Orbit Fit and Astrometric record for 525596

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: 525596    
# Created Thu Mar 28 01:08:40 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     41 observations of     41
# Arc:  12.92y
# First observation: 2005/05/11
#  Last observation: 2018/04/12
# Chi-squared of fit:    70.43 DOF:     76 RMS:  0.23
# Min/Max residuals:    -0.65    0.61
# Exact a, adot, b, bdot, g, gdot:
  1.567792E-05  2.126070E-02 -8.130184E-08 -1.059937E-03  2.254186E-02  2.205440E-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
    2.458991 -149.297070   -0.341486    0.040763   -0.946266  2453501.526543
# Heliocentric elements and errors
Epoch:              2453502.5000  =  2005/05/12
Mean Anomaly:           63.89403 +/-     0.000
Argument of Peri:       63.12136 +/-     0.000
Long of Asc Node:       71.15285 +/-     0.000
Inclination:             3.74050 +/-     0.000
Eccentricity:         0.11831435 +/-    0.0000
Semi-Major Axis:     47.19847409 +/-    0.0000
Time of Perihelion: 2432481.7536 +/-       0.0
Perihelion:          41.61421720 +/-    0.0000
Aphelion:            52.78273098 +/-    0.0000
Period (y)              324.2650 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -38.75236536 +/-    0.0000
Ecliptic Y          -23.40819998 +/-    0.0000
Ecliptic Z            1.90329842 +/-    0.0000
Ecliptic XDOT         0.00108427 +/-    0.0000
Ecliptic YDOT        -0.00236681 +/-    0.0000
Ecliptic ZDOT        -0.00011707 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   45.31341377 +/-    0.0000
Geocenter to KBO     44.36187746 +/-    0.0000
# Hcoef:  6.62

The following table shows the complete astrometric record for 525596. 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 (525596) followed by the observatory code and reference code for the source of the astrometry.

2005 05  11.02580  13 57 48.73   -09 24 46.6   22.1R 525596    807  Cn7093      
2005 05  11.11523  13 57 48.38   -09 24 44.7         525596    807  Cn7093      
2005 06  09.17404  13 56 08.98   -09 16 55.2   22.3R 525596    304  Cn7093      
2005 06  09.21480  13 56 08.82   -09 16 54.7         525596    304  Cn7093      
2006 04  26.18576  14 03 25.61   -09 58 47.8   21.7R 525596    807  Cr3594      
2006 04  26.27135  14 03 25.23   -09 58 46.1         525596    807  Cr3594      
2006 04  27.16021  14 03 21.41   -09 58 25.9         525596    807  Cr3594      
2006 06  19.98644  14 00 15.43   -09 43 47.7   21.7R 525596    304  Cr4851      
2006 06  20.08067  14 00 15.24   -09 43 46.9         525596    304  Cr4851      
2008 06  06.23704  14 09 50.33   -10 42 07.6   22.6R 525596    688  Cz1384      
2008 06  06.29938  14 09 50.15   -10 42 05.9         525596    688  Cz1384      
2012 04  27.47759  14 30 26.288  -12 41 32.67  23.4G 525596    F51  C~343n      
2012 05  21.38548  14 28 45.223  -12 33 46.54  23.8G 525596    F51  C~343n      
2013 05  09.44827  14 34 05.126  -13 03 27.49  23.7G 525596    F51  C~343n      
2013 05  18.37924  14 33 27.489  -13 00 38.80  22.6G 525596    F51  C~343n      
2013 07  13.27922  14 30 53.282  -12 50 33.44  21.7G 525596    F51  C~343n      
2014 03  27.56838  14 41 29.383  -13 42 31.77  23.3G 525596    F51  C~343n      
2014 04  05.52978  14 40 57.422  -13 39 56.64  23.2G 525596    F51  C~343n      
2014 05  09.38053  14 38 35.779  -13 29 01.56  23.8G 525596    F51  C~343n      
2014 05  21.35200  14 37 45.405  -13 25 19.97  23.5G 525596    F51  C~343n      
2014 05  27.37517  14 37 21.416  -13 23 36.46  23.1G 525596    F51  C~343n      
2014 06  28.30086  14 35 42.446  -13 17 02.37  23.4G 525596    F51  C~343n      
2015 01  22.64885  14 46 55.733  -14 13 21.63  23.8G 525596    F51  C~343n      
2015 03  18.56740  14 46 25.627  -14 09 32.42  23.2G 525596    F51  C~343n      
2015 03  19.51069  14 46 23.028  -14 09 19.82  23.0G 525596    F51  C~343n      
2015 03  19.52327  14 46 23.018  -14 09 19.84  24.0G 525596    F51  C~343n      
2015 03  19.54753  14 46 22.923  -14 09 19.50  22.9G 525596    F51  C~343n      
2015 03  19.56593  14 46 22.885  -14 09 19.18  22.8G 525596    F51  C~343n      
2015 04  24.50743  14 44 10.579  -13 58 57.64  23.6G 525596    F51  C~343n      
2015 04  25.50381  14 44 06.311  -13 58 38.72  22.0G 525596    F51  C~343n      
2015 05  22.42194  14 42 11.092  -13 50 12.30  23.8G 525596    F51  C~343n      
2016 03  06.51964  14 51 18.862  -14 35 54.52  23.6G 525596    F51  C~343n      
2016 03  13.40861  14 51 04.41   -14 34 41.3   22.8R 525596    G37  C~1pPl      
2016 03  13.49687  14 51 04.18   -14 34 40.4         525596    G37  C~1pPl      
2016 04  30.42779  14 48 11.302  -14 21 26.56  23.9G 525596    F51  C~343n      
2016 06  29.28317  14 44 32.716  -14 06 36.72  22.7G 525596    F51  C~343n      
2017 04  27.46219  14 52 54.610  -14 46 39.55  23.1G 525596    F51  C~343n      
2018 03  18.55090  14 59 47.944  -15 20 57.86  23.0G 525596    F51  C~343n      
2018 03  18.56203  14 59 47.887  -15 20 57.53  23.5G 525596    F51  C~343n      
2018 03  18.57312  14 59 47.870  -15 20 57.60  22.9G 525596    F51  C~343n      
2018 04  12.53784  14 58 26.229  -15 14 53.02  23.1G 525596    F51  C~343n      

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    -0.20       0.00    -0.07
     2   0.0002      0.00     0.04       0.00     0.03
     3   0.0798      0.00     0.30       0.00    -0.40
     4   0.0799      0.00    -0.45       0.00    -0.37
     5   0.9587      0.00    -0.03       0.00     0.41
     6   0.9589      0.00    -0.12       0.00     0.19
     7   0.9614      0.00    -0.20       0.00     0.61
     8   1.1087      0.00     0.08       0.00    -0.00
     9   1.1090      0.00     0.19       0.00     0.09
    10   3.0724      0.00     0.18       0.00    -0.65
    11   3.0726      0.00     0.38       0.00     0.22
    12   6.9636      0.00    -0.00       0.00    -0.18
    13   7.0290      0.00     0.02       0.00     0.01
    14   7.9957      0.00     0.14       0.00     0.01
    15   8.0201      0.00    -0.29       0.00    -0.26
    16   8.1732      0.00     0.00       0.00     0.53
    17   8.8776      0.00    -0.06       0.00    -0.14
    18   8.9021      0.00     0.03       0.00    -0.02
    19   8.9948      0.00    -0.17       0.00     0.14
    20   9.0276      0.00    -0.20       0.00    -0.28
    21   9.0441      0.00     0.15       0.00    -0.09
    22   9.1315      0.00    -0.06       0.00     0.10
    23   9.7019      0.00     0.04       0.00    -0.04
    24   9.8523      0.00    -0.18       0.00     0.18
    25   9.8549      0.00    -0.21       0.00    -0.13
    26   9.8549      0.00     0.18       0.00    -0.32
    27   9.8550      0.00    -0.20       0.00    -0.32
    28   9.8550      0.00     0.02       0.00    -0.25
    29   9.9534      0.00     0.23       0.00     0.29
    30   9.9561      0.00     0.17       0.00    -0.05
    31  10.0298      0.00    -0.21       0.00     0.21
    32  10.8213      0.00     0.26       0.00     0.32
    33  10.8402      0.00     0.14       0.00     0.24
    34  10.8404      0.00    -0.10       0.00     0.10
    35  10.9717      0.00     0.06       0.00     0.26
    36  11.1355      0.00    -0.04       0.00    -0.23
    37  11.9629      0.00     0.15       0.00     0.17
    38  12.8529      0.00     0.35       0.00    -0.14
    39  12.8529      0.00    -0.07       0.00     0.06
    40  12.8530      0.00     0.11       0.00    -0.14
    41  12.9213      0.00    -0.56       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.

525596    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        46.575    46.575    46.575
ecceobj         0.114     0.114     0.114
incobj          3.751     3.751     3.751
qmin           40.613    40.601    40.642
qmax           53.600    53.581    53.576
amean          46.925    46.926    46.925
amin           46.530    46.529    46.529
amax           47.358    47.366    47.367
emean           0.118     0.118     0.118
emin            0.105     0.105     0.105
emax            0.132     0.131     0.132
imean           2.436     2.436     2.436
imin            2.020     2.020     2.020
imax            2.867     2.867     2.866
excite_mean     0.125     0.125     0.125
fracstop        1.000     1.000     1.000
cjmean          3.118     3.118     3.118

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       172.3     172.4     172.4
kozaiamp        179.9     180.0     179.9