Orbit Fit and Astrometric record for 15RT245

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: 15RT245   
# Created Wed Dec 25 02:10:23 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     81 observations of     81
# Arc:   7.03y
# First observation: 2013/09/11
#  Last observation: 2020/09/21
# Chi-squared of fit:    19.61 DOF:    156 RMS:  0.09
# Min/Max residuals:    -0.19    0.35
# Exact a, adot, b, bdot, g, gdot:
  1.479762E-05  2.448345E-02  8.510576E-08  3.437368E-04  2.451291E-02  1.628313E-03
# Covariance matrix:
  1.3123E-13 -5.9167E-14  7.0809E-16 -5.5695E-16  1.3123E-14 -2.7168E-13
 -5.9167E-14  4.4845E-14 -6.2623E-16  5.5344E-16  1.7465E-14  2.6710E-13
  7.0809E-16 -6.2623E-16  7.8642E-14 -2.2448E-14 -1.4741E-16 -4.5990E-15
 -5.5695E-16  5.5344E-16 -2.2448E-14  8.3760E-15  2.6560E-16  4.0524E-15
  1.3123E-14  1.7465E-14 -1.4741E-16  2.6560E-16  6.8733E-14  1.2250E-13
 -2.7168E-13  2.6710E-13 -4.5990E-15  4.0524E-15  1.2250E-13  1.9562E-12
#      lat0       lon0       xBary       yBary       zBary        JD0
    0.526676    3.209789    0.257960    0.009050   -0.973876  2456546.774958
# Heliocentric elements and errors
Epoch:              2456546.5000  =  2013/09/11
Mean Anomaly:           40.92637 +/-     0.023
Argument of Peri:      344.67329 +/-     0.030
Long of Asc Node:      330.52018 +/-     0.008
Inclination:             0.96147 +/-     0.000
Eccentricity:         0.08300116 +/-    0.0001
Semi-Major Axis:     44.40986965 +/-    0.0020
Time of Perihelion: 2444257.4468 +/-       7.0
Perihelion:          40.72379889 +/-    0.0030
Aphelion:            48.09594042 +/-    0.0032
Period (y)              295.9562 +/-      0.02
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           41.71561217 +/-    0.0004
Ecliptic Y            2.08413882 +/-    0.0000
Ecliptic Z            0.37497364 +/-    0.0000
Ecliptic XDOT         0.00002193 +/-    0.0000
Ecliptic YDOT         0.00273926 +/-    0.0000
Ecliptic ZDOT         0.00004020 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   41.76928801 +/-    0.0004
Geocenter to KBO     40.79482037 +/-    0.0004
# Hcoef:  6.59

The following table shows the complete astrometric record for 15RT245. 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 (15RT245) followed by the observatory code and reference code for the source of the astrometry.

2013 09  11.27418  00 10 56.662  +01 45 34.36  23.6g 15RT245   W84  C~4yYK      
2013 10  12.12193  00 08 40.808  +01 30 58.07  22.5i 15RT245   W84  C~4yYK      
2013 10  12.12613  00 08 40.788  +01 30 57.84  22.2z 15RT245   W84  C~4yYK      
2013 10  13.09058  00 08 36.713  +01 30 31.33  21.8z 15RT245   W84  C~4yYK      
2013 10  13.11626  00 08 36.604  +01 30 30.68  22.5i 15RT245   W84  C~4yYK      
2013 10  28.06092  00 07 37.630  +01 24 05.10  22.9r 15RT245   W84  C~4yYK      
2013 10  28.06231  00 07 37.624  +01 24 04.91  22.5i 15RT245   W84  C~4yYK      
2013 11  22.12208  00 06 26.473  +01 16 12.71  22.7z 15RT245   W84  C~4yYK      
2013 11  23.08993  00 06 24.631  +01 16 00.17  22.9r 15RT245   W84  C~4yYK      
2013 11  23.09132  00 06 24.633  +01 16 00.00  22.7i 15RT245   W84  C~4yYK      
2014 11  13.09178  00 11 52.179  +01 52 49.88  22.7z 15RT245   W84  C~4yYK      
2015 06  23.57027  00 23 38.936  +03 09 10.33  22.3r 15RT245   568  C~2Gdr      
2015 07  14.58775  00 23 46.573  +03 10 22.10  23.1r 15RT245   568  C~2Gdr      
2015 07  19.56683  00 23 42.860  +03 10 03.34  23.2r 15RT245   568  C~2Gdr      
2015 08  11.46704  00 23 00.440  +03 05 51.56  22.9r 15RT245   568  C~2Gdr      
2015 08  11.51159  00 23 00.315  +03 05 50.85  22.4r 15RT245   568  C~2Gdr      
2015 09  08.37633  00 21 23.022  +02 55 42.29  22.9r 15RT245   568  C~2Gdr      
2015 09  08.48053  00 21 22.585  +02 55 39.56  22.8r 15RT245   568  C~2Gdr      
2015 09  08.52274  00 21 22.408  +02 55 38.43  22.9r 15RT245   568  C~2Gdr      
2015 09  09.49961  00 21 18.356  +02 55 12.71  23.2w 15RT245   568  C~2Gdr      
2015 09  10.44054  00 21 14.432  +02 54 47.78  22.4w 15RT245   568  C~2Gdr      
2015 09  16.42148  00 20 48.886  +02 52 05.40  23.1w 15RT245   568  C~2Gdr      
2015 10  03.33607  00 19 33.849  +02 44 04.67  22.1r 15RT245   568  C~2Gdr      
2015 10  03.34821  00 19 33.795  +02 44 04.26  23.0w 15RT245   568  C~2Gdr      
2015 10  03.40228  00 19 33.548  +02 44 02.69  22.5w 15RT245   568  C~2Gdr      
2015 10  07.28650  00 19 16.334  +02 42 11.63  22.8r 15RT245   568  C~2Gdr      
2015 10  07.31809  00 19 16.186  +02 42 10.78  22.8r 15RT245   568  C~2Gdr      
2015 10  07.37159  00 19 15.946  +02 42 09.24  22.0r 15RT245   568  C~2Gdr      
2015 11  05.24319  00 17 20.830  +02 29 39.24  22.6w 15RT245   568  C~2Gdr      
2015 11  07.07312  00 17 14.788  +02 28 59.77  23.1r 15RT245   W84  C~4yYK      
2015 11  07.07451  00 17 14.778  +02 28 59.93  23.1i 15RT245   W84  C~4yYK      
2015 11  07.21299  00 17 14.340  +02 28 56.56  22.2w 15RT245   568  C~2Gdr      
2015 11  07.26547  00 17 14.164  +02 28 55.46  22.4w 15RT245   568  C~2Gdr      
2015 11  08.31016  00 17 10.814  +02 28 33.55  23.1w 15RT245   568  C~2Gdr      
2015 11  08.37107  00 17 10.629  +02 28 32.10  23.4w 15RT245   568  C~2Gdr      
2015 11  10.33048  00 17 04.542  +02 27 51.91  22.8w 15RT245   568  C~2Gdr      
2015 11  10.34252  00 17 04.506  +02 27 51.69  22.5w 15RT245   568  C~2Gdr      
2015 12  07.28927  00 16 09.609  +02 21 40.81  21.8w 15RT245   568  C~2Gdr      
2016 01  01.21869  00 16 14.402  +02 21 54.37  22.8w 15RT245   568  C~2Gdr      
2016 09  05.54890  00 26 35.982  +03 30 33.47        15RT245   568  C~2Gdr      
2016 09  05.55294  00 26 35.962  +03 30 33.39        15RT245   568  C~2Gdr      
2016 09  07.48826  00 26 28.143  +03 29 44.14        15RT245   568  C~2Gdr      
2016 09  07.49232  00 26 28.142  +03 29 43.99        15RT245   568  C~2Gdr      
2016 09  07.53459  00 26 27.955  +03 29 42.98        15RT245   568  C~2Gdr      
2016 09  07.53863  00 26 27.934  +03 29 42.84        15RT245   568  C~2Gdr      
2016 09  10.267488 00 26 16.69   +03 28 32.0   22.5i 15RT245   W84  C~352k      
2016 09  10.26801  00 26 16.690  +03 28 31.98  22.5i 15RT245   W84  C~4yYK      
2016 09  10.32270  00 26 16.464  +03 28 30.67  23.2r 15RT245   W84  C~4yYK      
2016 09  10.32409  00 26 16.447  +03 28 30.61  24.1g 15RT245   W84  C~4yYK      
2016 09  26.56094  00 25 05.822  +03 21 01.21  23.3w 15RT245   568  C~2Gdr      
2016 09  26.57548  00 25 05.750  +03 21 00.83  23.2w 15RT245   568  C~2Gdr      
2016 11  03.22971  00 22 28.757  +03 04 05.37        15RT245   568  C~2Gdr      
2016 11  18.10756  00 21 43.488  +02 59 06.51  22.6i 15RT245   W84  C~4yYK      
2016 11  18.10895  00 21 43.488  +02 59 06.43  22.8r 15RT245   W84  C~4yYK      
2016 11  30.09555  00 21 18.472  +02 56 17.68  23.1r 15RT245   W84  C~4yYK      
2016 11  30.09692  00 21 18.469  +02 56 17.50  22.7i 15RT245   W84  C~4yYK      
2016 11  30.09830  00 21 18.482  +02 56 18.01  23.5g 15RT245   W84  C~4yYK      
2016 12  04.085660 00 21 12.73   +02 55 37.8   22.5z 15RT245   W84  C~352k      
2016 12  04.08619  00 21 12.736  +02 55 37.80  22.6z 15RT245   W84  C~4yYK      
2016 12  24.23886  00 21 05.243  +02 54 34.82  23.3w 15RT245   568  C~2Gdr      
2016 12  24.25172  00 21 05.254  +02 54 34.90  23.3w 15RT245   568  C~2Gdr      
2017 01  02.23941  00 21 13.839  +02 55 23.69  23.4w 15RT245   568  C~2Gdr      
2017 01  26.22433  00 22 11.532  +03 01 19.98  23.2w 15RT245   568  C~2Gdr      
2017 01  27.25017  00 22 15.043  +03 01 42.07  23.1w 15RT245   568  C~2Gdr      
2017 01  27.25763  00 22 15.074  +03 01 42.21  23.1w 15RT245   568  C~2Gdr      
2017 01  28.24596  00 22 18.538  +03 02 04.04  23.2w 15RT245   568  C~2Gdr      
2017 01  28.25342  00 22 18.554  +03 02 04.19  23.3w 15RT245   568  C~2Gdr      
2017 08  22.31770  00 32 32.136  +04 09 43.11  22.7i 15RT245   W84  C~4yYK      
2017 08  22.318542 00 32 32.15   +04 09 43.2   22.9r 15RT245   W84  C~352k      
2017 08  22.31907  00 32 32.148  +04 09 43.16  22.8r 15RT245   W84  C~4yYK      
2017 10  22.167280 00 28 19.42   +03 43 01.3   22.9r 15RT245   W84  C~352k      
2017 10  22.16780  00 28 19.424  +03 43 01.29  23.0r 15RT245   W84  C~4yYK      
2017 10  22.168646 00 28 19.42   +03 43 01.5   23.7g 15RT245   W84  C~352k      
2017 10  22.16918  00 28 19.415  +03 43 01.39  23.4g 15RT245   W84  C~4yYK      
2017 10  29.135671 00 27 51.71   +03 40 01.4   22.6z 15RT245   W84  C~352k      
2017 10  29.13620  00 27 51.710  +03 40 01.39  22.5z 15RT245   W84  C~4yYK      
2019 10  26.112210 00 38 12.227  +04 48 36.09  22.9G 15RT245   G37  C~3ctf      
2019 10  26.180800 00 38 11.950  +04 48 34.27        15RT245   G37  C~3ctf      
2019 10  26.297610 00 38 11.465  +04 48 31.28        15RT245   G37  C~3ctf      
2020 09  21.290000 00 45 44.905  +05 37 33.17  22.9G 15RT245   G37  C~4AD9      
2020 09  21.366330 00 45 44.556  +05 37 31.18        15RT245   G37  C~4AD9      

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     0.18       0.00     0.11
     2   0.0845      0.00    -0.03       0.00     0.06
     3   0.0845      0.00    -0.06       0.00    -0.05
     4   0.0871      0.00     0.01       0.00     0.00
     5   0.0872      0.00     0.03       0.00     0.06
     6   0.1281      0.00     0.03       0.00     0.06
     7   0.1281      0.00     0.02       0.00    -0.10
     8   0.1967      0.00    -0.04       0.00     0.12
     9   0.1994      0.00    -0.10       0.00     0.05
    10   0.1994      0.00    -0.03       0.00    -0.10
    11   1.1713      0.00    -0.00       0.00     0.07
    12   1.7804      0.00     0.05       0.00    -0.09
    13   1.8380      0.00     0.02       0.00    -0.01
    14   1.8516      0.00    -0.03       0.00    -0.03
    15   1.9143      0.00    -0.07       0.00    -0.08
    16   1.9144      0.00    -0.09       0.00    -0.06
    17   1.9907      0.00    -0.05       0.00     0.04
    18   1.9910      0.00    -0.03       0.00     0.03
    19   1.9911      0.00    -0.02       0.00     0.01
    20   1.9938      0.00    -0.05       0.00    -0.04
    21   1.9963      0.00    -0.03       0.00    -0.04
    22   2.0127      0.00     0.06       0.00     0.03
    23   2.0590      0.00    -0.01       0.00     0.03
    24   2.0591      0.00     0.00       0.00    -0.03
    25   2.0592      0.00    -0.02       0.00    -0.05
    26   2.0698      0.00     0.13       0.00    -0.01
    27   2.0699      0.00     0.03       0.00     0.04
    28   2.0701      0.00     0.04       0.00     0.02
    29   2.1491      0.00     0.17       0.00    -0.13
    30   2.1541      0.00     0.11       0.00    -0.02
    31   2.1541      0.00     0.03       0.00     0.17
    32   2.1545      0.00     0.07       0.00    -0.06
    33   2.1547      0.00     0.03       0.00    -0.04
    34   2.1575      0.00    -0.04       0.00     0.10
    35   2.1577      0.00     0.15       0.00    -0.08
    36   2.1631      0.00    -0.07       0.00    -0.10
    37   2.1631      0.00    -0.05       0.00    -0.08
    38   2.2369      0.00     0.01       0.00    -0.09
    39   2.3051      0.00     0.03       0.00    -0.09
    40   2.9850      0.00    -0.03       0.00    -0.02
    41   2.9850      0.00    -0.09       0.00     0.00
    42   2.9903      0.00    -0.12       0.00     0.03
    43   2.9903      0.00     0.12       0.00    -0.02
    44   2.9904      0.00    -0.04       0.00     0.06
    45   2.9905      0.00    -0.11       0.00     0.02
    46   2.9979      0.00    -0.02       0.00     0.03
    47   2.9979      0.00     0.01       0.00     0.02
    48   2.9981      0.00     0.10       0.00     0.15
    49   2.9981      0.00    -0.07       0.00     0.13
    50   3.0425      0.00    -0.02       0.00    -0.11
    51   3.0426      0.00    -0.11       0.00    -0.08
    52   3.1457      0.00     0.04       0.00     0.02
    53   3.1864      0.00     0.03       0.00     0.06
    54   3.1864      0.00     0.08       0.00     0.00
    55   3.2192      0.00     0.00       0.00    -0.01
    56   3.2192      0.00    -0.01       0.00    -0.18
    57   3.2192      0.00     0.22       0.00     0.35
    58   3.2301      0.00    -0.14       0.00    -0.19
    59   3.2301      0.00    -0.04       0.00    -0.19
    60   3.2853      0.00    -0.11       0.00    -0.06
    61   3.2854      0.00    -0.03       0.00    -0.01
    62   3.3100      0.00    -0.01       0.00    -0.00
    63   3.3756      0.00     0.04       0.00     0.00
    64   3.3784      0.00    -0.05       0.00    -0.01
    65   3.3785      0.00     0.03       0.00    -0.03
    66   3.3812      0.00     0.01       0.00     0.01
    67   3.3812      0.00    -0.15       0.00    -0.00
    68   3.9454      0.00    -0.10       0.00    -0.00
    69   3.9454      0.00     0.16       0.00     0.10
    70   3.9454      0.00     0.15       0.00     0.07
    71   4.1120      0.00     0.02       0.00     0.05
    72   4.1120      0.00     0.11       0.00     0.06
    73   4.1120      0.00     0.11       0.00     0.29
    74   4.1120      0.00     0.07       0.00     0.19
    75   4.1310      0.00     0.08       0.00     0.01
    76   4.1310      0.00     0.11       0.00     0.01
    77   6.1214      0.00    -0.12       0.00    -0.14
    78   6.1216      0.00    -0.01       0.00    -0.16
    79   6.1219      0.00    -0.00       0.00    -0.09
    80   7.0281      0.00     0.09       0.00     0.04
    81   7.0283      0.00    -0.12       0.00     0.10

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.

15RT245    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        44.674    44.674    44.674
ecceobj         0.088     0.088     0.088
incobj          0.958     0.958     0.958
qmin           40.008    40.013    40.003
qmax           49.132    49.125    49.139
amean          44.444    44.444    44.444
amin           44.088    44.086    44.090
amax           44.832    44.832    44.830
emean           0.081     0.081     0.081
emin            0.066     0.066     0.066
emax            0.097     0.096     0.097
imean           2.452     2.452     2.452
imin            1.770     1.770     1.770
imax            3.000     3.000     3.000
excite_mean     0.092     0.092     0.092
fracstop        1.000     1.000     1.000
cjmean          3.096     3.096     3.096

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       181.2     181.2     181.2
kozaiamp        180.0     179.9     180.0