    -0.11
    37   5.7913      0.00     0.13       0.00    -0.09

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.

14UP250    quality flag:3

Type:       SCATNEAR  SCATNEAR  SCATNEAR

axisobj        52.675    52.675    52.674
ecceobj         0.363     0.363     0.363
incobj         20.811    20.811    20.811
qmin           32.323    31.873    31.081
qmax           73.609    73.579    74.882
amean          52.320    52.354    52.266
amin           51.477    51.410    51.477
amax           53.295    53.251    53.903
emean           0.358     0.360     0.372
emin            0.332     0.335     0.333
emax            0.382     0.385     0.406
imean          21.095    21.016    20.124
imin           20.083    19.812    18.249
imax           22.281    22.214    22.277
excite_mean     0.508     0.508     0.507
fracstop        1.000     1.000     1.000
cjmean          2.871     2.871     2.871

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       180.4     182.4     197.6
kozaiamp        180.0     180.0     180.0