Orbit Fit and Astrometric record for 613412

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: 613412    
# Created Wed Dec 25 02:07:43 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     41 observations of     41
# Arc:  10.94y
# First observation: 2006/04/27
#  Last observation: 2017/04/04
# Chi-squared of fit:    54.76 DOF:     76 RMS:  0.20
# Min/Max residuals:    -0.55    0.61
# Exact a, adot, b, bdot, g, gdot:
  1.636925E-05  2.324238E-02 -3.056465E-06 -6.676615E-03  2.274871E-02 -8.548982E-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
    0.197206 -139.896302    0.058808    0.003558   -1.000283  2453852.737254
# Heliocentric elements and errors
Epoch:              2453852.5000  =  2006/04/27
Mean Anomaly:          343.78525 +/-     0.000
Argument of Peri:      236.75042 +/-     0.000
Long of Asc Node:       40.70141 +/-     0.000
Inclination:            16.00047 +/-     0.000
Eccentricity:         0.54225014 +/-    0.0000
Semi-Major Axis:     82.27283705 +/-    0.0000
Time of Perihelion: 2466129.4589 +/-       0.0
Perihelion:          37.66037981 +/-    0.0000
Aphelion:           126.88529429 +/-    0.0000
Period (y)              746.2647 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -34.42881396 +/-    0.0000
Ecliptic Y          -28.91956687 +/-    0.0000
Ecliptic Z            0.15116704 +/-    0.0000
Ecliptic XDOT         0.00259058 +/-    0.0000
Ecliptic YDOT        -0.00148428 +/-    0.0000
Ecliptic ZDOT        -0.00080711 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   44.96366215 +/-    0.0000
Geocenter to KBO     43.95882955 +/-    0.0000
# Hcoef:  7.00

The following table shows the complete astrometric record for 613412. 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 (613412) followed by the observatory code and reference code for the source of the astrometry.

2006 04  27.23650  14 31 01.72   -14 39 35.0   21.8R 613412    807  Cr3609      
2006 04  27.38137  14 31 01.08   -14 39 32.5         613412    807  Cr3609      
2006 04  28.16137  14 30 57.61   -14 39 18.5         613412    807  Cr3609      
2006 06  19.99374  14 27 33.87   -14 26 26.3   23.0R 613412    304  Cr4858      
2006 06  20.08726  14 27 33.62   -14 26 25.5         613412    304  Cr4858      
2006 08  21.02251  14 27 23.55   -14 29 48.2   22.0R 613412    807  Cs2782      
2006 08  22.02112  14 27 26.01   -14 30 04.1         613412    807  Cs2782      
2006 08  23.02379  14 27 28.55   -14 30 20.2         613412    807  Cs2782      
2007 06  16.00204  14 32 29.36   -15 14 11.9         613412    304  Cy6786      
2007 06  16.07550  14 32 29.14   -15 14 11.0         613412    304  Cy6786      
2007 07  15.02400  14 31 32.26   -15 11 26.4         613412    304  Cy6786      
2007 07  16.05277  14 31 31.46   -15 11 26.1         613412    304  Cy6786      
2008 05  03.30278  14 40 14.79   -16 12 31.7         613412    695  Cz0452      
2008 05  03.34326  14 40 14.62   -16 12 31.0         613412    695  Cz0452      
2012 05  14.40873  15 00 14.351  -19 23 14.06  22.8G 613412    F51  C~3442      
2012 05  19.38645  14 59 50.761  -19 21 55.78  23.7G 613412    F51  C~3442      
2012 05  20.37215  14 59 46.143  -19 21 40.12  23.6G 613412    F51  C~3442      
2012 06  08.30901  14 58 23.231  -19 16 53.09  22.9G 613412    F51  C~3442      
2013 06  01.35873  15 04 24.441  -20 07 43.66  23.2G 613412    F51  C~3442      
2013 06  01.37354  15 04 24.378  -20 07 43.43  23.6G 613412    F51  C~3442      
2013 06  01.38835  15 04 24.316  -20 07 42.89  23.0G 613412    F51  C~3442      
2014 04  30.47476  15 12 40.088  -21 04 48.19  23.0G 613412    F51  C~3442      
2014 05  08.46770  15 12 01.042  -21 02 57.85  22.4G 613412    F51  C~3442      
2014 05  08.47979  15 12 00.986  -21 02 57.74  23.2G 613412    F51  C~3442      
2014 05  08.49191  15 12 00.934  -21 02 57.91  23.2G 613412    F51  C~3442      
2014 05  08.50402  15 12 00.874  -21 02 57.65  23.5G 613412    F51  C~3442      
2014 05  20.37838  15 11 02.566  -21 00 02.19  23.7G 613412    F51  C~3442      
2014 05  20.38970  15 11 02.518  -21 00 02.04  22.7G 613412    F51  C~3442      
2014 05  20.40100  15 11 02.460  -21 00 01.66  24.0G 613412    F51  C~3442      
2014 05  20.41229  15 11 02.395  -21 00 01.58  22.8G 613412    F51  C~3442      
2014 07  01.31536  15 08 12.760  -20 50 28.29  23.4G 613412    F51  C~3442      
2014 07  01.32665  15 08 12.763  -20 50 27.89  22.8G 613412    F51  C~3442      
2014 07  01.34920  15 08 12.682  -20 50 27.41  22.9G 613412    F51  C~3442      
2015 03  30.64199  15 20 43.791  -21 58 16.33  23.2G 613412    F51  C~3442      
2015 05  20.10263  15 16 56.47   -21 49 24.5         613412    W84  C~1Tit      
2015 05  21.10791  15 16 51.50   -21 49 09.8   24.1V 613412    W84  C~1Tit      
2015 05  24.10031  15 16 36.80   -21 48 25.6         613412    W84  C~1Tit      
2015 06  11.34848  15 15 12.689  -21 43 58.14  22.9G 613412    F51  C~3442      
2016 03  07.61127  15 27 37.070  -22 46 10.53  22.4G 613412    F51  C~3442      
2016 05  07.48265  15 23 57.678  -22 41 19.37  22.7G 613412    F51  C~3442      
2017 04  04.51099  15 32 38.845  -23 34 38.89  22.8G 613412    F51  C~3442      

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    -0.15       0.00    -0.30
     2   0.0004      0.00     0.06       0.00    -0.35
     3   0.0025      0.00    -0.05       0.00     0.04
     4   0.1472      0.00    -0.04       0.00     0.10
     5   0.1474      0.00    -0.02       0.00     0.09
     6   0.3170      0.00    -0.06       0.00    -0.10
     7   0.3197      0.00     0.04       0.00    -0.06
     8   0.3225      0.00    -0.01       0.00     0.23
     9   1.1356      0.00    -0.11       0.00     0.11
    10   1.1358      0.00    -0.01       0.00     0.24
    11   1.2150      0.00     0.29       0.00     0.06
    12   1.2178      0.00     0.46       0.00     0.21
    13   2.0180      0.00    -0.44       0.00    -0.03
    14   2.0181      0.00    -0.17       0.00    -0.02
    15   6.0484      0.00     0.11       0.00     0.19
    16   6.0620      0.00     0.11       0.00    -0.14
    17   6.0647      0.00     0.15       0.00    -0.04
    18   6.1166      0.00     0.25       0.00     0.52
    19   7.0968      0.00     0.06       0.00    -0.26
    20   7.0969      0.00     0.12       0.00    -0.25
    21   7.0969      0.00     0.20       0.00     0.06
    22   8.0089      0.00     0.02       0.00    -0.01
    23   8.0307      0.00    -0.12       0.00     0.14
    24   8.0308      0.00    -0.05       0.00     0.08
    25   8.0308      0.00     0.08       0.00    -0.26
    26   8.0308      0.00     0.09       0.00    -0.18
    27   8.0634      0.00    -0.18       0.00    -0.29
    28   8.0634      0.00    -0.06       0.00    -0.31
    29   8.0634      0.00    -0.10       0.00    -0.10
    30   8.0635      0.00    -0.23       0.00    -0.19
    31   8.1782      0.00    -0.55       0.00    -0.19
    32   8.1782      0.00    -0.02       0.00     0.10
    33   8.1783      0.00    -0.25       0.00     0.34
    34   8.9238      0.00    -0.03       0.00     0.25
    35   9.0619      0.00     0.17       0.00     0.04
    36   9.0647      0.00     0.18       0.00    -0.01
    37   9.0729      0.00     0.15       0.00     0.01
    38   9.1228      0.00    -0.20       0.00    -0.07
    39   9.8628      0.00    -0.09       0.00     0.10
    40  10.0294      0.00     0.19       0.00    -0.35
    41  10.9385      0.00     0.16       0.00     0.61

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.

613412    quality flag:3

Type:       SCATNEAR  SCATNEAR  SCATNEAR

axisobj        80.249    80.248    80.250
ecceobj         0.533     0.533     0.533
incobj         16.087    16.087    16.087
qmin           36.737    36.741    36.655
qmax          128.384   128.550   128.593
amean          81.134    81.337    81.345
amin           79.844    79.965    80.020
amax           83.074    83.045    83.161
emean           0.534     0.535     0.534
emin            0.520     0.522     0.521
emax            0.547     0.548     0.548
imean          15.786    15.856    15.865
imin           15.073    15.125    15.101
imax           16.627    16.674    16.743
excite_mean     0.599     0.600     0.600
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       184.7     181.7     183.8
kozaiamp        179.9     180.0     179.9