Orbit Fit and Astrometric record for 13RM158

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: 13RM158   
# Created Sun Dec 22 02:09:37 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     21 observations of     21
# Arc:  10.99y
# First observation: 2013/09/05
#  Last observation: 2024/08/30
# Chi-squared of fit:     3.94 DOF:     36 RMS:  0.08
# Min/Max residuals:    -0.16    0.23
# Exact a, adot, b, bdot, g, gdot:
  1.548324E-05  2.619860E-02 -4.572795E-06 -7.494395E-03  2.601006E-02  9.039702E-04
# Covariance matrix:
  4.1696E-13 -5.5764E-14  1.5407E-14  1.4923E-15  5.2096E-13 -4.3102E-14
 -5.5764E-14  4.6013E-14  1.9289E-14 -1.1953E-14  7.4001E-14  1.4989E-13
  1.5407E-14  1.9289E-14  1.7927E-13 -3.3575E-14  1.1238E-13  8.4050E-14
  1.4923E-15 -1.1953E-14 -3.3575E-14  1.1355E-14 -4.1861E-14 -4.8708E-14
  5.2096E-13  7.4001E-14  1.1238E-13 -4.1861E-14  1.5933E-12  4.6359E-13
 -4.3102E-14  1.4989E-13  8.4050E-14 -4.8708E-14  4.6359E-13  6.0338E-13
#      lat0       lon0       xBary       yBary       zBary        JD0
    9.140774  -27.341804   -0.170021    0.158119   -0.982237  2456540.575604
# Heliocentric elements and errors
Epoch:              2456540.5000  =  2013/09/05
Mean Anomaly:           19.13570 +/-     0.033
Argument of Peri:      126.92518 +/-     0.041
Long of Asc Node:      181.28776 +/-     0.000
Inclination:            18.25875 +/-     0.000
Eccentricity:         0.10116322 +/-    0.0001
Semi-Major Axis:     43.53318987 +/-    0.0094
Time of Perihelion: 2450963.8809 +/-       9.9
Perihelion:          39.12923234 +/-    0.0104
Aphelion:            47.93714741 +/-    0.0120
Period (y)              287.2360 +/-      0.09
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           34.67967032 +/-    0.0016
Ecliptic Y          -17.73715195 +/-    0.0009
Ecliptic Z            6.10749521 +/-    0.0003
Ecliptic XDOT         0.00145519 +/-    0.0000
Ecliptic YDOT         0.00234779 +/-    0.0000
Ecliptic ZDOT        -0.00076360 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   39.42823544 +/-    0.0015
Geocenter to KBO     38.44668118 +/-    0.0019
# Hcoef:  6.78

The following table shows the complete astrometric record for 13RM158. 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 (13RM158) followed by the observatory code and reference code for the source of the astrometry.

2013 09  05.074826 22 05 22.95   -01 59 03.6   22.8g 13RM158   W84  C~55Nc      
2013 09  08.142222 22 05 09.16   -02 00 45.5   22.8g 13RM158   W84  C~55Nc      
2013 09  11.184630 22 04 55.75   -02 02 27.6   22.8g 13RM158   W84  C~55Nc      
2013 10  12.029062 22 03 05.00   -02 19 21.7   22.8i 13RM158   W84  C~55Nc      
2013 10  12.030440 22 03 05.00   -02 19 21.9   22.3z 13RM158   W84  C~55Nc      
2013 11  23.046146 22 02 34.25   -02 34 59.6   22.6r 13RM158   W84  C~55Nc      
2016 09  23.10367  22 22 38.488  -01 46 01.42  22.4i 13RM158   W84  C~55Nc      
2016 09  23.10505  22 22 38.484  -01 46 01.31  23.0r 13RM158   W84  C~55Nc      
2016 09  23.10643  22 22 38.493  -01 46 01.30  23.1g 13RM158   W84  C~55Nc      
2016 09  29.08927  22 22 15.178  -01 49 23.14  22.3z 13RM158   W84  C~55Nc      
2017 09  27.12202  22 28 32.829  -01 40 16.83  22.7r 13RM158   W84  C~55Nc      
2017 09  27.12340  22 28 32.821  -01 40 16.92  23.2z 13RM158   W84  C~55Nc      
2017 09  27.12478  22 28 32.805  -01 40 17.05  22.2i 13RM158   W84  C~55Nc      
2017 10  22.06145  22 27 13.656  -01 53 20.82  23.3g 13RM158   W84  C~55Nc      
2017 10  22.06282  22 27 13.653  -01 53 20.82  22.8r 13RM158   W84  C~55Nc      
2017 10  22.06421  22 27 13.646  -01 53 20.76  23.0i 13RM158   W84  C~55Nc      
2018 09  17.23010  22 35 24.065  -01 26 33.63  22.8r 13RM158   W84  C~55Nc      
2018 09  17.23147  22 35 24.059  -01 26 33.66  22.4i 13RM158   W84  C~55Nc      
2018 09  17.23284  22 35 24.053  -01 26 33.70  23.4g 13RM158   W84  C~55Nc      
2024 08  30.370930 23 13 21.858  -00 27 43.82  22.7G 13RM158   G37  C~8Dcp      
2024 08  30.427560 23 13 21.600  -00 27 45.56        13RM158   G37  C~8Dcp      

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     0.04
     2   0.0084      0.00    -0.00       0.00     0.09
     3   0.0167      0.00    -0.10       0.00    -0.01
     4   0.1012      0.00    -0.05       0.00    -0.00
     5   0.1012      0.00     0.00       0.00    -0.16
     6   0.2162      0.00     0.08       0.00     0.11
     7   3.0500      0.00    -0.01       0.00    -0.16
     8   3.0500      0.00     0.01       0.00    -0.01
     9   3.0501      0.00     0.23       0.00     0.05
    10   3.0664      0.00    -0.11       0.00    -0.04
    11   4.0604      0.00     0.04       0.00     0.03
    12   4.0604      0.00     0.01       0.00    -0.01
    13   4.0604      0.00    -0.15       0.00    -0.09
    14   4.1286      0.00     0.03       0.00    -0.06
    15   4.1286      0.00     0.03       0.00    -0.02
    16   4.1286      0.00    -0.03       0.00     0.08
    17   5.0326      0.00    -0.00       0.00     0.06
    18   5.0326      0.00    -0.00       0.00     0.08
    19   5.0326      0.00    -0.00       0.00     0.09
    20  10.9851      0.00     0.01       0.00    -0.05
    21  10.9852      0.00    -0.01       0.00     0.02

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.

13RM158    quality flag:3

Type:       SCATEXTD  SCATEXTD  SCATEXTD

axisobj        43.711    43.711    43.711
ecceobj         0.105     0.105     0.105
incobj         18.221    18.221    18.221
qmin           38.066    38.038    38.113
qmax           49.564    49.760    49.699
amean          43.739    43.752    43.718
amin           43.299    43.316    43.307
amax           44.172    44.180    44.158
emean           0.103     0.102     0.101
emin            0.080     0.080     0.077
emax            0.125     0.128     0.126
imean          18.326    18.327    18.320
imin           17.719    17.729    17.747
imax           18.893    18.895    18.888
excite_mean     0.331     0.331     0.330
fracstop        1.000     1.000     1.000
cjmean          2.964     2.964     2.964

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       179.3     179.5     179.6
kozaiamp        180.0     180.0     179.9