Orbit Fit and Astrometric record for 14FP43

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: 14FP43    
# Created Sat Apr 20 01:15:44 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     66 observations of     66
# Arc:  11.21y
# First observation: 2010/12/15
#  Last observation: 2022/03/02
# Chi-squared of fit:    68.79 DOF:    126 RMS:  0.18
# Min/Max residuals:    -0.46    0.64
# Exact a, adot, b, bdot, g, gdot:
  1.518445E-05  2.401896E-02 -7.409862E-06 -1.267713E-02  2.557080E-02  2.859987E-03
# Covariance matrix:
  2.8006E-13 -6.0421E-14 -5.4837E-14  2.2926E-14  8.1330E-14 -1.6556E-13
 -6.0421E-14  2.6927E-14  2.5823E-14 -1.2477E-14  1.2131E-14  9.4695E-14
 -5.4837E-14  2.5823E-14  1.3907E-13 -3.5817E-14  6.0448E-15  1.1173E-13
  2.2926E-14 -1.2477E-14 -3.5817E-14  1.2273E-14 -6.5714E-15 -5.4184E-14
  8.1330E-14  1.2131E-14  6.0448E-15 -6.5714E-15  1.1237E-13  5.8508E-14
 -1.6556E-13  9.4695E-14  1.1173E-13 -5.4184E-14  5.8508E-14  4.1172E-13
#      lat0       lon0       xBary       yBary       zBary        JD0
    6.138566  175.402397    0.984111   -0.003319    0.030953  2455546.091076
# Heliocentric elements and errors
Epoch:              2455546.5000  =  2010/12/16
Mean Anomaly:           28.64641 +/-     0.008
Argument of Peri:      128.51319 +/-     0.011
Long of Asc Node:        5.48743 +/-     0.000
Inclination:            28.28625 +/-     0.000
Eccentricity:         0.14993664 +/-    0.0000
Semi-Major Axis:     44.67884960 +/-    0.0028
Time of Perihelion: 2446866.5137 +/-       2.7
Perihelion:          37.97985302 +/-    0.0030
Aphelion:            51.37784618 +/-    0.0037
Period (y)              298.6491 +/-      0.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -38.64373433 +/-    0.0005
Ecliptic Y            4.09379109 +/-    0.0001
Ecliptic Z            4.18153934 +/-    0.0001
Ecliptic XDOT        -0.00065496 +/-    0.0000
Ecliptic YDOT        -0.00252115 +/-    0.0000
Ecliptic ZDOT        -0.00131680 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   39.08424658 +/-    0.0005
Geocenter to KBO     39.10705624 +/-    0.0005
# Hcoef:  6.86

The following table shows the complete astrometric record for 14FP43. 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 (14FP43) followed by the observatory code and reference code for the source of the astrometry.

2010 12  15.59031  11 52 55.763  +07 27 31.28  23.5G 14FP43    F51  C~2rY1      
2011 04  02.30687  11 47 18.522  +07 59 52.35  22.0G 14FP43    F51  C~2rY1      
2011 04  02.33816  11 47 18.397  +07 59 52.88  22.9G 14FP43    F51  C~2rY1      
2011 04  02.35325  11 47 18.314  +07 59 53.39  22.9G 14FP43    F51  C~2rY1      
2012 02  26.40700  11 54 14.888  +06 30 54.00  23.4G 14FP43    F51  C~2rY1      
2012 03  27.35058  11 51 45.568  +06 43 26.98  22.7G 14FP43    F51  C~2rY2      
2013 03  08.46386  11 57 21.054  +05 21 09.54  22.2G 14FP43    F51  C~2rY2      
2014 02  10.52861  12 03 13.565  +03 56 40.16  23.4G 14FP43    F51  C~2rY2      
2014 02  26.565755 12 02 06.322  +04 02 46.18  21.8R 14FP43    F51  C~13iB      
2014 02  26.590206 12 02 06.196  +04 02 46.92  22.8R 14FP43    F51  C~13iB      
2014 02  26.59634  12 02 06.185  +04 02 46.87  23.1G 14FP43    F51  C~2rY2      
2014 02  27.48333  12 02 02.085  +04 03 08.62  22.7G 14FP43    F51  C~2rY2      
2014 02  27.489450 12 02 02.044  +04 03 08.72  22.1R 14FP43    F51  C~13iB      
2014 02  27.49557  12 02 02.022  +04 03 08.94  22.6G 14FP43    F51  C~2rY2      
2014 02  27.50788  12 02 01.966  +04 03 09.21  23.1G 14FP43    F51  C~2rY2      
2014 02  27.514050 12 02 01.925  +04 03 09.35  22.1R 14FP43    F51  C~13iB      
2014 02  27.52022  12 02 01.913  +04 03 09.67  22.6G 14FP43    F51  C~2rY2      
2014 03  24.357077 11 59 59.716  +04 13 32.00  21.7R 14FP43    F51  C~12hA      
2014 03  24.369194 11 59 59.640  +04 13 32.12  21.8R 14FP43    F51  C~12hA      
2014 03  24.381310 11 59 59.570  +04 13 32.43  21.6R 14FP43    F51  C~12hA      
2014 03  24.393469 11 59 59.511  +04 13 32.53  21.5R 14FP43    F51  C~12hA      
2014 03  29.357850 11 59 34.62   +04 15 30.8   22.2R 14FP43    H01  C~12hA      
2014 03  29.396542 11 59 34.42   +04 15 31.8   21.6R 14FP43    H01  C~12hA      
2014 03  29.409973 11 59 34.36   +04 15 32.2   21.9R 14FP43    H01  C~12hA      
2014 03  29.427194 11 59 34.28   +04 15 32.6   22.1R 14FP43    H01  C~12hA      
2014 04  04.35492  11 59 05.135  +04 17 46.65  24.0G 14FP43    F51  C~2rY2      
2014 04  26.307867 11 57 27.581  +04 24 22.43  21.3R 14FP43    568  C~13iB      
2014 04  26.309120 11 57 27.581  +04 24 22.47  21.8R 14FP43    568  C~13iB      
2014 04  26.375578 11 57 27.316  +04 24 23.44  21.6R 14FP43    568  C~13iB      
2014 04  26.376833 11 57 27.306  +04 24 23.54  21.8R 14FP43    568  C~13iB      
2014 04  26.378086 11 57 27.301  +04 24 23.53  21.9R 14FP43    568  C~13iB      
2014 04  30.29757  11 57 12.456  +04 25 12.54  23.1G 14FP43    F51  C~2rY2      
2014 05  20.28688  11 56 13.483  +04 27 19.29  23.0G 14FP43    F51  C~2rY2      
2014 06  28.28212  11 55 55.982  +04 20 17.76  23.4G 14FP43    F51  C~2rY2      
2015 01  21.60273  12 08 05.738  +02 38 00.86  22.8G 14FP43    F51  C~2rY2      
2015 01  21.61494  12 08 05.723  +02 38 01.06  23.0G 14FP43    F51  C~2rY2      
2015 01  21.62723  12 08 05.693  +02 38 01.02  23.1G 14FP43    F51  C~2rY2      
2015 01  21.63952  12 08 05.671  +02 38 01.10  23.3G 14FP43    F51  C~2rY2      
2015 02  18.53106  12 06 37.061  +02 45 50.00  22.6G 14FP43    F51  C~2rY2      
2015 02  18.54353  12 06 37.022  +02 45 50.23  22.7G 14FP43    F51  C~2rY2      
2015 02  18.55598  12 06 36.951  +02 45 50.01  23.0G 14FP43    F51  C~2rY2      
2015 02  18.56852  12 06 36.889  +02 45 50.70  22.8G 14FP43    F51  C~2rY2      
2015 02  19.54371  12 06 32.869  +02 46 11.81  21.4G 14FP43    F51  C~2rY2      
2015 03  16.27425  12 04 37.30   +02 56 10.8   22.7R 14FP43    G37  C~1zPr      
2015 03  16.34661  12 04 36.95   +02 56 12.4         14FP43    G37  C~1zPr      
2015 03  23.51541  12 04 00.982  +02 59 10.85  22.8G 14FP43    F51  C~2rY2      
2015 03  24.41580  12 03 56.475  +02 59 32.88  22.4G 14FP43    F51  C~2rY2      
2015 03  24.43027  12 03 56.419  +02 59 33.29  22.0G 14FP43    F51  C~2rY2      
2015 03  24.44473  12 03 56.327  +02 59 33.62  22.2G 14FP43    F51  C~2rY2      
2015 03  24.45925  12 03 56.243  +02 59 33.81  23.1G 14FP43    F51  C~2rY2      
2015 05  21.30420  12 00 05.444  +03 14 26.37  23.8G 14FP43    F51  C~2rY2      
2016 03  13.24780  12 08 42.70   +01 41 39.1   22.0R 14FP43    G37  C~1zPr      
2016 03  13.29615  12 08 42.42   +01 41 40.4         14FP43    G37  C~1zPr      
2017 02  21.52489  12 14 06.944  +00 20 46.76  22.8G 14FP43    F51  C~2rY2      
2017 03  23.17431  12 11 47.31   +00 32 24.6   22.9V 14FP43    W84  C~2y1p      
2017 03  23.24308  12 11 46.96   +00 32 26.4         14FP43    W84  C~2y1p      
2017 03  24.21933  12 11 42.10   +00 32 50.3         14FP43    W84  C~2y1p      
2017 04  03.46024  12 10 51.313  +00 36 56.79  22.0G 14FP43    F51  C~2rY2      
2017 04  20.36550  12 09 32.690  +00 42 59.35  22.7G 14FP43    F51  C~2rY2      
2018 04  13.34940  12 13 56.552  -00 32 12.08  23.9G 14FP43    F51  C~2rY2      
2018 04  13.36191  12 13 56.487  -00 32 11.61  22.5G 14FP43    F51  C~2rY2      
2018 04  13.37449  12 13 56.424  -00 32 11.50  22.9G 14FP43    F51  C~2rY2      
2018 04  13.38708  12 13 56.368  -00 32 11.02  23.0G 14FP43    F51  C~2rY2      
2022 03  02.403570 12 32 28.950  -05 34 28.36  23.2G 14FP43    G37  C~5S0Y      
2022 03  02.443720 12 32 28.760  -05 34 27.08        14FP43    G37  C~5S0Y      
2022 03  02.484420 12 32 28.574  -05 34 27.28        14FP43    G37  C~5S0Y      

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    -0.05
     2   0.2949      0.00    -0.22       0.00     0.10
     3   0.2950      0.00     0.25       0.00    -0.01
     4   0.2950      0.00     0.13       0.00     0.19
     5   1.1987      0.00     0.17       0.00     0.09
     6   1.2807      0.00     0.25       0.00    -0.10
     7   2.2283      0.00     0.01       0.00    -0.15
     8   3.1566      0.00     0.11       0.00    -0.03
     9   3.2005      0.00     0.28       0.00     0.04
    10   3.2005      0.00     0.11       0.00     0.18
    11   3.2006      0.00     0.37       0.00    -0.02
    12   3.2030      0.00     0.02       0.00    -0.06
    13   3.2030      0.00    -0.16       0.00    -0.11
    14   3.2030      0.00    -0.05       0.00    -0.04
    15   3.2031      0.00    -0.02       0.00    -0.07
    16   3.2031      0.00    -0.20       0.00    -0.09
    17   3.2031      0.00     0.05       0.00     0.08
    18   3.2711      0.00     0.09       0.00     0.29
    19   3.2711      0.00    -0.12       0.00     0.11
    20   3.2712      0.00    -0.24       0.00     0.13
    21   3.2712      0.00    -0.19       0.00    -0.07
    22   3.2848      0.00    -0.39       0.00    -0.04
    23   3.2849      0.00    -0.46       0.00     0.05
    24   3.2849      0.00    -0.35       0.00     0.14
    25   3.2850      0.00    -0.25       0.00     0.14
    26   3.3012      0.00     0.09       0.00     0.05
    27   3.3613      0.00    -0.06       0.00    -0.14
    28   3.3613      0.00     0.02       0.00    -0.12
    29   3.3615      0.00     0.03       0.00    -0.05
    30   3.3615      0.00    -0.04       0.00     0.04
    31   3.3615      0.00    -0.04       0.00     0.01
    32   3.3722      0.00    -0.08       0.00    -0.27
    33   3.4270      0.00     0.10       0.00     0.01
    34   3.5337      0.00     0.40       0.00    -0.05
    35   4.1013      0.00    -0.17       0.00     0.04
    36   4.1014      0.00     0.01       0.00     0.11
    37   4.1014      0.00    -0.05       0.00    -0.06
    38   4.1014      0.00     0.02       0.00    -0.11
    39   4.1778      0.00     0.05       0.00     0.17
    40   4.1778      0.00     0.25       0.00     0.13
    41   4.1779      0.00    -0.03       0.00    -0.37
    42   4.1779      0.00    -0.16       0.00     0.05
    43   4.1806      0.00     0.29       0.00    -0.33
    44   4.2483      0.00    -0.13       0.00     0.23
    45   4.2485      0.00     0.12       0.00     0.02
    46   4.2681      0.00    -0.03       0.00     0.10
    47   4.2706      0.00     0.05       0.00     0.05
    48   4.2706      0.00     0.32       0.00     0.11
    49   4.2706      0.00     0.05       0.00     0.09
    50   4.2707      0.00    -0.10       0.00    -0.08
    51   4.4291      0.00     0.47       0.00     0.04
    52   5.2420      0.00     0.47       0.00     0.10
    53   5.2422      0.00    -0.10       0.00     0.20
    54   6.1874      0.00    -0.26       0.00    -0.18
    55   6.2685      0.00    -0.16       0.00    -0.15
    56   6.2687      0.00    -0.18       0.00    -0.04
    57   6.2714      0.00    -0.01       0.00    -0.12
    58   6.2994      0.00    -0.26       0.00     0.10
    59   6.3457      0.00    -0.26       0.00    -0.06
    60   7.3258      0.00    -0.04       0.00    -0.24
    61   7.3259      0.00    -0.12       0.00    -0.05
    62   7.3259      0.00    -0.17       0.00    -0.21
    63   7.3259      0.00    -0.12       0.00    -0.01
    64  11.2110      0.00     0.35       0.00     0.10
    65  11.2111      0.00     0.15       0.00     0.64
    66  11.2112      0.00     0.04       0.00    -0.32

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.

14FP43    quality flag:3

Type:       SCATEXTD  SCATEXTD  SCATEXTD

axisobj        44.752    44.752    44.752
ecceobj         0.151     0.151     0.151
incobj         28.289    28.289    28.289
qmin           37.252    37.221    37.226
qmax           52.899    52.885    52.922
amean          44.888    44.888    44.889
amin           44.520    44.530    44.520
amax           45.300    45.299    45.298
emean           0.152     0.152     0.152
emin            0.137     0.138     0.137
emax            0.168     0.168     0.169
imean          28.454    28.454    28.454
imin           28.069    28.067    28.071
imax           28.773    28.778    28.768
excite_mean     0.500     0.500     0.500
fracstop        1.000     1.000     1.000
cjmean          2.793     2.793     2.793

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       182.2     182.2     182.4
kozaiamp        180.0     179.9     180.0