Orbit Fit and Astrometric record for 541132

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: 541132    
# Created Mon Apr 28 01:07:33 2025
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     34 observations of     36
# Arc:  13.03y
# First observation: 2005/10/05
#  Last observation: 2018/10/17
# Chi-squared of fit:    39.01 DOF:     62 RMS:  0.19
# Min/Max residuals:    -0.38    0.56
# Exact a, adot, b, bdot, g, gdot:
 -3.155294E-05  9.996029E-03 -8.928641E-06  1.054571E-03  1.200939E-02 -5.406457E-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
   10.192289    0.170960   -0.206946    0.174005   -0.967287  2453648.743714
# Heliocentric elements and errors
Epoch:              2453648.5000  =  2005/10/05
Mean Anomaly:          359.18716 +/-     0.000
Argument of Peri:      118.26744 +/-     0.000
Long of Asc Node:      301.03675 +/-     0.000
Inclination:            11.67693 +/-     0.000
Eccentricity:         0.93627616 +/-    0.0000
Semi-Major Axis:   1016.91544385 +/-    0.0000
Time of Perihelion: 2480392.5570 +/-       0.0
Perihelion:          64.80175383 +/-    0.0000
Aphelion:          1969.02913387 +/-    0.0000
Period (y)            32429.1426 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           82.93206078 +/-    0.0000
Ecliptic Y            0.45014584 +/-    0.0000
Ecliptic Z           14.73378770 +/-    0.0000
Ecliptic XDOT        -0.00126037 +/-    0.0000
Ecliptic YDOT         0.00226854 +/-    0.0000
Ecliptic ZDOT         0.00001854 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   84.23249358 +/-    0.0000
Geocenter to KBO     83.26883238 +/-    0.0000
# Hcoef:  5.51

The following table shows the complete astrometric record for 541132. 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 (541132) followed by the observatory code and reference code for the source of the astrometry.

2005 10  05.242971 23 44 15.71   +09 24 40.3         541132    695  C~8qjb      
2005 10  05.249322 23 44 15.67   +09 24 40.3         541132    695  C~8qjb      
2015 10  13.255661 00 05 33.685  +12 21 12.16  24.0G 541132    T09  C~2lVV      
2015 10  13.341162 00 05 33.486  +12 21 10.71  24.0G 541132    T09  C~2lVV      
2015 10  13.487574 00 05 33.145  +12 21 08.31  24.0G 541132    T09  C~2lVV      
2015 12  07.03832  00 04 10.961  +12 07 26.32  24.3r 541132    304  C~2lVV      
2015 12  09.07673  00 04 10.197  +12 07 04.63  24.2r 541132    304  C~2lVV      
2016 09  25.16349  00 08 33.733  +12 44 17.33  24.0r 541132    304  C~2lVV      
2016 09  25.24466  00 08 33.531  +12 44 16.25  24.1r 541132    304  C~2lVV      
2016 09  26.11520  00 08 31.404  +12 44 03.50  24.0r 541132    304  C~2lVV      
2016 09  28.23197  00 08 26.240  +12 43 31.76  24.1r 541132    304  C~2lVV      
2016 10  01.23767  00 08 18.913  +12 42 46.07  24.0r 541132    304  C~2lVV      
2016 11  02.12125  00 07 08.649  +12 33 58.44        541132    304  C~2lVV      
2016 11  03.05868  00 07 06.943  +12 33 42.54  24.2r 541132    304  C~2lVV      
2016 12  30.06127  00 06 30.754  +12 22 47.03  24.3r 541132    304  C~2lVV      
2017 09  21.18143  00 11 04.641  +13 03 56.62  24.2R 541132    G37  C~2lVV      
2017 09  21.18871  00 11 04.623  +13 03 56.15  24.1R 541132    G37  C~2lVV      
2017 09  21.23762  00 11 04.505  +13 03 55.69  24.2R 541132    G37  C~2lVV      
2017 09  21.25991  00 11 04.451  +13 03 55.12  24.1R 541132    G37  C~2lVV      
2017 09  22.14910  00 11 02.269  +13 03 42.62  24.0R 541132    G37  C~2lVV      
2017 12  13.05631  00 08 44.228  +12 43 11.02        541132    304  C~2lVV      
2017 12  14.05111  00 08 44.094  +12 43 01.20        541132    304  C~2lVV      
2018 05  16.41893  00 14 31.482  +13 13 23.50  24.3r 541132    304  C~2lVV      
2018 05  19.42075  00 14 37.764  +13 14 25.34  24.2r 541132    304  C~2lVV      
2018 10  15.991030 00 12 27.49   +13 16 19.2   24.4r 541132    950  C~2nvw      
2018 10  16.937686 00 12 25.30   +13 16 03.4   24.7r 541132    950  C~2nvw      
2018 10  16.946484 00 12 25.26   +13 16 03.3   24.6r 541132    950  C~2nvw      
2018 10  16.955674 00 12 25.24   +13 16 03.2   24.5r 541132    950  C~2nvw      
2018 10  17.917361 00 12 23.03   +13 15 46.9   24.8r 541132    950  C~2nvw      
2018 10  17.922245 00 12 23.02   +13 15 46.8   24.6r 541132    950  C~2nvw      
2018 10  17.926727 00 12 23.02   +13 15 46.7   24.7r 541132    950  C~2nvw      
2018 10  17.933141 00 12 23.01   +13 15 46.6   24.9r 541132    950  C~2nvw      
2018 10  17.937832 00 12 23.00   +13 15 46.4   25.0r 541132    950  C~2nvw      
2018 10  17.952652 00 12 22.95   +13 15 46.1   24.8r 541132    950  C~2nvw      
2018 10  17.957695 00 12 22.95   +13 15 46.0   25.1r 541132    950  C~2nvw      
2018 10  20.215602 00 12 17.892  +13 15 07.50        541132    275  S~7mm3      

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 (   7.69)      0.00 (   5.67)
     2   0.0000      0.00 (   7.30)      0.00 (   5.76)
     3  10.0206      0.00    -0.11       0.00     0.10
     4  10.0208      0.00    -0.10       0.00     0.06
     5  10.0212      0.00    -0.09       0.00     0.09
     6  10.1706      0.00    -0.06       0.00     0.25
     7  10.1761      0.00     0.04       0.00    -0.05
     8  10.9731      0.00    -0.05       0.00    -0.15
     9  10.9733      0.00    -0.05       0.00    -0.04
    10  10.9757      0.00    -0.12       0.00     0.01
    11  10.9815      0.00     0.07       0.00    -0.12
    12  10.9897      0.00     0.01       0.00     0.18
    13  11.0770      0.00     0.14       0.00     0.19
    14  11.0796      0.00     0.21       0.00    -0.21
    15  11.2356      0.00     0.00       0.00     0.13
    16  11.9615      0.00    -0.01       0.00     0.14
    17  11.9615      0.00    -0.01       0.00    -0.23
    18  11.9617      0.00     0.04       0.00    -0.02
    19  11.9617      0.00     0.06       0.00    -0.28
    20  11.9642      0.00    -0.04       0.00    -0.38
    21  12.1884      0.00     0.24       0.00     0.14
    22  12.1911      0.00     0.39       0.00    -0.32
    23  12.6110      0.00     0.35       0.00    -0.19
    24  12.6192      0.00     0.39       0.00    -0.18
    25  13.0287      0.00     0.17       0.00    -0.08
    26  13.0313      0.00     0.06       0.00     0.11
    27  13.0314      0.00    -0.23       0.00     0.16
    28  13.0314      0.00    -0.21       0.00     0.21
    29  13.0340      0.00    -0.34       0.00     0.20
    30  13.0340      0.00    -0.32       0.00     0.18
    31  13.0340      0.00    -0.16       0.00     0.15
    32  13.0341      0.00    -0.09       0.00     0.16
    33  13.0341      0.00    -0.07       0.00     0.04
    34  13.0341      0.00    -0.31       0.00    -0.01
    35  13.0341      0.00    -0.13       0.00    -0.02
    36  13.0403      0.00     0.56       0.00    -0.17

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.

541132    quality flag:3

Type:       SCATNEAR  SCATNEAR  SCATNEAR

axisobj      1415.896  1415.675  1416.118
ecceobj         0.954     0.954     0.954
incobj         11.674    11.674    11.674
qmin           51.996    51.998    51.994
qmax         2864.174  2766.322  2767.217
amean        1120.287  1119.405  1120.116
amin          963.571   986.760   989.715
amax         1464.571  1415.672  1416.115
emean           0.942     0.942     0.942
emin            0.929     0.929     0.930
emax            0.956     0.954     0.954
imean          13.234    13.232    13.233
imin           12.569    12.547    12.552
imax           14.038    14.050    14.048
excite_mean     0.969     0.969     0.969
fracstop        1.000     1.000     1.000
cjmean          4.012     4.012     4.012

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       118.7     118.6     118.6
kozaiamp          6.4       6.3       6.5