Orbit Fit and Astrometric record for 18FY73

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: 18FY73    
# Created Sun Dec 22 02:11:02 2024
# Orbit generated from Bernstein formalism
# Fitting     21 observations of     21
# Arc:   2.97y
# First observation: 2016/03/17
#  Last observation: 2019/03/08
Preliminary a, adot, b, bdot, g, gdot:
  -0.000025   0.033639  -0.000014   0.002404   0.029685   0.000000
# Chi-squared of fit:     7.75 DOF:     36 RMS:  0.11
# Min/Max residuals:    -0.24    0.25
# Exact a, adot, b, bdot, g, gdot:
  1.759191E-05  3.366916E-02  1.189660E-06  2.401696E-03  2.935476E-02  3.695762E-04
# Covariance matrix:
  7.3246E-13 -5.9858E-13  1.1467E-14 -2.5738E-14 -2.3671E-13 -3.4477E-12
 -5.9858E-13  1.3870E-12 -4.2393E-14  9.6302E-14  1.5239E-12  1.2885E-11
  1.1467E-14 -4.2393E-14  5.6709E-13 -2.3295E-13 -5.2934E-14 -4.2981E-13
 -2.5738E-14  9.6302E-14 -2.3295E-13  1.1381E-13  1.2129E-13  9.7773E-13
 -2.3671E-13  1.5239E-12 -5.2934E-14  1.2129E-13  2.4891E-12  1.6215E-11
 -3.4477E-12  1.2885E-11 -4.2981E-13  9.7773E-13  1.6215E-11  1.3080E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
    0.299014  170.429019   -0.111906    0.005287   -0.985178  2457464.925037
# Heliocentric elements and errors
Epoch:              2457460.5000  =  2016/03/13
Mean Anomaly:            3.54252 +/-     0.088
Argument of Peri:      358.88571 +/-     0.129
Long of Asc Node:      166.53967 +/-     0.001
Inclination:             4.08114 +/-     0.001
Eccentricity:         0.17990728 +/-    0.0001
Semi-Major Axis:     42.71806535 +/-    0.0085
Time of Perihelion: 2456456.9820 +/-      24.8
Perihelion:          35.03277458 +/-    0.0084
Aphelion:            50.40335612 +/-    0.0111
Period (y)              279.2065 +/-      0.08
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -34.58533638 +/-    0.0018
Ecliptic Y            5.71499265 +/-    0.0003
Ecliptic Z            0.17783952 +/-    0.0000
Ecliptic XDOT        -0.00055500 +/-    0.0000
Ecliptic YDOT        -0.00309798 +/-    0.0000
Ecliptic ZDOT         0.00022419 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   35.05478940 +/-    0.0018
Geocenter to KBO     34.06602469 +/-    0.0018
# Hcoef:  7.58

The following table shows the complete astrometric record for 18FY73. 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 (18FY73) followed by the observatory code and reference code for the source of the astrometry.

2016 03  17.424248 11 25 17.70   +04 04 01.7         18FY73    T09  C~89VN      
2016 03  17.566829 11 25 16.93   +04 04 06.6         18FY73    T09  C~89VN      
2018 03  10.454806 11 40 35.66   +02 43 15.6         18FY73    T09  C~89VN      
2018 03  18.45971  11 39 53.98   +02 47 57.0   23.2i 18FY73    T09  C~89VN      
2018 03  18.48956  11 39 53.82   +02 47 58.2   23.0i 18FY73    T09  C~89VN      
2018 03  18.50304  11 39 53.75   +02 47 58.5   22.8i 18FY73    T09  C~89VN      
2018 03  18.56001  11 39 53.45   +02 48 00.4   22.6i 18FY73    T09  C~89VN      
2018 04  22.298971 11 37 10.17   +03 06 12.7         18FY73    T09  C~89VN      
2018 04  22.407617 11 37 09.74   +03 06 15.6         18FY73    T09  C~89VN      
2018 04  24.35200  11 37 02.43   +03 07 04.4   23.0z 18FY73    T09  C~89VN      
2018 04  24.39881  11 37 02.24   +03 07 05.4   22.9z 18FY73    T09  C~89VN      
2018 04  24.42918  11 37 02.13   +03 07 06.2   22.4z 18FY73    T09  C~89VN      
2018 04  24.44256  11 37 02.09   +03 07 06.2   22.7z 18FY73    T09  C~89VN      
2018 04  24.48536  11 37 01.93   +03 07 07.6   22.4z 18FY73    T09  C~89VN      
2019 02  05.457878 11 50 23.90   +01 47 27.7         18FY73    T09  C~89VN      
2019 02  05.498105 11 50 23.75   +01 47 28.8         18FY73    T09  C~89VN      
2019 03  02.51613  11 48 34.35   +02 00 11.5   23.0y 18FY73    T09  C~8CPH      
2019 03  02.55921  11 48 34.13   +02 00 12.8   22.9y 18FY73    T09  C~8CPH      
2019 03  02.60017  11 48 33.93   +02 00 14.5   22.5y 18FY73    T09  C~8CPH      
2019 03  08.391723 11 48 04.73   +02 03 34.2         18FY73    T09  C~89VN      
2019 03  08.433927 11 48 04.51   +02 03 35.7         18FY73    T09  C~89VN      

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     0.11       0.00     0.02
     2   0.0004    -12.52    -0.11      -0.03    -0.11
     3   1.9795  14565.48    -0.02     981.52     0.13
     4   2.0015  13877.35    -0.02     991.93     0.07
     5   2.0015  13874.66    -0.10     992.08     0.20
     6   2.0016  13873.57    -0.01     991.94     0.05
     7   2.0017  13868.67     0.04     991.90    -0.03
     8   2.0969  11180.17     0.25    1024.59    -0.08
     9   2.0971  11173.08     0.15    1024.70     0.02
    10   2.1025  11052.87    -0.07    1026.11     0.13
    11   2.1026  11049.85    -0.19    1025.90    -0.08
    12   2.1027  11048.02    -0.15    1025.98    -0.00
    13   2.1027  11047.47     0.12    1025.74    -0.24
    14   2.1028  11044.71    -0.01    1026.08     0.09
    15   2.8885  24070.90     0.10    1420.44    -0.03
    16   2.8886  24068.37     0.05    1420.55     0.02
    17   2.9571  22237.37    -0.11    1466.52    -0.06
    18   2.9572  22233.79    -0.07    1466.39    -0.22
    19   2.9574  22230.32    -0.10    1466.76     0.10
    20   2.9732  21743.80     0.07    1475.54     0.00
    21   2.9733  21740.14     0.06    1475.60     0.03

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.

18FY73    quality flag:3

Type:          5:3EE     5:3EE     5:3EE

axisobj        42.325    42.344    42.305
ecceobj         0.172     0.172     0.171
incobj          4.098     4.098     4.098
qmin           34.346    34.231    34.249
qmax           50.886    51.134    50.803
amean          42.328    42.328    42.328
amin           41.889    41.867    41.901
amax           42.812    42.851    42.810
emean           0.172     0.173     0.172
emin            0.155     0.155     0.156
emax            0.189     0.194     0.188
imean           3.911     3.969     3.872
imin            3.282     3.249     3.335
imax            4.820     4.799     4.548
excite_mean     0.185     0.186     0.185
fracstop        1.000     1.000     1.000
cjmean          3.042     3.041     3.042

libcent 0       181.1     179.1     180.8
libamp  0        82.2      93.5      72.9
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       158.1     198.7     192.2
kozaiamp        180.0     179.9     180.0