Orbit Fit and Astrometric record for 10MR116

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: 10MR116   
# Created Wed Dec 25 02:09:04 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     79 observations of     79
# Arc:  17.28y
# First observation: 2000/10/02
#  Last observation: 2018/01/13
# Chi-squared of fit:    88.81 DOF:    152 RMS:  0.19
# Min/Max residuals:    -0.47    0.60
# Exact a, adot, b, bdot, g, gdot:
  1.816065E-05  3.060431E-02  5.284913E-06  1.083303E-02  2.698463E-02  1.597232E-03
# Covariance matrix:
  1.1970E-13 -2.1874E-14  1.3642E-14 -5.4440E-15  1.1096E-14 -2.8419E-14
 -2.1874E-14  6.9811E-15 -5.5534E-15  2.2326E-15 -3.3923E-16  1.1585E-14
  1.3642E-14 -5.5534E-15  8.3118E-14 -7.8955E-15 -8.2606E-16 -1.0107E-14
 -5.4440E-15  2.2326E-15 -7.8955E-15  1.3727E-15  5.6964E-16  4.0734E-15
  1.1096E-14 -3.3923E-16 -8.2606E-16  5.6964E-16  6.0305E-14  1.9510E-15
 -2.8419E-14  1.1585E-14 -1.0107E-14  4.0734E-15  1.9510E-15  2.1094E-14
#      lat0       lon0       xBary       yBary       zBary        JD0
    1.724484   -3.842543   -0.225041    0.028979   -0.968571  2451819.841812
# Heliocentric elements and errors
Epoch:              2451820.5000  =  2000/10/03
Mean Anomaly:            4.05527 +/-     0.001
Argument of Peri:      354.62243 +/-     0.001
Long of Asc Node:      351.76286 +/-     0.000
Inclination:            19.54011 +/-     0.000
Eccentricity:         0.40403873 +/-    0.0000
Semi-Major Axis:     63.51479279 +/-    0.0047
Time of Perihelion: 2449737.7925 +/-       0.4
Perihelion:          37.85235631 +/-    0.0037
Aphelion:            89.17722927 +/-    0.0070
Period (y)              506.1981 +/-      0.06
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           37.94537054 +/-    0.0003
Ecliptic Y           -2.31753250 +/-    0.0000
Ecliptic Z            1.11541126 +/-    0.0000
Ecliptic XDOT         0.00032918 +/-    0.0000
Ecliptic YDOT         0.00309446 +/-    0.0000
Ecliptic ZDOT         0.00110365 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   38.03240000 +/-    0.0003
Geocenter to KBO     37.05813338 +/-    0.0003
# Hcoef:  6.66

The following table shows the complete astrometric record for 10MR116. 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 (10MR116) followed by the observatory code and reference code for the source of the astrometry.

2000 10  02.341069 23 43 09.39   +00 03 19.1   21.4V 10MR116   645  C~2PON      
2000 10  02.341898 23 43 09.39   +00 03 18.9   20.8V 10MR116   645  C~2PON      
2000 10  02.344386 23 43 09.39   +00 03 19.1   22.4V 10MR116   645  C~2PON      
2001 10  14.289923 23 47 42.33   +01 14 21.1   22.1V 10MR116   645  C~2PON      
2001 10  14.290752 23 47 42.34   +01 14 20.8   21.9V 10MR116   645  C~2PON      
2001 10  14.293240 23 47 42.33   +01 14 20.9   22.9V 10MR116   645  C~2PON      
2001 10  15.303021 23 47 37.91   +01 13 56.9   22.3V 10MR116   645  C~2PON      
2001 10  15.303851 23 47 37.89   +01 13 56.9   21.9V 10MR116   645  C~2PON      
2001 10  15.306338 23 47 37.89   +01 13 56.7   23.2V 10MR116   645  C~2PON      
2001 11  12.152017 23 45 59.56   +01 05 06.2   22.4V 10MR116   645  C~2PON      
2001 11  12.152846 23 45 59.56   +01 05 06.3   23.2V 10MR116   645  C~2PON      
2001 11  12.155334 23 45 59.56   +01 05 06.2   23.5V 10MR116   645  C~2PON      
2001 11  18.187600 23 45 45.89   +01 03 55.3   22.4V 10MR116   645  C~2PON      
2001 11  18.188430 23 45 45.90   +01 03 55.3   21.7V 10MR116   645  C~2PON      
2001 11  18.190918 23 45 45.89   +01 03 55.3   23.4V 10MR116   645  C~2PON      
2004 10  15.20937  00 03 48.77   +04 58 33.8   22.0R 10MR116   695  C~1w3i      
2004 10  15.30137  00 03 48.35   +04 58 31.4         10MR116   695  C~1w3i      
2005 09  12.324263 00 11 51.32   +06 26 21.0   22.1V 10MR116   645  C~2PON      
2005 09  12.325092 00 11 51.31   +06 26 20.9   21.9V 10MR116   645  C~2PON      
2005 09  12.327580 00 11 51.30   +06 26 20.8   22.8V 10MR116   645  C~2PON      
2005 09  28.256852 00 10 33.57   +06 19 54.3   22.4V 10MR116   645  C~2PON      
2005 09  28.257681 00 10 33.57   +06 19 54.5   21.8V 10MR116   645  C~2PON      
2005 09  28.260169 00 10 33.58   +06 19 54.5   23.8V 10MR116   645  C~2PON      
2008 11  01.335306 00 24 01.54   +09 42 18.3   22.6V 10MR116   645  C~2PON      
2008 11  01.336136 00 24 01.54   +09 42 18.3   22.2V 10MR116   645  C~2PON      
2008 11  01.338623 00 24 01.54   +09 42 18.3   23.6V 10MR116   645  C~2PON      
2010 06  15.57858  00 40 47.262  +12 12 49.68  22.6w 10MR116   F51  C~1w3i      
2010 06  19.56080  00 40 56.560  +12 14 55.65  22.8w 10MR116   F51  C~1w3i      
2010 06  19.56182  00 40 56.504  +12 14 55.41  22.6w 10MR116   F51  C~1w3i      
2010 10  14.36921  00 36 07.954  +12 11 28.83  22.7G 10MR116   F51  C~36lq      
2010 11  01.28175  00 34 46.426  +12 03 24.48  23.1w 10MR116   F51  C~1w3i      
2010 11  01.29733  00 34 46.361  +12 03 23.91  23.0w 10MR116   F51  C~1w3i      
2010 11  01.31455  00 34 46.282  +12 03 23.44  22.8w 10MR116   F51  C~1w3i      
2010 11  01.33167  00 34 46.225  +12 03 23.18  22.9w 10MR116   F51  C~1w3i      
2011 01  30.23908  00 34 03.392  +11 50 29.75  22.3G 10MR116   F51  C~36lq      
2011 07  01.58876  00 46 29.677  +13 27 15.13  23.3w 10MR116   F51  C~1w3i      
2011 08  10.55778  00 46 03.359  +13 36 43.27  23.4G 10MR116   F51  C~36lq      
2011 09  04.43283  00 44 40.450  +13 34 29.54  22.9w 10MR116   F51  C~1w3i      
2011 09  04.44768  00 44 40.395  +13 34 29.30  22.8w 10MR116   F51  C~1w3i      
2011 09  04.46258  00 44 40.335  +13 34 29.19  22.9w 10MR116   F51  C~1w3i      
2011 09  04.47759  00 44 40.263  +13 34 29.05  22.9w 10MR116   F51  C~1w3i      
2011 09  19.39833  00 43 33.888  +13 30 29.78  22.2i 10MR116   F51  C~1w3i      
2011 10  02.50259  00 42 30.204  +13 25 43.92  22.3g 10MR116   F51  C~1w3i      
2012 10  09.34859  00 47 15.372  +14 30 37.86  22.0w 10MR116   F51  C~1w3i      
2012 10  09.39121  00 47 15.194  +14 30 37.17  22.2w 10MR116   F51  C~1w3i      
2012 11  03.42378  00 45 18.270  +14 19 21.34  21.7i 10MR116   F51  C~1w3i      
2012 11  04.24796  00 45 14.840  +14 18 58.92  22.5w 10MR116   F51  C~1w3i      
2012 11  04.26208  00 45 14.773  +14 18 58.59  22.6w 10MR116   F51  C~1w3i      
2012 11  04.27616  00 45 14.712  +14 18 58.20  22.7w 10MR116   F51  C~1w3i      
2012 11  04.29034  00 45 14.645  +14 18 57.75  22.6w 10MR116   F51  C~1w3i      
2013 09  15.54642  00 54 34.053  +15 45 53.13  22.3w 10MR116   F51  C~1w3i      
2013 09  15.56014  00 54 33.969  +15 45 52.91  22.3w 10MR116   F51  C~1w3i      
2014 06  30.58666  01 02 09.776  +16 41 01.24  22.7G 10MR116   F51  C~36lq      
2014 06  30.59061  01 02 09.818  +16 41 00.84  22.7G 10MR116   F51  C~36lq      
2014 06  30.59456  01 02 09.800  +16 41 00.91  22.7G 10MR116   F51  C~36lq      
2014 06  30.59850  01 02 09.811  +16 41 01.11  22.3G 10MR116   F51  C~36lq      
2014 09  13.59653  01 00 05.728  +16 51 47.71  23.5G 10MR116   F51  C~36lq      
2014 09  19.52054  00 59 39.011  +16 50 19.33  23.0G 10MR116   F51  C~36lq      
2014 09  19.53306  00 59 38.955  +16 50 18.85  22.8G 10MR116   F51  C~36lq      
2014 09  19.54516  00 59 38.902  +16 50 18.72  22.7G 10MR116   F51  C~36lq      
2014 09  19.55726  00 59 38.830  +16 50 18.43  22.4G 10MR116   F51  C~36lq      
2015 07  25.55618  01 07 39.121  +17 53 36.43  23.0G 10MR116   F51  C~36lq      
2015 07  25.56976  01 07 39.126  +17 53 37.06  23.2G 10MR116   F51  C~36lq      
2015 07  25.58340  01 07 39.110  +17 53 37.02  22.7G 10MR116   F51  C~36lq      
2015 07  25.59714  01 07 39.097  +17 53 37.30  22.3G 10MR116   F51  C~36lq      
2016 10  25.45235  01 07 25.223  +18 44 22.31  22.5G 10MR116   F51  C~36lq      
2016 10  25.46505  01 07 25.174  +18 44 21.95  22.1G 10MR116   F51  C~36lq      
2016 10  25.47764  01 07 25.101  +18 44 21.64  22.2G 10MR116   F51  C~36lq      
2016 10  25.49017  01 07 25.024  +18 44 21.39  23.2G 10MR116   F51  C~36lq      
2017 08  26.39016  01 17 17.096  +20 01 27.40  22.5G 10MR116   F51  C~36lq      
2017 08  26.61495  01 17 16.371  +20 01 27.65  22.5G 10MR116   F51  C~36lq      
2017 08  27.38668  01 17 14.020  +20 01 28.17  22.3G 10MR116   F51  C~36lq      
2017 09  21.56794  01 15 34.931  +19 58 33.91  23.3G 10MR116   F51  C~36lq      
2017 09  21.58186  01 15 34.904  +19 58 33.60  23.3G 10MR116   F51  C~36lq      
2017 09  21.59573  01 15 34.817  +19 58 33.79  22.6G 10MR116   F51  C~36lq      
2017 09  21.60961  01 15 34.754  +19 58 33.24  22.6G 10MR116   F51  C~36lq      
2017 10  28.31556  01 12 34.931  +19 45 18.77  22.4G 10MR116   F51  C~36lq      
2018 01  01.27040  01 09 33.589  +19 19 17.37  22.9G 10MR116   F51  C~36lq      
2018 01  13.22101  01 09 41.042  +19 17 21.71  24.0G 10MR116   F51  C~36lq      

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    -0.13       0.00     0.18
     2   0.0000      0.00    -0.07       0.00     0.00
     3   0.0000      0.00     0.11       0.00     0.27
     4   1.0320      0.00    -0.05       0.00     0.18
     5   1.0320      0.00     0.16       0.00    -0.10
     6   1.0320      0.00     0.18       0.00     0.06
     7   1.0348      0.00     0.27       0.00    -0.06
     8   1.0348      0.00     0.03       0.00    -0.04
     9   1.0348      0.00     0.19       0.00    -0.18
    10   1.1110      0.00    -0.18       0.00    -0.23
    11   1.1111      0.00    -0.15       0.00    -0.12
    12   1.1111      0.00    -0.05       0.00    -0.19
    13   1.1276      0.00    -0.05       0.00    -0.09
    14   1.1276      0.00     0.13       0.00    -0.08
    15   1.1276      0.00     0.06       0.00    -0.05
    16   4.0352      0.00    -0.25       0.00     0.09
    17   4.0355      0.00    -0.19       0.00     0.05
    18   4.9445      0.00     0.07       0.00    -0.00
    19   4.9445      0.00    -0.02       0.00    -0.08
    20   4.9445      0.00     0.01       0.00    -0.13
    21   4.9881      0.00    -0.12       0.00    -0.28
    22   4.9881      0.00    -0.06       0.00    -0.06
    23   4.9881      0.00     0.28       0.00     0.00
    24   8.0821      0.00     0.14       0.00    -0.04
    25   8.0821      0.00     0.19       0.00    -0.02
    26   8.0821      0.00     0.34       0.00     0.05
    27   9.7009      0.00    -0.47       0.00     0.32
    28   9.7118      0.00     0.60       0.00     0.11
    29   9.7118      0.00    -0.27       0.00    -0.16
    30  10.0316      0.00    -0.01       0.00    -0.00
    31  10.0806      0.00     0.08       0.00     0.32
    32  10.0806      0.00     0.11       0.00     0.16
    33  10.0807      0.00     0.03       0.00     0.15
    34  10.0807      0.00     0.27       0.00     0.35
    35  10.3269      0.00    -0.04       0.00    -0.00
    36  10.7440      0.00     0.06       0.00    -0.14
    37  10.8534      0.00    -0.07       0.00    -0.41
    38  10.9215      0.00    -0.10       0.00     0.05
    39  10.9216      0.00     0.01       0.00    -0.00
    40  10.9216      0.00     0.05       0.00     0.07
    41  10.9217      0.00    -0.08       0.00     0.11
    42  10.9625      0.00    -0.15       0.00     0.18
    43  10.9984      0.00    -0.41       0.00     0.28
    44  12.0192      0.00    -0.30       0.00    -0.09
    45  12.0193      0.00     0.25       0.00     0.30
    46  12.0878      0.00    -0.17       0.00    -0.08
    47  12.0901      0.00    -0.08       0.00     0.01
    48  12.0901      0.00    -0.19       0.00     0.06
    49  12.0902      0.00    -0.21       0.00     0.06
    50  12.0902      0.00    -0.31       0.00    -0.01
    51  12.9533      0.00     0.04       0.00     0.17
    52  12.9534      0.00    -0.27       0.00     0.17
    53  13.7419      0.00    -0.35       0.00     0.38
    54  13.7420      0.00     0.18       0.00    -0.14
    55  13.7420      0.00    -0.18       0.00    -0.19
    56  13.7420      0.00    -0.11       0.00    -0.11
    57  13.9473      0.00    -0.02       0.00     0.18
    58  13.9635      0.00    -0.10       0.00     0.05
    59  13.9636      0.00    -0.05       0.00    -0.23
    60  13.9636      0.00     0.01       0.00    -0.16
    61  13.9636      0.00    -0.22       0.00    -0.25
    62  14.8096      0.00     0.03       0.00    -0.03
    63  14.8097      0.00     0.22       0.00     0.35
    64  14.8097      0.00     0.11       0.00     0.06
    65  14.8097      0.00     0.04       0.00     0.09
    66  16.0633      0.00    -0.03       0.00    -0.04
    67  16.0633      0.00     0.17       0.00    -0.06
    68  16.0633      0.00    -0.00       0.00    -0.02
    69  16.0634      0.00    -0.24       0.00     0.07
    70  16.8981      0.00     0.13       0.00    -0.06
    71  16.8988      0.00    -0.11       0.00    -0.09
    72  16.9009      0.00     0.35       0.00    -0.13
    73  16.9698      0.00    -0.00       0.00    -0.17
    74  16.9699      0.00     0.57       0.00    -0.28
    75  16.9699      0.00     0.23       0.00     0.11
    76  16.9699      0.00     0.26       0.00    -0.24
    77  17.0704      0.00     0.03       0.00    -0.33
    78  17.2483      0.00     0.25       0.00    -0.21
    79  17.2810      0.00    -0.29       0.00     0.31

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.

10MR116    quality flag:3

Type:       SCATNEAR  SCATNEAR  SCATNEAR

axisobj        63.740    63.740    63.740
ecceobj         0.406     0.406     0.406
incobj         19.523    19.523    19.523
qmin           36.487    36.613    36.622
qmax           90.858    90.571    90.612
amean          62.634    62.634    62.636
amin           61.607    61.626    61.587
amax           63.951    63.912    63.920
emean           0.399     0.398     0.398
emin            0.381     0.381     0.381
emax            0.421     0.417     0.418
imean          19.978    20.046    20.011
imin           19.249    19.266    19.223
imax           20.589    20.585    20.548
excite_mean     0.525     0.525     0.525
fracstop        1.000     1.000     1.000
cjmean          2.965     2.966     2.966

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       154.2     158.9     157.3
kozaiamp        180.0     180.0     180.0