Orbit Fit and Astrometric record for 506439

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: 506439    
# Created Wed Dec 25 02:07:11 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     36 observations of     36
# Arc:  17.01y
# First observation: 2000/12/16
#  Last observation: 2017/12/20
# Chi-squared of fit:   119.78 DOF:     66 RMS:  0.32
# Min/Max residuals:    -1.01    0.68
# Exact a, adot, b, bdot, g, gdot:
  1.625216E-05  2.707331E-02  2.206479E-06  3.257685E-04  2.660484E-02  4.560529E-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
   -3.837469   55.948865   -0.473081   -0.057513   -0.855014  2451894.767073
# Heliocentric elements and errors
Epoch:              2451894.5000  =  2000/12/16
Mean Anomaly:           59.87367 +/-     0.000
Argument of Peri:      217.88296 +/-     0.000
Long of Asc Node:      135.56979 +/-     0.000
Inclination:             3.82202 +/-     0.000
Eccentricity:         0.03265989 +/-    0.0000
Semi-Major Axis:     39.06012687 +/-    0.0000
Time of Perihelion: 2437064.8041 +/-       0.0
Perihelion:          37.78442744 +/-    0.0000
Aphelion:            40.33582631 +/-    0.0000
Period (y)              244.1230 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           21.09120716 +/-    0.0000
Ecliptic Y           32.05267699 +/-    0.0000
Ecliptic Z           -2.51548763 +/-    0.0000
Ecliptic XDOT        -0.00228891 +/-    0.0000
Ecliptic YDOT         0.00160483 +/-    0.0000
Ecliptic ZDOT         0.00003048 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   38.45178103 +/-    0.0000
Geocenter to KBO     37.58718617 +/-    0.0000
# Hcoef:  7.06

The following table shows the complete astrometric record for 506439. 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 (506439) followed by the observatory code and reference code for the source of the astrometry.

2000 12  16.26633  03 38 15.33   +15 30 41.2   22.4R 506439    695  Cc4111      
2000 12  16.35374  03 38 14.93   +15 30 40.1   22.3R 506439    695  Cc4111      
2000 12  16.38591  03 38 14.78   +15 30 39.8   22.2R 506439    695  Cc4111      
2000 12  18.09808  03 38 06.81   +15 30 18.1         506439    695  Cc4111      
2001 02  14.84637  03 36 05.09   +15 28 43.3         506439    950  Cc6738      
2001 02  16.85280  03 36 07.14   +15 29 03.4   22.2R 506439    950  Cc6738      
2001 09  19.41135  03 51 07.08   +16 16 21.1         506439    695  Cd5779      
2001 09  19.46490  03 51 06.97   +16 16 20.5         506439    695  Cd5779      
2001 09  21.43870  03 51 03.04   +16 15 57.6         506439    290  Cd5779      
2001 09  21.48613  03 51 02.93   +16 15 57.0         506439    290  Cd5779      
2001 10  21.32125  03 49 22.02   +16 08 34.0         506439    696  Cd9166      
2001 10  21.35896  03 49 21.88   +16 08 32.8   22.3R 506439    696  Cd9166      
2001 12  13.08442  03 44 48.38   +15 53 44.8         506439    950  Ce3555      
2001 12  13.14503  03 44 48.08   +15 53 44.0         506439    950  Ce3555      
2003 12  21.167282 03 56 46.12   +16 34 38.2   22.5V 506439    645  C~1PqX      
2003 12  21.168111 03 56 46.12   +16 34 38.2   22.0V 506439    645  C~1PqX      
2003 12  21.170599 03 56 46.11   +16 34 38.2   23.1V 506439    645  C~1PqX      
2004 11  20.30587  04 05 43.59   +17 01 27.5   22.5R 506439    568  Cm0397      
2004 11  20.36370  04 05 43.27   +17 01 26.8         506439    568  Cm0397      
2004 11  21.37478  04 05 37.73   +17 01 11.3         506439    568  Cm0397      
2008 09  10.14754  04 34 50.38   +18 25 11.5   25.4R 506439    250  S~06AO      
2008 09  10.15379  04 34 50.38   +18 25 11.4         506439    250  S~06AO      
2008 09  10.16004  04 34 50.39   +18 25 11.5         506439    250  S~06AO      
2008 09  10.21560  04 34 50.37   +18 25 11.1         506439    250  S~06AO      
2015 02  18.12244  05 02 58.58   +19 31 15.7   24.7R 506439    695  C~1M60      
2015 02  18.16654  05 02 58.53   +19 31 15.7         506439    695  C~1M60      
2015 02  18.21444  05 02 58.48   +19 31 15.9         506439    695  C~1M60      
2017 10  21.53957  05 30 39.897  +20 08 10.49        506439    568  C~2PjQ      
2017 10  21.54352  05 30 39.883  +20 08 10.46        506439    568  C~2PjQ      
2017 10  27.51948  05 30 21.428  +20 07 36.99        506439    568  C~2PjQ      
2017 11  17.45228  05 28 53.870  +20 05 39.48  22.7w 506439    568  C~2XLd      
2017 11  21.51758  05 28 33.500  +20 05 17.46  22.7w 506439    568  C~2XLd      
2017 12  16.33062  05 26 17.063  +20 03 20.93  22.7w 506439    568  C~2XLd      
2017 12  16.33862  05 26 17.027  +20 03 20.89  22.7w 506439    568  C~2XLd      
2017 12  20.42628  05 25 53.894  +20 03 05.71  22.6R 506439    G37  C~2VU7      
2017 12  20.48802  05 25 53.550  +20 03 06.02        506439    G37  C~2VU7      

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    -0.41
     2   0.0002      0.00     0.28       0.00    -0.39
     3   0.0003      0.00     0.31       0.00    -0.28
     4   0.0050      0.00    -1.01       0.00    -0.79
     5   0.1659      0.00     0.39       0.00    -0.01
     6   0.1714      0.00     0.27       0.00    -0.01
     7   0.7588      0.00     0.00       0.00     0.56
     8   0.7589      0.00    -0.06       0.00     0.55
     9   0.7643      0.00    -0.10       0.00     0.30
    10   0.7645      0.00    -0.21       0.00     0.26
    11   0.8461      0.00    -0.58       0.00     0.68
    12   0.8462      0.00    -0.09       0.00     0.13
    13   0.9906      0.00     0.11       0.00    -0.06
    14   0.9908      0.00     0.15       0.00    -0.04
    15   3.0114      0.00     0.51       0.00    -0.22
    16   3.0114      0.00     0.57       0.00    -0.21
    17   3.0114      0.00     0.60       0.00    -0.19
    18   3.9289      0.00    -0.61       0.00    -0.29
    19   3.9291      0.00    -0.58       0.00    -0.12
    20   3.9319      0.00    -0.44       0.00    -0.11
    21   7.7341      0.00     0.03       0.00     0.26
    22   7.7341      0.00     0.02       0.00     0.19
    23   7.7341      0.00     0.16       0.00     0.32
    24   7.7343      0.00    -0.23       0.00     0.20
    25  14.1735      0.00    -0.28       0.00     0.35
    26  14.1736      0.00    -0.28       0.00     0.18
    27  14.1737      0.00    -0.22       0.00     0.19
    28  16.8467      0.00     0.00       0.00    -0.11
    29  16.8468      0.00    -0.04       0.00    -0.12
    30  16.8631      0.00    -0.13       0.00    -0.22
    31  16.9204      0.00     0.04       0.00    -0.09
    32  16.9316      0.00     0.02       0.00    -0.10
    33  16.9995      0.00    -0.03       0.00    -0.14
    34  16.9995      0.00     0.12       0.00    -0.15
    35  17.0107      0.00     0.17       0.00    -0.23
    36  17.0109      0.00     0.26       0.00     0.32

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.

506439    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        39.053    39.053    39.053
ecceobj         0.034     0.034     0.034
incobj          3.823     3.823     3.823
qmin           36.500    36.503    36.468
qmax           41.257    41.258    41.256
amean          38.786    38.786    38.787
amin           38.500    38.498    38.501
amax           39.088    39.089    39.088
emean           0.037     0.037     0.037
emin            0.011     0.011     0.011
emax            0.057     0.057     0.057
imean           2.347     2.347     2.347
imin            0.317     0.317     0.317
imax            3.782     3.783     3.780
excite_mean     0.058     0.058     0.058
fracstop        1.000     1.000     1.000
cjmean          3.043     3.043     3.043

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       180.0     179.8     180.0
kozaiamp        180.0     180.0     180.0