Orbit Fit and Astrometric record for 612217

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: 612217    
# Created Sun Nov 24 02:07:39 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     64 observations of     64
# Arc:  23.02y
# First observation: 2001/04/26
#  Last observation: 2024/05/04
# Chi-squared of fit:   114.41 DOF:    122 RMS:  0.24
# Min/Max residuals:    -0.72    0.43
# Exact a, adot, b, bdot, g, gdot:
  1.498961E-05  2.255081E-02 -7.704333E-07 -7.108926E-04  2.371961E-02  8.178076E-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
    2.373958 -143.491693    0.008971    0.041819   -1.011515  2452025.564443
# Heliocentric elements and errors
Epoch:              2452026.5000  =  2001/04/27
Mean Anomaly:          108.77278 +/-     0.000
Argument of Peri:       14.81015 +/-     0.000
Long of Asc Node:       88.52631 +/-     0.000
Inclination:             2.94005 +/-     0.000
Eccentricity:         0.04080913 +/-    0.0000
Semi-Major Axis:     42.54377210 +/-    0.0000
Time of Perihelion: 2421401.9187 +/-       0.0
Perihelion:          40.80759758 +/-    0.0000
Aphelion:            44.27994663 +/-    0.0000
Period (y)              277.4995 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -34.67224935 +/-    0.0000
Ecliptic Y          -25.65095033 +/-    0.0000
Ecliptic Z            1.74624811 +/-    0.0000
Ecliptic XDOT         0.00146168 +/-    0.0000
Ecliptic YDOT        -0.00214775 +/-    0.0000
Ecliptic ZDOT        -0.00007788 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   43.16460858 +/-    0.0000
Geocenter to KBO     42.15920811 +/-    0.0000
# Hcoef:  6.55

The following table shows the complete astrometric record for 612217. 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 (612217) followed by the observatory code and reference code for the source of the astrometry.

2001 04  26.06370  14 19 54.61   -11 26 46.0   22.7R 612217    809  Cd0940      
2001 04  26.06370  14 19 54.61   -11 26 46.1   21.7R 612217    I03  Cl0812      
2001 04  26.17021  14 19 54.12   -11 26 44.0   21.5R 612217    I03  Cl0812      
2001 04  26.17021  14 19 54.12   -11 26 43.3         612217    809  Cd0940      
2001 04  26.29482  14 19 53.52   -11 26 41.6   21.8R 612217    I03  Cl0812      
2001 04  26.29482  14 19 53.52   -11 26 40.6         612217    809  Cd0940      
2001 04  26.40156  14 19 53.06   -11 26 38.2         612217    809  Cd0940      
2001 04  27.13784  14 19 49.70   -11 26 21.4         612217    809  Cd0940      
2001 04  27.30981  14 19 48.91   -11 26 17.5         612217    809  Cd0940      
2001 04  27.36375  14 19 48.66   -11 26 16.2         612217    809  Cd0940      
2001 05  25.21555  14 17 47.24   -11 16 33.1         612217    309  Cd1312      
2001 05  25.22042  14 17 47.22   -11 16 33.0         612217    309  Cd1312      
2001 05  25.22712  14 17 47.20   -11 16 32.9   23. R 612217    309  Cd1312      
2003 06  01.01684  14 27 12.24   -12 09 18.5   21.6R 612217    807  Ci2655      
2003 06  01.10585  14 27 11.90   -12 09 16.9         612217    807  Ci2655      
2003 07  06.27623  14 25 36.68   -12 03 10.6   22.7R 612217    568  Ci2655      
2003 07  06.34710  14 25 36.61   -12 03 10.5         612217    568  Ci2655      
2007 05  03.51003  14 49 08.37   -14 03 16.1   22.8R 612217    250  S~06AP      
2007 05  03.51698  14 49 08.34   -14 03 16.0         612217    250  S~06AP      
2007 05  03.52392  14 49 08.30   -14 03 15.9         612217    250  S~06AP      
2007 05  03.53087  14 49 08.27   -14 03 15.7         612217    250  S~06AP      
2007 05  08.24318  14 48 46.51   -14 01 39.6   22.2R 612217    304  Cu8806      
2007 05  08.28983  14 48 46.27   -14 01 38.6         612217    304  Cu8806      
2013 05  08.43408  15 18 49.142  -16 25 19.69  22.7G 612217    F51  C~36iU      
2013 05  08.44817  15 18 49.076  -16 25 19.41  22.9G 612217    F51  C~36iU      
2013 05  08.46225  15 18 49.002  -16 25 19.15  22.7G 612217    F51  C~36iU      
2013 05  08.47639  15 18 48.925  -16 25 18.99  22.4G 612217    F51  C~36iU      
2013 06  04.41508  15 16 45.262  -16 17 47.64  23.2G 612217    F51  C~36iU      
2014 03  14.62089  15 27 12.610  -17 00 42.55  22.5G 612217    F51  C~36iU      
2014 04  30.46155  15 24 30.532  -16 50 00.35  22.5G 612217    F51  C~36iU      
2014 05  08.47847  15 23 53.289  -16 47 42.89  22.7G 612217    F51  C~36iU      
2014 05  08.49059  15 23 53.235  -16 47 42.18  21.8G 612217    F51  C~36iU      
2014 05  08.50270  15 23 53.179  -16 47 42.33  22.7G 612217    F51  C~36iU      
2014 05  08.51482  15 23 53.113  -16 47 42.20  22.7G 612217    F51  C~36iU      
2014 07  26.28985  15 19 19.463  -16 32 53.87  23.5G 612217    F51  C~36iU      
2015 05  22.26927  15 27 53.60   -17 05 49.4   23.1V 612217    W84  C~1TiY      
2015 05  23.18226  15 27 49.35   -17 05 34.7         612217    W84  C~1TiY      
2015 05  24.18154  15 27 44.68   -17 05 18.6         612217    W84  C~1TiY      
2015 05  24.42140  15 27 43.557  -17 05 15.13  22.3G 612217    F51  C~36iU      
2015 05  24.43291  15 27 43.524  -17 05 15.10  22.4G 612217    F51  C~36iU      
2015 05  24.44441  15 27 43.451  -17 05 14.85  23.6G 612217    F51  C~36iU      
2015 05  24.45589  15 27 43.351  -17 05 14.65  23.1G 612217    F51  C~36iU      
2015 05  25.40962  15 27 38.927  -17 04 59.40  22.8G 612217    F51  C~36iU      
2015 06  11.35307  15 26 23.678  -17 00 47.00  22.3G 612217    F51  C~36iU      
2015 07  19.27725  15 24 28.279  -16 55 07.21  22.8G 612217    F51  C~36iU      
2016 05  07.46249  15 34 05.458  -17 31 04.45  22.1G 612217    F51  C~36iU      
2016 05  07.47357  15 34 05.439  -17 31 04.37  22.7G 612217    F51  C~36iU      
2016 05  07.48464  15 34 05.390  -17 31 04.06  23.5G 612217    F51  C~36iU      
2017 03  25.58696  15 41 56.387  -18 01 32.45  23.2G 612217    F51  C~36iU      
2017 04  26.49180  15 40 03.022  -17 54 48.24  23.6G 612217    F51  C~36iU      
2017 04  26.50300  15 40 02.957  -17 54 48.18  23.2G 612217    F51  C~36iU      
2017 04  26.51420  15 40 02.912  -17 54 48.04  22.8G 612217    F51  C~36iU      
2017 04  26.52543  15 40 02.866  -17 54 47.81  23.4G 612217    F51  C~36iU      
2017 05  19.41549  15 38 16.599  -17 48 53.67  22.6G 612217    F51  C~36iU      
2017 05  19.42688  15 38 16.532  -17 48 53.52  23.6G 612217    F51  C~36iU      
2017 05  19.43826  15 38 16.498  -17 48 52.80  22.4G 612217    F51  C~36iU      
2017 05  19.44969  15 38 16.437  -17 48 53.05  22.7G 612217    F51  C~36iU      
2017 07  15.33886  15 34 38.488  -17 37 59.69  23.4G 612217    F51  C~36iU      
2018 05  19.43222  15 43 25.129  -18 09 23.32  21.6G 612217    F51  C~36iU      
2018 05  19.44412  15 43 25.098  -18 09 23.60  22.1G 612217    F51  C~36iU      
2018 05  19.45605  15 43 25.038  -18 09 23.26  22.5G 612217    F51  C~36iU      
2018 05  19.46795  15 43 24.984  -18 09 22.88  22.6G 612217    F51  C~36iU      
2024 05  04.362520 16 15 29.608  -20 03 02.40  22.7G 612217    G37  C~838o      
2024 05  04.397680 16 15 29.436  -20 03 01.92        612217    G37  C~838o      

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     0.03       0.00     0.05
     2   0.0000      0.00     0.03       0.00     0.15
     3   0.0003      0.00     0.08       0.00     0.43
     4   0.0003      0.00     0.08       0.00    -0.27
     5   0.0006      0.00    -0.24       0.00     0.28
     6   0.0006      0.00    -0.24       0.00    -0.72
     7   0.0009      0.00     0.25       0.00     0.22
     8   0.0029      0.00     0.06       0.00     0.25
     9   0.0034      0.00     0.19       0.00     0.23
    10   0.0036      0.00     0.17       0.00     0.29
    11   0.0798      0.00     0.08       0.00     0.33
    12   0.0798      0.00     0.08       0.00     0.34
    13   0.0798      0.00     0.18       0.00     0.32
    14   2.0971      0.00     0.01       0.00    -0.26
    15   2.0973      0.00     0.08       0.00    -0.12
    16   2.1936      0.00    -0.35       0.00    -0.48
    17   2.1938      0.00     0.19       0.00    -0.64
    18   6.0190      0.00    -0.37       0.00    -0.31
    19   6.0190      0.00    -0.34       0.00    -0.35
    20   6.0191      0.00    -0.46       0.00    -0.40
    21   6.0191      0.00    -0.43       0.00    -0.34
    22   6.0320      0.00     0.39       0.00     0.11
    23   6.0321      0.00     0.07       0.00     0.16
    24  12.0339      0.00     0.11       0.00    -0.05
    25  12.0339      0.00     0.14       0.00    -0.02
    26  12.0339      0.00     0.04       0.00    -0.01
    27  12.0340      0.00    -0.10       0.00    -0.10
    28  12.1077      0.00     0.15       0.00    -0.34
    29  12.8831      0.00     0.13       0.00     0.20
    30  13.0114      0.00     0.42       0.00    -0.18
    31  13.0333      0.00     0.02       0.00    -0.13
    32  13.0333      0.00     0.08       0.00     0.37
    33  13.0334      0.00     0.11       0.00     0.01
    34  13.0334      0.00    -0.02       0.00    -0.07
    35  13.2491      0.00     0.07       0.00    -0.06
    36  14.0704      0.00    -0.59       0.00     0.24
    37  14.0729      0.00    -0.12       0.00     0.16
    38  14.0756      0.00     0.03       0.00     0.16
    39  14.0763      0.00     0.01       0.00    -0.06
    40  14.0763      0.00     0.34       0.00    -0.21
    41  14.0763      0.00     0.07       0.00    -0.15
    42  14.0764      0.00    -0.62       0.00    -0.13
    43  14.0790      0.00    -0.30       0.00    -0.15
    44  14.1254      0.00    -0.13       0.00    -0.09
    45  14.2292      0.00    -0.33       0.00    -0.01
    46  15.0319      0.00    -0.33       0.00    -0.04
    47  15.0319      0.00     0.17       0.00    -0.14
    48  15.0320      0.00     0.23       0.00    -0.01
    49  15.9138      0.00    -0.07       0.00     0.10
    50  16.0012      0.00     0.27       0.00     0.11
    51  16.0012      0.00     0.04       0.00     0.01
    52  16.0012      0.00     0.12       0.00    -0.02
    53  16.0013      0.00     0.18       0.00     0.04
    54  16.0639      0.00     0.03       0.00    -0.12
    55  16.0640      0.00    -0.15       0.00    -0.15
    56  16.0640      0.00     0.17       0.00     0.40
    57  16.0640      0.00     0.09       0.00    -0.03
    58  16.2198      0.00     0.07       0.00    -0.27
    59  17.0633      0.00    -0.29       0.00     0.42
    60  17.0633      0.00     0.12       0.00    -0.03
    61  17.0634      0.00     0.08       0.00     0.13
    62  17.0634      0.00     0.14       0.00     0.33
    63  23.0234      0.00     0.06       0.00     0.03
    64  23.0235      0.00    -0.14       0.00     0.12

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.

612217    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        42.467    42.467    42.467
ecceobj         0.040     0.040     0.040
incobj          2.939     2.939     2.939
qmin           39.523    39.516    39.521
qmax           46.311    46.323    46.288
amean          42.772    42.772    42.772
amin           42.437    42.439    42.436
amax           43.121    43.124    43.115
emean           0.050     0.050     0.050
emin            0.028     0.028     0.028
emax            0.074     0.074     0.074
imean           1.340     1.340     1.340
imin            0.056     0.056     0.056
imax            2.393     2.393     2.393
excite_mean     0.056     0.056     0.056
fracstop        1.000     1.000     1.000
cjmean          3.083     3.083     3.083

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       171.1     171.1     171.2
kozaiamp        180.0     180.0     179.9