Orbit Fit and Astrometric record for 534074

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: 534074    
# Created Thu Apr 25 01:08:41 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     51 observations of     51
# Arc:  12.11y
# First observation: 2011/09/04
#  Last observation: 2023/10/14
# Chi-squared of fit:    34.70 DOF:     96 RMS:  0.15
# Min/Max residuals:    -0.43    0.40
# Exact a, adot, b, bdot, g, gdot:
  1.365734E-05  2.085550E-02  2.799015E-07  1.817327E-03  2.287624E-02 -9.919336E-04
# 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
    4.275417   15.654548    0.567466    0.061835   -0.827580  2455808.934256
# Heliocentric elements and errors
Epoch:              2455808.5000  =  2011/09/04
Mean Anomaly:          234.93951 +/-     0.000
Argument of Peri:      171.86404 +/-     0.000
Long of Asc Node:      335.16599 +/-     0.000
Inclination:             6.54291 +/-     0.000
Eccentricity:         0.07743517 +/-    0.0000
Semi-Major Axis:     42.49848424 +/-    0.0000
Time of Perihelion: 2490962.6175 +/-       0.0
Perihelion:          39.20760683 +/-    0.0000
Aphelion:            45.78936164 +/-    0.0000
Period (y)              277.0565 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           42.93058322 +/-    0.0000
Ecliptic Y           11.44149919 +/-    0.0000
Ecliptic Z            3.25891553 +/-    0.0000
Ecliptic XDOT        -0.00080632 +/-    0.0000
Ecliptic YDOT         0.00237247 +/-    0.0000
Ecliptic ZDOT         0.00020811 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   44.54847729 +/-    0.0000
Geocenter to KBO     43.71352982 +/-    0.0000
# Hcoef:  5.88

The following table shows the complete astrometric record for 534074. 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 (534074) followed by the observatory code and reference code for the source of the astrometry.

2011 09  04.43349  00 50 59.314  +10 06 14.36  22.7w 534074    F51  C~1vXi      
2011 09  04.44834  00 50 59.253  +10 06 13.88  22.4w 534074    F51  C~1vXi      
2011 09  04.46324  00 50 59.213  +10 06 13.64  22.5w 534074    F51  C~1vXi      
2011 09  04.47825  00 50 59.151  +10 06 13.37  22.6w 534074    F51  C~1vXi      
2011 10  25.28773  00 47 27.522  +09 45 52.02  22.2G 534074    F51  C~2r7W      
2012 09  26.50249  00 53 48.501  +10 31 56.72  21.4G 534074    F51  C~2r7W      
2012 10  09.35135  00 52 52.497  +10 26 31.24  22.0G 534074    F51  C~2r7W      
2012 10  09.36547  00 52 52.433  +10 26 30.80  22.2G 534074    F51  C~2r7W      
2012 10  09.37970  00 52 52.361  +10 26 30.54  22.2G 534074    F51  C~2r7W      
2012 10  09.39400  00 52 52.310  +10 26 30.16  22.4G 534074    F51  C~2r7W      
2012 11  03.41242  00 51 07.798  +10 15 27.29  22.8G 534074    F51  C~2r7W      
2012 11  04.25003  00 51 04.615  +10 15 05.88  22.3w 534074    F51  C~1vXi      
2012 11  04.26414  00 51 04.568  +10 15 05.71  22.3w 534074    F51  C~1vXi      
2012 11  04.27822  00 51 04.513  +10 15 05.36  22.3w 534074    F51  C~1vXi      
2012 11  04.29242  00 51 04.452  +10 15 05.01  22.3w 534074    F51  C~1vXi      
2013 09  15.54773  00 58 56.673  +11 09 46.62  22.2G 534074    F51  C~2r7W      
2013 09  15.56146  00 58 56.628  +11 09 46.50  22.9G 534074    F51  C~2r7W      
2013 09  15.57527  00 58 56.553  +11 09 46.32  22.8G 534074    F51  C~2r7W      
2014 06  30.58798  01 05 16.292  +11 46 25.97  22.5w 534074    F51  C~1vXi      
2014 06  30.59192  01 05 16.297  +11 46 25.87  22.3w 534074    F51  C~1vXi      
2014 06  30.59588  01 05 16.296  +11 46 26.03  22.6w 534074    F51  C~1vXi      
2014 06  30.59982  01 05 16.311  +11 46 26.11  22.2w 534074    F51  C~1vXi      
2014 08  28.44831  01 04 24.386  +11 48 15.08  22.7w 534074    F51  C~1vXi      
2014 08  28.47287  01 04 24.317  +11 48 14.66  22.6w 534074    F51  C~1vXi      
2014 08  28.48506  01 04 24.277  +11 48 14.35  22.3w 534074    F51  C~1vXi      
2014 09  19.44819  01 03 04.756  +11 41 55.16  22.5G 534074    F51  C~2r7W      
2014 09  29.51918  01 02 22.197  +11 38 06.96  22.3w 534074    F51  C~1vXi      
2014 09  29.53062  01 02 22.144  +11 38 06.73  22.2w 534074    F51  C~1vXi      
2014 09  29.54206  01 02 22.109  +11 38 06.51  22.2w 534074    F51  C~1vXi      
2014 09  29.55351  01 02 22.043  +11 38 06.11  22.1w 534074    F51  C~1vXi      
2014 11  18.25537  00 58 58.265  +11 16 50.06  22.1w 534074    F51  C~1vXi      
2014 11  18.26729  00 58 58.251  +11 16 50.30  22.2w 534074    F51  C~1vXi      
2014 11  18.29121  00 58 58.136  +11 16 49.80  22.2w 534074    F51  C~1vXi      
2015 11  18.23609  01 03 21.345  +11 50 16.39  22.6G 534074    F51  C~2r7W      
2015 12  03.24445  01 02 38.619  +11 44 54.78  22.5G 534074    F51  C~2r7W      
2015 12  14.31909  01 02 17.570  +11 41 49.81  22.4G 534074    F51  C~2r7W      
2016 10  06.50824  01 10 39.611  +12 41 31.22  22.6G 534074    F51  C~2r7W      
2016 10  06.52075  01 10 39.542  +12 41 30.96  21.7G 534074    F51  C~2r7W      
2016 10  06.53327  01 10 39.505  +12 41 30.64  22.1G 534074    F51  C~2r7W      
2016 10  06.54577  01 10 39.449  +12 41 30.38  22.2G 534074    F51  C~2r7W      
2017 09  19.54016  01 16 20.951  +13 20 52.12  23.1G 534074    F51  C~2r7W      
2017 09  19.55303  01 16 20.895  +13 20 51.90  22.3G 534074    F51  C~2r7W      
2017 09  19.56577  01 16 20.860  +13 20 51.74  22.3G 534074    F51  C~2r7W      
2017 09  19.57850  01 16 20.793  +13 20 51.32  22.6G 534074    F51  C~2r7W      
2017 10  22.46877  01 13 57.095  +13 07 44.82  22.5G 534074    F51  C~2r7W      
2017 11  10.29066  01 12 38.337  +12 59 29.97  21.7G 534074    F51  C~2r7W      
2018 02  04.26199  01 11 35.541  +12 45 30.12  22.4G 534074    F51  C~2r7W      
2023 10  14.344603 01 42 10.620  +16 25 09.74  22.4w 534074    F52  C~7MED      
2023 10  14.357520 01 42 10.531  +16 25 09.55  22.3w 534074    F52  C~7MED      
2023 10  14.370491 01 42 10.487  +16 25 09.31  22.2w 534074    F52  C~7MED      
2023 10  14.383412 01 42 10.423  +16 25 08.83  22.2w 534074    F52  C~7MED      

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     0.25
     2   0.0000      0.00    -0.04       0.00     0.03
     3   0.0001      0.00     0.18       0.00     0.05
     4   0.0001      0.00     0.07       0.00     0.04
     5   0.1392      0.00    -0.43       0.00    -0.27
     6   1.0625      0.00    -0.17       0.00    -0.05
     7   1.0977      0.00    -0.03       0.00    -0.02
     8   1.0977      0.00    -0.05       0.00    -0.09
     9   1.0977      0.00    -0.17       0.00     0.03
    10   1.0978      0.00     0.02       0.00     0.02
    11   1.1663      0.00     0.28       0.00    -0.07
    12   1.1686      0.00    -0.04       0.00    -0.05
    13   1.1686      0.00     0.06       0.00     0.14
    14   1.1686      0.00     0.05       0.00     0.15
    15   1.1687      0.00    -0.05       0.00     0.16
    16   2.0318      0.00     0.10       0.00    -0.14
    17   2.0318      0.00     0.26       0.00     0.02
    18   2.0319      0.00    -0.03       0.00     0.13
    19   2.8204      0.00    -0.08       0.00     0.01
    20   2.8204      0.00    -0.09       0.00    -0.16
    21   2.8204      0.00    -0.19       0.00    -0.06
    22   2.8204      0.00    -0.05       0.00    -0.05
    23   2.9816      0.00    -0.05       0.00     0.06
    24   2.9816      0.00     0.07       0.00    -0.05
    25   2.9817      0.00     0.04       0.00    -0.21
    26   3.0418      0.00     0.11       0.00    -0.27
    27   3.0694      0.00    -0.08       0.00     0.12
    28   3.0694      0.00    -0.12       0.00     0.16
    29   3.0694      0.00     0.11       0.00     0.22
    30   3.0695      0.00    -0.12       0.00     0.09
    31   3.2055      0.00    -0.09       0.00    -0.17
    32   3.2056      0.00     0.29       0.00     0.35
    33   3.2056      0.00    -0.25       0.00     0.40
    34   4.2048      0.00     0.07       0.00    -0.02
    35   4.2459      0.00    -0.15       0.00    -0.09
    36   4.2762      0.00    -0.04       0.00    -0.18
    37   5.0899      0.00     0.15       0.00    -0.17
    38   5.0899      0.00    -0.04       0.00    -0.12
    39   5.0899      0.00     0.25       0.00    -0.12
    40   5.0900      0.00     0.26       0.00    -0.07
    41   6.0427      0.00     0.00       0.00    -0.03
    42   6.0428      0.00    -0.04       0.00     0.00
    43   6.0428      0.00     0.22       0.00     0.10
    44   6.0428      0.00    -0.01       0.00    -0.07
    45   6.1329      0.00     0.01       0.00    -0.15
    46   6.1844      0.00    -0.14       0.00    -0.07
    47   6.4198      0.00     0.17       0.00    -0.11
    48  12.1093      0.00     0.16       0.00     0.01
    49  12.1093      0.00    -0.27       0.00     0.12
    50  12.1093      0.00    -0.03       0.00     0.19
    51  12.1094      0.00    -0.08       0.00     0.01

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.

534074    quality flag:3

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

axisobj        42.552    42.552    42.552
ecceobj         0.076     0.076     0.076
incobj          6.540     6.540     6.540
qmin           37.041    37.041    37.041
qmax           48.090    48.089    48.089
amean          42.329    42.329    42.329
amin           41.934    41.935    41.934
amax           42.757    42.757    42.758
emean           0.096     0.096     0.096
emin            0.065     0.065     0.065
emax            0.125     0.125     0.125
imean           6.803     6.803     6.802
imin            5.592     5.592     5.592
imax            8.169     8.169     8.169
excite_mean     0.153     0.153     0.153
fracstop        1.000     1.000     1.000
cjmean          3.054     3.054     3.054

libcent 0       181.6     181.5     182.3
libamp  0        96.7      96.7      95.5
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       175.5     175.6     175.6
kozaiamp        180.0     180.0     180.0