Orbit Fit and Astrometric record for 23RS61

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: 23RS61    
# Created Sun Dec 22 02:11:25 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     63 observations of     64
# Arc:   9.24y
# First observation: 2015/09/05
#  Last observation: 2024/12/02
# Chi-squared of fit:   197.88 DOF:    120 RMS:  0.31
# Min/Max residuals:    -0.95    0.95
# Exact a, adot, b, bdot, g, gdot:
  2.084527E-05  1.002464E-01  8.027894E-06  3.270084E-02  7.457754E-02 -2.993614E-02
# Covariance matrix:
  1.4046E-09 -8.8490E-08  5.0288E-10 -6.9697E-08 -9.2895E-10 -9.4389E-07
 -8.8490E-08  6.6581E-06 -3.1623E-08  4.4173E-06  5.8364E-08  5.9981E-05
  5.0288E-10 -3.1623E-08  1.8084E-10 -2.5114E-08 -3.3279E-10 -3.3775E-07
 -6.9697E-08  4.4173E-06 -2.5114E-08  4.5805E-06  4.6013E-08  4.7658E-05
 -9.2895E-10  5.8364E-08 -3.3279E-10  4.6013E-08  6.1492E-10  6.2263E-07
 -9.4389E-07  5.9981E-05 -3.3775E-07  4.7658E-05  6.2263E-07  6.4934E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
   -8.705837  -37.477855   -0.338662   -0.144133   -0.942289  2457270.572529
# Heliocentric elements and errors
Epoch:              2457270.5000  =  2015/09/05
Mean Anomaly:          242.07255 +/-     0.001
Argument of Peri:      120.19694 +/-     0.000
Long of Asc Node:      346.98499 +/-     0.000
Inclination:            19.99877 +/-     0.000
Eccentricity:         0.32541619 +/-    0.0000
Semi-Major Axis:     11.79417180 +/-    0.0000
Time of Perihelion: 2462116.8191 +/-       0.0
Perihelion:           7.95615735 +/-    0.0000
Aphelion:            15.63218626 +/-    0.0000
Period (y)               40.5051 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           11.47767912 +/-    0.0000
Ecliptic Y           -8.37634108 +/-    0.0000
Ecliptic Z           -2.02947714 +/-    0.0000
Ecliptic XDOT         0.00151944 +/-    0.0000
Ecliptic YDOT         0.00346457 +/-    0.0000
Ecliptic ZDOT         0.00135306 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   14.35343797 +/-    0.0000
Geocenter to KBO     13.40898897 +/-    0.0000
# Hcoef: 11.25

The following table shows the complete astrometric record for 23RS61. 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 (23RS61) followed by the observatory code and reference code for the source of the astrometry.

2015 09  05.07174  21 51 41.98   -22 13 00.5   24.6V 23RS61    W84  C~7Mwd      
2015 09  05.14618  21 51 40.93   -22 13 03.1         23RS61    W84  C~7Mwd      
2015 09  05.21860  21 51 39.94   -22 13 05.5         23RS61    W84  C~7Mwd      
2020 09  15.396392 23 40 30.534  +01 43 09.85  22.0w 23RS61    F51  C~7Mwd      
2020 09  15.423414 23 40 30.100  +01 43 08.32  22.9w 23RS61    F51  C~7Mwd      
2020 09  15.436911 23 40 29.882  +01 43 07.36  22.5w 23RS61    F51  C~7Mwd      
2021 09  05.600402 00 11 07.642  +08 21 10.38  22.4G 23RS61    T09  C~7Mwd      
2021 09  06.606889 00 10 52.664  +08 20 24.07  22.5G 23RS61    T09  C~7Mwd      
2023 09  15.425595 01 20 42.390  +22 58 32.88  21.9w 23RS61    F52  C~7BxE      
2023 09  15.438514 01 20 42.159  +22 58 32.86  21.8w 23RS61    F52  C~7BxE      
2023 09  15.451309 01 20 41.992  +22 58 32.89  21.6w 23RS61    F52  C~7BxE      
2023 09  15.464389 01 20 41.752  +22 58 32.80  21.7w 23RS61    F52  C~7BxE      
2023 10  05.334106 01 15 00.385  +22 50 51.10  21.6w 23RS61    F51  C~7BxE      
2023 10  05.354694 01 14 59.988  +22 50 50.39  21.9w 23RS61    F51  C~7BxE      
2023 10  05.365019 01 14 59.794  +22 50 49.65  22.0w 23RS61    F51  C~7BxE      
2023 10  07.26739  01 14 24.21   +22 49 14.8   21.0R 23RS61    691  C~7BxE      
2023 10  07.27832  01 14 23.95   +22 49 14.4   21.1R 23RS61    691  C~7BxE      
2023 10  07.28926  01 14 23.76   +22 49 12.8   21.1R 23RS61    691  C~7BxE      
2023 10  07.374926 01 14 22.154  +22 49 09.37  21.3G 23RS61    F52  C~7BxE      
2023 10  07.375736 01 14 22.148  +22 49 09.01  20.9G 23RS61    F52  C~7BxE      
2023 10  10.268156 01 13 27.541  +22 46 29.50  21.0G 23RS61    G96  C~7BxE      
2023 10  10.273336 01 13 27.419  +22 46 29.24  20.6G 23RS61    G96  C~7BxE      
2023 10  10.279466 01 13 27.311  +22 46 27.77  20.5G 23RS61    G96  C~7BxE      
2023 10  10.286606 01 13 27.116  +22 46 27.55  20.4G 23RS61    G96  C~7BxE      
2023 10  22.25116  01 09 40.23   +22 32 33.4   20.8R 23RS61    691  C~7Mwd      
2023 10  22.29180  01 09 39.45   +22 32 30.2   21.0R 23RS61    691  C~7Mwd      
2023 10  23.42807  01 09 18.23   +22 30 58.2   21.5R 23RS61    691  C~7Mwd      
2023 10  23.44384  01 09 17.91   +22 30 57.5   21.2R 23RS61    691  C~7Mwd      
2023 10  23.45960  01 09 17.61   +22 30 56.0   21.4R 23RS61    691  C~7Mwd      
2023 11  10.259905 01 04 09.415  +22 03 56.75  21.8w 23RS61    F52  C~7RSd      
2023 11  10.270398 01 04 09.210  +22 03 55.55  21.7w 23RS61    F52  C~7RSd      
2023 11  10.291216 01 04 08.895  +22 03 53.37  21.5w 23RS61    F52  C~7RSd      
2024 09  01.533181 02 12 37.026  +30 27 29.46  21.1w 23RS61    F52  C~8DsV      
2024 09  01.543718 02 12 36.941  +30 27 30.52  21.2w 23RS61    F52  C~8DsV      
2024 09  01.554291 02 12 36.864  +30 27 31.60  21.3w 23RS61    F52  C~8DsV      
2024 09  01.564916 02 12 36.787  +30 27 32.62  21.2w 23RS61    F52  C~8DsV      
2024 09  29.581535 02 06 42.895  +30 54 26.26  21.3w 23RS61    F51  C~8Hed      
2024 09  29.595350 02 06 42.630  +30 54 26.54  21.4w 23RS61    F51  C~8Hed      
2024 09  29.608998 02 06 42.393  +30 54 26.81  21.4w 23RS61    F51  C~8Hed      
2024 09  29.622616 02 06 42.164  +30 54 26.84  21.5w 23RS61    F51  C~8Hed      
2024 10  10.334042 02 03 20.969  +30 54 18.69  21.0w 23RS61    F51  C~8Hed      
2024 10  10.345848 02 03 20.715  +30 54 18.62  21.0w 23RS61    F51  C~8Hed      
2024 10  10.357701 02 03 20.488  +30 54 18.42  21.3w 23RS61    F51  C~8Hed      
2024 10  10.369859 02 03 20.259  +30 54 18.57  21.1w 23RS61    F51  C~8Hed      
2024 10  22.459113 01 59 09.893  +30 47 16.28  20.9w 23RS61    F51  C~8Mns      
2024 10  22.471258 01 59 09.634  +30 47 15.74  21.2w 23RS61    F51  C~8Mns      
2024 10  22.483367 01 59 09.354  +30 47 15.14  20.9w 23RS61    F51  C~8Mns      
2024 10  22.495463 01 59 09.105  +30 47 14.41  21.2w 23RS61    F51  C~8Mns      
2024 10  31.285918 01 56 02.368  +30 37 56.42  20.2G 23RS61    V00  C~8Mns      
2024 10  31.291542 01 56 02.245  +30 37 55.92  20.6G 23RS61    V00  C~8Mns      
2024 10  31.297152 01 56 02.116  +30 37 55.52  20.6G 23RS61    V00  C~8Mns      
2024 10  31.302774 01 56 01.993  +30 37 55.13  20.3G 23RS61    V00  C~8Mns      
2024 11  02.88894  01 55 07.68   +30 34 34.8   19.9R 23RS61    157  C~8Q7R      
2024 11  02.91335  01 55 07.17   +30 34 33.5   19.7R 23RS61    157  C~8Q7R      
2024 11  03.639780 01 54 52.03   +30 33 34.2   19.3R 23RS61    D29  C~8Q7R      
2024 11  03.645968 01 54 51.92   +30 33 34.6   19.2R 23RS61    D29  C~8Q7R      
2024 11  03.646851 01 54 51.85   +30 33 34.8   20.3R 23RS61    D29  C~8Q7R      
2024 11  03.653038 01 54 51.97   +30 33 32.9   19.4R 23RS61    D29  C~8Q7R      
2024 12  01.80865  01 46 27.90   +29 45 42.7   20.2R 23RS61    157  C~8Smu      
2024 12  01.83414  01 46 27.60   +29 45 39.5   20.4R 23RS61    157  C~8Smu      
2024 12  02.217345 01 46 22.314  +29 44 56.18  20.7G 23RS61    V00  C~8Smu      
2024 12  02.222952 01 46 22.256  +29 44 55.64  21.0G 23RS61    V00  C~8Smu      
2024 12  02.228558 01 46 22.177  +29 44 54.85  20.6G 23RS61    V00  C~8Smu      
2024 12  02.234172 01 46 22.098  +29 44 53.99  20.8G 23RS61    V00  C~8Smu      

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     0.17       0.00    -0.18
     2   0.0002      0.00    -0.09       0.00    -0.20
     3   0.0004      0.00     0.12       0.00    -0.14
     4   5.0303      0.00     0.16       0.00     0.08
     5   5.0304      0.00     0.04       0.00     0.34
     6   5.0304      0.00    -0.03       0.00     0.28
     7   6.0028      0.00     0.02       0.00     0.18
     8   6.0056      0.00    -0.04       0.00     0.19
     9   8.0283      0.00     0.12       0.00     0.15
    10   8.0284      0.00    -0.33       0.00     0.09
    11   8.0284      0.00     0.15       0.00     0.08
    12   8.0285      0.00    -0.39       0.00    -0.05
    13   8.0829      0.00    -0.07       0.00     0.23
    14   8.0829      0.00    -0.17       0.00     0.47
    15   8.0829      0.00    -0.14       0.00     0.21
    16   8.0881      0.00     0.42       0.00     0.08
    17   8.0882      0.00    -0.34       0.00     0.24
    18   8.0882      0.00    -0.04       0.00    -0.80
    19   8.0884      0.00    -0.22       0.00     0.06
    20   8.0884      0.00    -0.08       0.00    -0.26
    21   8.0964      0.00     0.41       0.00     0.12
    22   8.0964      0.00     0.08       0.00     0.16
    23   8.0964      0.00     0.24       0.00    -0.95
    24   8.0964      0.00    -0.62       0.00    -0.76
    25   8.1292      0.00    -0.37       0.00    -0.37
    26   8.1293      0.00    -0.43       0.00    -0.32
    27   8.1324      0.00     0.14       0.00    -0.40
    28   8.1324      0.00    -0.21       0.00     0.21
    29   8.1325      0.00    -0.27       0.00     0.03
    30   8.1812      0.00     0.44       0.00     0.27
    31   8.1812      0.00    -0.13       0.00     0.08
    32   8.1813      0.00     0.12       0.00    -0.10
    33   8.9924      0.00    -0.16       0.00     0.26
    34   8.9924      0.00    -0.24       0.00     0.29
    35   8.9924      0.00    -0.21       0.00     0.35
    36   8.9925      0.00    -0.16       0.00     0.33
    37   9.0692      0.00    -0.04       0.00     0.22
    38   9.0692      0.00    -0.32       0.00     0.30
    39   9.0692      0.00    -0.22       0.00     0.38
    40   9.0693      0.00    -0.01       0.00     0.23
    41   9.0986      0.00    -0.13       0.00    -0.07
    42   9.0986      0.00    -0.36       0.00     0.04
    43   9.0987      0.00    -0.16       0.00     0.02
    44   9.0987      0.00     0.11       0.00     0.35
    45   9.1318      0.00    -0.21       0.00     0.11
    46   9.1318      0.00    -0.15       0.00     0.20
    47   9.1319      0.00    -0.41       0.00     0.25
    48   9.1319      0.00    -0.22       0.00     0.16
    49   9.1560      0.00    -0.00       0.00    -0.07
    50   9.1560      0.00    -0.03       0.00    -0.15
    51   9.1560      0.00    -0.15       0.00    -0.13
    52   9.1560      0.00    -0.18       0.00    -0.10
    53   9.1631      0.00     0.09       0.00    -0.75
    54   9.1632      0.00     0.23       0.00    -0.10
    55   9.1651      0.00     0.62       0.00    -0.88
    56   9.1652      0.00     0.94       0.00     0.03
    57   9.1652      0.00     0.17       0.00     0.30
    58   9.1652      0.00 (   3.95)      0.00 (  -1.09)
    59   9.2423      0.00     0.08       0.00     0.34
    60   9.2423      0.00     0.95       0.00     0.01
    61   9.2434      0.00     0.10       0.00    -0.26
    62   9.2434      0.00     0.40       0.00    -0.16
    63   9.2434      0.00     0.39       0.00    -0.32
    64   9.2434      0.00     0.37       0.00    -0.54

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.

23RS61    quality flag:3

Type:       CENTAURR  CENTAURR  CENTAURR

axisobj        11.779    11.779    11.779
ecceobj         0.326     0.326     0.326
incobj         19.980    19.980    19.980
qmin            7.167     7.377     7.451
qmax           17.976    20.354    16.759
amean          12.370    13.084    11.845
amin           11.779    11.780    11.242
amax           12.736    13.945    12.182
emean           0.392     0.415     0.350
emin            0.326     0.326     0.297
emax            0.423     0.462     0.382
imean          18.441    17.410    18.512
imin           17.303    14.808    16.571
imax           20.824    20.824    21.798
excite_mean     0.505     0.515     0.473
fracstop        0.002     0.001     0.003
cjmean          3.554     3.448     3.657

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       181.3     134.7     188.2
kozaiamp         62.4      17.9      68.4