Orbit Fit and Astrometric record for 13RU157

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: 13RU157   
# Created Sat Apr 27 01:14:58 2024
# Orbit generated from Bernstein formalism
# Fitting     21 observations of     21
# Arc:   4.04y
# First observation: 2013/09/11
#  Last observation: 2017/09/24
Preliminary a, adot, b, bdot, g, gdot:
  -0.000054   0.016729   0.000048  -0.010318   0.022095   0.000000
# Chi-squared of fit:     5.88 DOF:     36 RMS:  0.09
# Min/Max residuals:    -0.25    0.23
# Exact a, adot, b, bdot, g, gdot:
  1.221516E-05  1.650325E-02 -6.062626E-06 -1.017247E-02  2.204306E-02 -3.156562E-03
# Covariance matrix:
  3.5593E-13 -7.6758E-14  3.3806E-15 -1.1963E-14  3.1960E-13  2.7574E-13
 -7.6758E-14  2.6930E-13  4.8999E-14 -1.6205E-13  1.6686E-13  3.9439E-12
  3.3806E-15  4.8999E-14  2.2067E-13 -9.4224E-14  4.8803E-14  8.1863E-13
 -1.1963E-14 -1.6205E-13 -9.4224E-14  1.3734E-13 -1.6319E-13 -2.7103E-12
  3.1960E-13  1.6686E-13  4.8803E-14 -1.6319E-13  8.7198E-13  3.9364E-12
  2.7574E-13  3.9439E-12  8.1863E-13 -2.7103E-12  3.9364E-12  6.5903E-11
#      lat0       lon0       xBary       yBary       zBary        JD0
   -9.944178    9.470897    0.362831   -0.162216   -0.925802  2456546.763018
# Heliocentric elements and errors
Epoch:              2456540.5000  =  2013/09/05
Mean Anomaly:          258.15095 +/-     0.091
Argument of Peri:      319.23759 +/-     0.069
Long of Asc Node:      173.72849 +/-     0.000
Inclination:            33.06921 +/-     0.000
Eccentricity:         0.18406138 +/-    0.0003
Semi-Major Axis:     43.35193288 +/-    0.0086
Time of Perihelion: 2486036.6675 +/-      24.9
Perihelion:          35.37251646 +/-    0.0160
Aphelion:            51.33134930 +/-    0.0176
Period (y)              285.4440 +/-      0.09
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           45.06147732 +/-    0.0019
Ecliptic Y            7.15241327 +/-    0.0003
Ecliptic Z           -7.83443795 +/-    0.0003
Ecliptic XDOT        -0.00093958 +/-    0.0000
Ecliptic YDOT         0.00192123 +/-    0.0000
Ecliptic ZDOT        -0.00117664 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   46.29332751 +/-    0.0018
Geocenter to KBO     45.36574702 +/-    0.0019
# Hcoef:  6.53

The following table shows the complete astrometric record for 13RU157. 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 (13RU157) followed by the observatory code and reference code for the source of the astrometry.

2013 09  11.26224  00 50 27.030  -05 23 31.17  23.0g 13RU157   W84  C~52RP      
2013 09  29.21656  00 49 17.120  -05 33 41.83  24.3g 13RU157   W84  C~52RP      
2013 09  29.21795  00 49 17.121  -05 33 41.92  23.3r 13RU157   W84  C~52RP      
2013 09  29.21933  00 49 17.113  -05 33 42.03  22.9i 13RU157   W84  C~52RP      
2013 11  08.08585  00 46 42.023  -05 51 29.15  22.9i 13RU157   W84  C~52RP      
2013 11  08.08722  00 46 42.017  -05 51 29.28  22.8z 13RU157   W84  C~52RP      
2014 10  03.30184  00 53 27.288  -05 45 40.17  22.7r 13RU157   W84  C~52RP      
2014 10  03.30321  00 53 27.266  -05 45 40.33  22.7i 13RU157   W84  C~52RP      
2016 08  16.42600  01 05 03.236  -05 38 03.71  22.4i 13RU157   W84  C~52RP      
2016 08  26.36153  01 04 38.820  -05 43 35.95  23.4r 13RU157   W84  C~52RP      
2016 09  30.20197  01 02 34.840  -06 03 53.77  23.3r 13RU157   W84  C~52RP      
2016 09  30.20335  01 02 34.831  -06 03 53.82  23.2i 13RU157   W84  C~52RP      
2016 09  30.20472  01 02 34.821  -06 03 53.89  23.9g 13RU157   W84  C~52RP      
2016 11  07.20759  01 00 02.516  -06 21 07.28  21.6z 13RU157   W84  C~52RP      
2017 08  28.32246  01 09 04.262  -05 54 07.68  23.5r 13RU157   W84  C~52RP      
2017 08  28.32384  01 09 04.255  -05 54 07.86  23.2i 13RU157   W84  C~52RP      
2017 08  28.32522  01 09 04.264  -05 54 08.04  24.1g 13RU157   W84  C~52RP      
2017 08  28.40635  01 09 04.018  -05 54 10.70  22.3z 13RU157   W84  C~52RP      
2017 09  24.24497  01 07 31.129  -06 10 03.69  23.2r 13RU157   W84  C~52RP      
2017 09  24.24634  01 07 31.139  -06 10 03.79  23.1i 13RU157   W84  C~52RP      
2017 09  24.32878  01 07 30.810  -06 10 06.65  22.9z 13RU157   W84  C~52RP      

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    -0.08       0.00    -0.25
     2   0.0492  -1200.02    -0.04    -150.14     0.10
     3   0.0492  -1200.04     0.03    -150.23     0.02
     4   0.0492  -1200.19    -0.02    -150.29    -0.03
     5   0.1583  -3748.54     0.05    -221.45     0.02
     6   0.1583  -3748.67    -0.01    -221.53    -0.07
     7   1.0597   1948.22     0.15   -2283.38     0.15
     8   1.0597   1947.85    -0.12   -2283.39     0.14
     9   2.9299  11677.19     0.23   -6001.18     0.02
    10   2.9572  11208.83    -0.06   -6160.08     0.03
    11   3.0525   9020.55     0.07   -6537.16    -0.02
    12   3.0525   9020.41     0.02   -6537.15    -0.00
    13   3.0525   9020.25    -0.04   -6537.16     0.00
    14   3.1566   6520.59    -0.06   -6578.48    -0.06
    15   3.9618  14603.15    -0.01   -8336.13     0.10
    16   3.9618  14602.98    -0.11   -8336.26    -0.00
    17   3.9618  14603.03     0.02   -8336.48    -0.20
    18   3.9621  14598.58    -0.09   -8337.44     0.03
    19   4.0355  12938.70    -0.12   -8653.41     0.11
    20   4.0355  12938.79     0.07   -8653.56    -0.03
    21   4.0358  12933.12     0.12   -8654.21    -0.05

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.

13RU157    quality flag:3

Type:       SCATEXTD  SCATEXTD  SCATEXTD

axisobj        43.518    43.542    43.494
ecceobj         0.180     0.181     0.180
incobj         32.957    32.956    32.957
qmin           34.237    34.190    34.251
qmax           52.921    52.731    52.697
amean          43.334    43.335    43.298
amin           42.965    42.956    42.950
amax           43.764    43.773    43.707
emean           0.187     0.186     0.186
emin            0.167     0.168     0.167
emax            0.209     0.207     0.207
imean          32.473    32.481    32.485
imin           31.983    31.998    31.982
imax           32.860    32.878    32.876
excite_mean     0.569     0.569     0.568
fracstop        1.000     1.000     1.000
cjmean          2.683     2.683     2.683

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       171.4     174.0     173.3
kozaiamp        180.0     180.0     180.0