Orbit Fit and Astrometric record for 535229

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: 535229    
# Created Fri Nov 22 02:07:30 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     64 observations of     64
# Arc:  11.16y
# First observation: 2011/12/23
#  Last observation: 2023/02/20
# Chi-squared of fit:    54.78 DOF:    122 RMS:  0.16
# Min/Max residuals:    -0.66    0.55
# Exact a, adot, b, bdot, g, gdot:
  1.822955E-05  3.429976E-02 -5.803763E-06 -1.068094E-02  3.092535E-02  4.535172E-03
# Covariance matrix:
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
#      lat0       lon0       xBary       yBary       zBary        JD0
    8.546630   99.079637    0.134787    0.144661   -0.962393  2455918.877176
# Heliocentric elements and errors
Epoch:              2455918.5000  =  2011/12/23
Mean Anomaly:           30.53088 +/-     0.000
Argument of Peri:      108.51740 +/-     0.000
Long of Asc Node:      303.81188 +/-     0.000
Inclination:            19.05687 +/-     0.000
Eccentricity:         0.20101089 +/-    0.0000
Semi-Major Axis:     39.61238573 +/-    0.0000
Time of Perihelion: 2448195.5757 +/-       0.0
Perihelion:          31.64986485 +/-    0.0000
Aphelion:            47.57490661 +/-    0.0000
Period (y)              249.3186 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           -5.06396322 +/-    0.0000
Ecliptic Y           32.55968635 +/-    0.0000
Ecliptic Z            4.80536614 +/-    0.0000
Ecliptic XDOT        -0.00308757 +/-    0.0000
Ecliptic YDOT         0.00005636 +/-    0.0000
Ecliptic ZDOT        -0.00087534 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   33.29960223 +/-    0.0000
Geocenter to KBO     32.33589362 +/-    0.0000
# Hcoef:  7.13

The following table shows the complete astrometric record for 535229. 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 (535229) followed by the observatory code and reference code for the source of the astrometry.

2011 12  23.37641  06 42 15.267  +31 39 12.86  22.1G 535229    F51  C~2rYH      
2012 01  03.34691  06 40 56.150  +31 39 27.02  23.2G 535229    F51  C~2rYH      
2012 12  31.50519  06 50 06.200  +30 53 25.44  22.5G 535229    F51  C~2rYH      
2013 01  01.51402  06 49 58.978  +30 53 27.80  23.1G 535229    F51  C~2rYH      
2013 01  10.46715  06 48 55.232  +30 53 32.05  21.9G 535229    F51  C~2rYH      
2013 04  11.25775  06 44 27.790  +30 33 01.12  22.8G 535229    F51  C~2rYH      
2013 09  14.62090  07 03 08.248  +29 52 47.35  22.6G 535229    F51  C~2rYH      
2013 11  25.54628  07 02 35.657  +30 01 04.92  22.4G 535229    F51  C~2rYH      
2013 12  04.42972  07 01 47.748  +30 02 30.07  22.6w 535229    F51  C~1vXz      
2013 12  04.44367  07 01 47.667  +30 02 30.09  22.4w 535229    F51  C~1vXz      
2013 12  04.45766  07 01 47.587  +30 02 30.36  22.3w 535229    F51  C~1vXz      
2013 12  04.47165  07 01 47.517  +30 02 30.67  22.4w 535229    F51  C~1vXz      
2013 12  26.37431  06 59 25.725  +30 05 12.65  22.1w 535229    F51  C~1vXz      
2013 12  26.37499  06 59 25.729  +30 05 12.60  22.1w 535229    F51  C~1vXz      
2013 12  26.38973  06 59 25.617  +30 05 12.75  22.4w 535229    F51  C~1vXz      
2013 12  26.39042  06 59 25.623  +30 05 12.78  22.2w 535229    F51  C~1vXz      
2013 12  26.40517  06 59 25.510  +30 05 12.71  22.6w 535229    F51  C~1vXz      
2013 12  26.40585  06 59 25.512  +30 05 12.87  22.4w 535229    F51  C~1vXz      
2014 11  20.63391  07 11 20.390  +29 10 16.80  22.5G 535229    F51  C~2rYH      
2014 12  26.52041  07 07 54.228  +29 15 39.28  22.2w 535229    F51  C~1vXz      
2014 12  26.53273  07 07 54.147  +29 15 39.24  22.5w 535229    F51  C~1vXz      
2014 12  26.54502  07 07 54.065  +29 15 39.44  22.4w 535229    F51  C~1vXz      
2015 01  18.28845  07 05 16.683  +29 17 10.55  22.5G 535229    F51  C~2rYH      
2015 01  20.32299  07 05 02.989  +29 17 12.01  21.9w 535229    F51  C~1vXz      
2015 01  20.33492  07 05 02.899  +29 17 11.97  22.3w 535229    F51  C~1vXz      
2015 01  20.34682  07 05 02.812  +29 17 11.92  22.2w 535229    F51  C~1vXz      
2015 01  20.35877  07 05 02.728  +29 17 11.86  22.2w 535229    F51  C~1vXz      
2015 01  22.29898  07 04 49.807  +29 17 12.29  22.5w 535229    F51  C~1vXz      
2015 01  22.31086  07 04 49.718  +29 17 12.21  22.5w 535229    F51  C~1vXz      
2015 01  22.32274  07 04 49.648  +29 17 12.26  22.4w 535229    F51  C~1vXz      
2015 01  28.32475  07 04 10.797  +29 17 05.89  22.5G 535229    F51  C~2rYH      
2015 09  17.59185  07 19 16.021  +28 14 35.33  23.1G 535229    F51  C~2rYH      
2015 12  04.62718  07 18 23.572  +28 21 16.90  22.4G 535229    F51  C~2rYH      
2016 02  09.26371  07 11 17.413  +28 26 45.58  22.2G 535229    F51  C~2rYH      
2016 02  09.27788  07 11 17.318  +28 26 45.53  22.5G 535229    F51  C~2rYH      
2016 02  09.29212  07 11 17.263  +28 26 45.40  21.9G 535229    F51  C~2rYH      
2016 02  09.30643  07 11 17.172  +28 26 45.50  22.3G 535229    F51  C~2rYH      
2017 01  28.43494  07 20 26.744  +27 35 43.96  22.4G 535229    F51  C~2rYH      
2017 01  28.44719  07 20 26.669  +27 35 43.30  22.9G 535229    F51  C~2rYH      
2017 01  28.45950  07 20 26.552  +27 35 43.69  23.0G 535229    F51  C~2rYH      
2017 01  28.47181  07 20 26.466  +27 35 43.58  22.8G 535229    F51  C~2rYH      
2017 12  20.47108  07 32 34.360  +26 38 06.62  22.4R 535229    G37  C~2Uxt      
2017 12  20.51274  07 32 34.098  +26 38 06.99        535229    G37  C~2Uxt      
2017 12  25.53683  07 32 02.799  +26 38 57.67  22.3G 535229    F51  C~2rYH      
2017 12  25.54894  07 32 02.729  +26 38 58.00  22.2G 535229    F51  C~2rYH      
2017 12  25.56105  07 32 02.644  +26 38 58.15  21.8G 535229    F51  C~2rYH      
2017 12  25.57317  07 32 02.567  +26 38 58.27  21.7G 535229    F51  C~2rYH      
2018 01  08.37682  07 30 31.852  +26 41 04.65  22.2G 535229    F51  C~2rYH      
2018 01  15.32999  07 29 45.114  +26 41 57.78  22.2G 535229    F51  C~2rYH      
2018 01  15.33129  07 29 45.097  +26 41 57.64  22.3G 535229    F51  C~2rYI      
2018 01  15.34250  07 29 45.013  +26 41 57.91  23.1G 535229    F51  C~2rYI      
2018 01  15.34379  07 29 45.001  +26 41 57.62  21.7G 535229    F51  C~2rYI      
2018 01  15.35499  07 29 44.940  +26 41 57.76  22.0G 535229    F51  C~2rYI      
2018 01  15.35628  07 29 44.931  +26 41 57.61  21.4G 535229    F51  C~2rYI      
2018 01  15.36747  07 29 44.867  +26 41 57.87  22.1G 535229    F51  C~2rYI      
2018 01  15.36876  07 29 44.843  +26 41 58.20  22.6G 535229    F51  C~2rYI      
2018 02  20.24791  07 26 10.657  +26 43 26.99  19.9G 535229    F51  C~2rYI      
2018 02  20.27293  07 26 10.566  +26 43 27.07  22.9G 535229    F51  C~2rYI      
2020 12  09.410900 07 55 39.129  +23 50 37.10  22.6G 535229    G37  C~4Tuj      
2020 12  09.462430 07 55 38.864  +23 50 37.88        535229    G37  C~4Tuj      
2020 12  09.507100 07 55 38.660  +23 50 38.52        535229    G37  C~4Tuj      
2023 02  20.136030 08 02 30.449  +22 10 40.90  22.5G 535229    G37  C~6IlA      
2023 02  20.180810 08 02 30.220  +22 10 41.18        535229    G37  C~6IlA      
2023 02  20.226490 08 02 29.984  +22 10 41.55        535229    G37  C~6IlA      

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    -0.16       0.00     0.08
     2   0.0300      0.00    -0.14       0.00    -0.06
     3   1.0243      0.00     0.19       0.00    -0.17
     4   1.0271      0.00     0.05       0.00     0.16
     5   1.0516      0.00    -0.25       0.00    -0.35
     6   1.3002      0.00     0.27       0.00    -0.06
     7   1.7283      0.00     0.10       0.00    -0.02
     8   1.9252      0.00     0.35       0.00    -0.17
     9   1.9495      0.00    -0.19       0.00     0.08
    10   1.9495      0.00    -0.18       0.00    -0.04
    11   1.9496      0.00    -0.14       0.00     0.10
    12   1.9496      0.00     0.05       0.00     0.28
    13   2.0096      0.00    -0.13       0.00     0.06
    14   2.0096      0.00     0.01       0.00     0.00
    15   2.0096      0.00    -0.11       0.00     0.07
    16   2.0096      0.00     0.05       0.00     0.10
    17   2.0097      0.00    -0.08       0.00    -0.06
    18   2.0097      0.00     0.02       0.00     0.10
    19   2.9110      0.00     0.01       0.00     0.05
    20   3.0093      0.00    -0.00       0.00     0.06
    21   3.0093      0.00     0.06       0.00    -0.05
    22   3.0094      0.00     0.11       0.00     0.07
    23   3.0716      0.00    -0.25       0.00     0.09
    24   3.0772      0.00     0.24       0.00     0.05
    25   3.0772      0.00     0.11       0.00     0.01
    26   3.0773      0.00     0.03       0.00    -0.05
    27   3.0773      0.00    -0.01       0.00    -0.12
    28   3.0826      0.00     0.07       0.00     0.07
    29   3.0826      0.00    -0.07       0.00    -0.01
    30   3.0827      0.00     0.08       0.00     0.03
    31   3.0991      0.00    -0.04       0.00     0.05
    32   3.7350      0.00    -0.29       0.00     0.21
    33   3.9487      0.00     0.00       0.00    -0.21
    34   4.1311      0.00     0.03       0.00    -0.11
    35   4.1311      0.00    -0.20       0.00    -0.11
    36   4.1312      0.00     0.18       0.00    -0.20
    37   4.1312      0.00     0.03       0.00    -0.06
    38   5.1008      0.00     0.48       0.00     0.55
    39   5.1008      0.00     0.54       0.00    -0.14
    40   5.1008      0.00    -0.03       0.00     0.23
    41   5.1009      0.00    -0.13       0.00     0.10
    42   5.9934      0.00     0.07       0.00     0.04
    43   5.9935      0.00    -0.00       0.00    -0.00
    44   6.0073      0.00    -0.03       0.00    -0.19
    45   6.0073      0.00     0.10       0.00     0.02
    46   6.0074      0.00    -0.01       0.00     0.06
    47   6.0074      0.00     0.01       0.00     0.06
    48   6.0452      0.00    -0.02       0.00    -0.14
    49   6.0642      0.00     0.05       0.00     0.07
    50   6.0642      0.00    -0.07       0.00    -0.08
    51   6.0642      0.00    -0.19       0.00     0.11
    52   6.0643      0.00    -0.24       0.00    -0.19
    53   6.0643      0.00    -0.01       0.00    -0.13
    54   6.0643      0.00    -0.01       0.00    -0.29
    55   6.0643      0.00     0.17       0.00    -0.11
    56   6.0643      0.00    -0.05       0.00     0.21
    57   6.1626      0.00    -0.66       0.00    -0.15
    58   6.1626      0.00    -0.22       0.00    -0.01
    59   8.9638      0.00     0.18       0.00    -0.26
    60   8.9640      0.00    -0.05       0.00    -0.00
    61   8.9641      0.00     0.12       0.00     0.19
    62  11.1616      0.00    -0.06       0.00     0.07
    63  11.1617      0.00     0.03       0.00     0.02
    64  11.1618      0.00     0.08       0.00     0.06

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.

535229    quality flag:3

Type:           3:2E      3:2E      3:2E

axisobj        39.757    39.757    39.756
ecceobj         0.204     0.204     0.204
incobj         19.058    19.058    19.058
qmin           27.196    27.196    27.197
qmax           52.478    52.475    52.470
amean          39.455    39.455    39.455
amin           39.004    39.003    39.005
amax           40.000    39.997    39.998
emean           0.253     0.254     0.254
emin            0.179     0.179     0.179
emax            0.312     0.312     0.312
imean          18.086    18.084    18.085
imin           15.684    15.680    15.687
imax           20.865    20.865    20.865
excite_mean     0.403     0.403     0.403
fracstop        1.000     1.000     1.000
cjmean          2.866     2.866     2.866

libcent 0       178.5     178.7     178.6
libamp  0        91.1      91.3      91.1
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        89.4      89.4      89.5
kozaiamp         71.3      71.4      71.3