Orbit Fit and Astrometric record for 16EM398

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: 16EM398   
# Created Sat Feb 22 02:10:46 2025
# Orbit generated from Bernstein formalism
# Fitting     21 observations of     21
# Arc:  32.90d
# First observation: 2016/02/08
#  Last observation: 2016/03/12
Preliminary a, adot, b, bdot, g, gdot:
  -0.000013   0.361454   0.000031  -0.195291   0.147585   0.000000
# Chi-squared of fit:    12.06 DOF:     36 RMS:  0.13
# Min/Max residuals:    -0.35    0.38
# Exact a, adot, b, bdot, g, gdot:
  2.714757E-05  2.048535E-01 -2.437938E-05 -1.912613E-01  1.232409E-01  1.112448E-03
# Covariance matrix:
  2.6792E-13 -1.5428E-10 -8.4696E-16 -2.0063E-12 -2.0747E-11  5.4202E-10
 -1.5428E-10  1.2403E-06  1.7025E-10 -1.2166E-08  1.8334E-07 -2.6656E-06
 -8.4696E-16  1.7025E-10  2.1485E-13 -5.1611E-12  2.5699E-11 -2.9862E-10
 -2.0063E-12 -1.2166E-08 -5.1611E-12  3.6045E-10 -1.8915E-09  1.4386E-08
 -2.0747E-11  1.8334E-07  2.5699E-11 -1.8915E-09  2.7147E-08 -3.8831E-07
  5.4202E-10 -2.6656E-06 -2.9862E-10  1.4386E-08 -3.8831E-07  6.4545E-06
#      lat0       lon0       xBary       yBary       zBary        JD0
  -10.759176  141.913594    0.055393   -0.183364   -0.965911  2457426.975609
# Heliocentric elements and errors
Epoch:              2457420.5000  =  2016/02/02
Mean Anomaly:          356.37924 +/-     2.090
Argument of Peri:      199.10435 +/-     3.196
Long of Asc Node:      311.46431 +/-     0.054
Inclination:            43.91024 +/-     0.155
Eccentricity:         0.19234202 +/-    0.0029
Semi-Major Axis:     11.23986045 +/-    0.0189
Time of Perihelion: 2457558.9324 +/-      79.9
Perihelion:           9.07796299 +/-    0.0365
Aphelion:            13.40175792 +/-    0.0400
Period (y)               37.6834 +/-      0.09
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           -7.01778302 +/-    0.0084
Ecliptic Y            5.56543668 +/-    0.0066
Ecliptic Z           -1.51497775 +/-    0.0020
Ecliptic XDOT        -0.00220245 +/-    0.0000
Ecliptic YDOT        -0.00406322 +/-    0.0000
Ecliptic ZDOT        -0.00417886 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO    9.08397058 +/-    0.0076
Geocenter to KBO      8.11418896 +/-    0.0108
# Hcoef: 13.77

The following table shows the complete astrometric record for 16EM398. 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 (16EM398) followed by the observatory code and reference code for the source of the astrometry.

2016 02  08.47482  09 23 16.13   +04 00 04.5   23.3r 16EM398   T09  C~8eUq      
2016 02  08.50614  09 23 15.40   +04 00 04.2   23.2r 16EM398   T09  C~8eUq      
2016 02  08.51715  09 23 15.15   +04 00 04.2   23.5r 16EM398   T09  C~8eUq      
2016 02  08.52379  09 23 15.00   +04 00 04.2   23.4r 16EM398   T09  C~8eUq      
2016 02  12.28283  09 21 48.31   +03 59 55.9   22.9y 16EM398   T09  C~8eUq      
2016 02  12.28555  09 21 48.25   +03 59 55.9   23.0y 16EM398   T09  C~8eUq      
2016 02  12.29096  09 21 48.11   +03 59 56.0   22.7y 16EM398   T09  C~8eUq      
2016 02  12.29906  09 21 47.95   +03 59 56.0   22.5y 16EM398   T09  C~8eUq      
2016 02  12.30448  09 21 47.80   +03 59 55.9   22.3y 16EM398   T09  C~8eUq      
2016 03  04.38892  09 14 08.70   +04 03 36.9   23.1i 16EM398   T09  C~8eUq      
2016 03  04.39973  09 14 08.48   +04 03 37.0   23.1i 16EM398   T09  C~8eUq      
2016 03  04.41331  09 14 08.21   +04 03 37.4   23.0i 16EM398   T09  C~8eUq      
2016 03  07.36412  09 13 11.06   +04 04 29.4   24.4g 16EM398   T09  C~8eUq      
2016 03  07.40429  09 13 10.26   +04 04 30.0   23.7g 16EM398   T09  C~8eUq      
2016 03  07.40643  09 13 10.23   +04 04 30.0   23.8g 16EM398   T09  C~8eUq      
2016 03  07.42361  09 13 09.89   +04 04 30.2   23.7g 16EM398   T09  C~8eUq      
2016 03  12.30861  09 11 40.91   +04 05 58.5   23.3z 16EM398   T09  C~8eUq      
2016 03  12.32109  09 11 40.65   +04 05 58.8   22.8z 16EM398   T09  C~8eUq      
2016 03  12.35149  09 11 40.09   +04 05 59.2   23.9z 16EM398   T09  C~8eUq      
2016 03  12.36538  09 11 39.87   +04 05 59.7   23.0z 16EM398   T09  C~8eUq      
2016 03  12.37656  09 11 39.68   +04 05 59.8   23.4z 16EM398   T09  C~8eUq      

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    -0.03
     2   0.0001    -10.28    -0.04      -3.71    -0.14
     3   0.0001    -13.83     0.07      -4.89    -0.04
     4   0.0001    -15.96     0.14      -5.59     0.02
     5   0.0104  -1245.11    -0.00    -420.32     0.01
     6   0.0104  -1245.96     0.05    -420.60     0.03
     7   0.0104  -1247.98    -0.18    -421.16     0.05
     8   0.0105  -1250.25     0.23    -421.91     0.18
     9   0.0105  -1252.35    -0.07    -422.71    -0.02
    10   0.0682  -7851.36    -0.05   -2359.39    -0.06
    11   0.0682  -7854.52    -0.05   -2360.32    -0.15
    12   0.0683  -7858.49    -0.04   -2361.20     0.03
    13   0.0764  -8688.78     0.17   -2578.16     0.20
    14   0.0765  -8700.37    -0.09   -2581.32    -0.00
    15   0.0765  -8700.80     0.08   -2581.46     0.01
    16   0.0765  -8705.70     0.01   -2582.85    -0.12
    17   0.0899 -10001.44     0.38   -2913.31     0.08
    18   0.0899 -10005.24    -0.17   -2914.24    -0.02
    19   0.0900 -10013.35    -0.35   -2916.47    -0.24
    20   0.0900 -10016.64    -0.03   -2917.01     0.13
    21   0.0901 -10019.38     0.14   -2917.80     0.08

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.

16EM398    quality flag:1

Type:       CENTAURR  CENTAURR  CENTAURR

axisobj        11.223    12.987     9.802
ecceobj         0.185     0.152     0.259
incobj         43.916    44.135    43.700
qmin            9.017     9.227     6.772
qmax           13.302    17.163    12.343
amean          11.103    13.112     9.251
amin           10.928    12.705     8.955
amax           11.223    13.790     9.802
emean           0.179     0.219     0.251
emin            0.159     0.148     0.233
emax            0.192     0.281     0.267
imean          45.494    44.734    45.721
imin           45.315    42.976    45.124
imax           45.803    45.642    46.101
excite_mean     0.735     0.738     0.759
fracstop        0.000     0.043     0.001
cjmean          3.542     3.214     4.003

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       197.8     199.8     218.1
kozaiamp          1.1     177.8       2.9