Orbit Fit and Astrometric record for 16QN158

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: 16QN158   
# Created Wed Mar 26 01:10:54 2025
# Orbit generated from Bernstein formalism
# Fitting     22 observations of     22
# Arc:   4.20y
# First observation: 2015/07/15
#  Last observation: 2019/09/27
Preliminary a, adot, b, bdot, g, gdot:
  -0.000047   0.026211   0.000028   0.010198   0.026310   0.000000
# Chi-squared of fit:    15.92 DOF:     38 RMS:  0.15
# Min/Max residuals:    -0.55    0.28
# Exact a, adot, b, bdot, g, gdot:
  1.540619E-05  2.627212E-02  6.660723E-06  1.017287E-02  2.680172E-02  3.358292E-03
# Covariance matrix:
  2.5871E-13 -2.6669E-13  5.8526E-14 -1.0439E-13 -1.1500E-14 -2.3869E-12
 -2.6669E-13  6.0694E-13 -1.3170E-13  2.2073E-13  5.3802E-13  5.1654E-12
  5.8526E-14 -1.3170E-13  1.7701E-13 -1.2442E-13 -8.3131E-14 -1.3592E-12
 -1.0439E-13  2.2073E-13 -1.2442E-13  1.5824E-13  1.1190E-13  2.3526E-12
 -1.1500E-14  5.3802E-13 -8.3131E-14  1.1190E-13  1.3308E-12  2.8625E-12
 -2.3869E-12  5.1654E-12 -1.3592E-12  2.3526E-12  2.8625E-12  5.4392E-11
#      lat0       lon0       xBary       yBary       zBary        JD0
    3.755234   -6.980384    0.883665    0.033149   -0.503485  2457219.072559
# Heliocentric elements and errors
Epoch:              2457210.5000  =  2015/07/07
Mean Anomaly:           48.70173 +/-     0.047
Argument of Peri:      310.19024 +/-     0.072
Long of Asc Node:      342.24678 +/-     0.000
Inclination:            21.56270 +/-     0.001
Eccentricity:         0.11819659 +/-    0.0003
Semi-Major Axis:     40.62857129 +/-    0.0072
Time of Perihelion: 2444414.1048 +/-      12.0
Perihelion:          35.82641279 +/-    0.0123
Aphelion:            45.43072979 +/-    0.0132
Period (y)              258.9736 +/-      0.07
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           37.34500620 +/-    0.0016
Ecliptic Y           -5.46281103 +/-    0.0002
Ecliptic Z            2.44395871 +/-    0.0001
Ecliptic XDOT         0.00059611 +/-    0.0000
Ecliptic YDOT         0.00262424 +/-    0.0000
Ecliptic ZDOT         0.00105948 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   37.82148498 +/-    0.0016
Geocenter to KBO     37.31104251 +/-    0.0016
# Hcoef:  9.14

The following table shows the complete astrometric record for 16QN158. 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 (16QN158) followed by the observatory code and reference code for the source of the astrometry.

2015 07  15.57177  23 28 25.68   +00 40 44.7   24.7r 16QN158   T09  C~8iej      
2015 07  15.58216  23 28 25.64   +00 40 44.9   24.9r 16QN158   T09  C~8iej      
2015 07  15.59249  23 28 25.63   +00 40 44.7   24.9r 16QN158   T09  C~8iej      
2015 07  20.573884 23 28 13.51   +00 40 26.0         16QN158   T09  C~83Ea      
2015 07  20.617410 23 28 13.39   +00 40 25.7         16QN158   T09  C~83Ea      
2016 08  01.45987  23 32 11.10   +01 46 29.6   24.9z 16QN158   T09  C~83Ea      
2016 08  01.48148  23 32 11.01   +01 46 29.6   25.0z 16QN158   T09  C~83Ea      
2016 08  01.49500  23 32 10.96   +01 46 29.8   24.5z 16QN158   T09  C~83Ea      
2016 08  01.50310  23 32 10.94   +01 46 29.8   24.0z 16QN158   T09  C~83Ea      
2016 08  01.52754  23 32 10.85   +01 46 29.4   24.3z 16QN158   T09  C~83Ea      
2016 08  01.55200  23 32 10.77   +01 46 29.3   24.7z 16QN158   T09  C~83Ea      
2016 08  01.57640  23 32 10.68   +01 46 28.8   24.2z 16QN158   T09  C~83Ea      
2016 08  28.39408  23 30 16.67   +01 38 48.9   25.9g 16QN158   T09  C~83Ea      
2016 08  28.41119  23 30 16.60   +01 38 48.5   25.5g 16QN158   T09  C~83Ea      
2016 08  28.41778  23 30 16.55   +01 38 48.2   25.9g 16QN158   T09  C~83Ea      
2016 08  28.41990  23 30 16.55   +01 38 48.4   25.9g 16QN158   T09  C~83Ea      
2016 09  07.39090  23 29 27.10   +01 34 49.3   25.2r 16QN158   T09  C~83Ea      
2016 09  07.45841  23 29 26.76   +01 34 47.6   24.6r 16QN158   T09  C~83Ea      
2016 09  07.48918  23 29 26.60   +01 34 46.8   25.0r 16QN158   T09  C~83Ea      
2017 06  24.574465 23 37 56.78   +02 52 44.1         16QN158   T09  C~83Ea      
2019 09  27.251196 23 41 43.17   +04 49 06.5         16QN158   T09  C~83Ea      
2019 09  27.272128 23 41 43.07   +04 49 05.9         16QN158   T09  C~83Ea      

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     0.02       0.00    -0.14
     2   0.0000     -0.47    -0.11       0.42     0.16
     3   0.0001     -0.69     0.01       0.30    -0.08
     4   0.0137   -175.09     0.18      54.90    -0.07
     5   0.0138   -176.86     0.14      55.33    -0.13
     6   1.0483   4664.10    -0.17    2290.73    -0.55
     7   1.0483   4662.86    -0.25    2291.26    -0.26
     8   1.0484   4662.25    -0.14    2291.74     0.07
     9   1.0484   4661.97     0.02    2291.86     0.10
    10   1.0485   4660.57    -0.07    2292.02    -0.01
    11   1.0485   4659.43     0.10    2292.40     0.09
    12   1.0486   4657.99    -0.03    2292.48    -0.11
    13   1.1220   2905.15    -0.09    2544.35     0.25
    14   1.1221   2904.03     0.10    2544.40     0.15
    15   1.1221   2903.22    -0.20    2544.42     0.12
    16   1.1221   2903.30     0.04    2544.60     0.28
    17   1.1494   2127.51     0.02    2617.56     0.09
    18   1.1496   2122.15     0.12    2618.01     0.05
    19   1.1497   2119.63     0.09    2618.22     0.04
    20   1.9439  11002.89     0.19    3904.98     0.03
    21   4.2017  16898.30    -0.03    9017.33    -0.03
    22   4.2018  16896.68     0.05    9017.36    -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.

16QN158    quality flag:3

Type:       SCATEXTD  SCATEXTD  SCATEXTD

axisobj        40.944    40.967    40.921
ecceobj         0.122     0.123     0.122
incobj         21.477    21.478    21.477
qmin           34.967    35.056    35.147
qmax           46.898    46.920    46.771
amean          40.851    40.846    40.818
amin           40.515    40.514    40.463
amax           41.222    41.200    41.176
emean           0.122     0.121     0.119
emin            0.106     0.106     0.104
emax            0.140     0.139     0.137
imean          22.160    22.176    22.197
imin           21.445    21.464    21.473
imax           22.796    22.804    22.799
excite_mean     0.397     0.396     0.396
fracstop        1.000     1.000     1.000
cjmean          2.877     2.877     2.877

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       174.9     174.9     175.0
kozaiamp        180.0     180.0     179.9