Orbit Fit and Astrometric record for 16GR368

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: 16GR368   
# Created Sun Dec 22 02:10:41 2024
# Orbit generated from Bernstein formalism
# Fitting     21 observations of     21
# Arc:  89.79d
# First observation: 2016/03/07
#  Last observation: 2016/06/05
Preliminary a, adot, b, bdot, g, gdot:
  -0.000044   0.025419   0.000002   0.006425   0.025023   0.000000
# Chi-squared of fit:     9.11 DOF:     36 RMS:  0.12
# Min/Max residuals:    -0.37    0.23
# Exact a, adot, b, bdot, g, gdot:
  1.482884E-05  2.429774E-02  5.157686E-06  6.425788E-03  2.485096E-02  2.663117E-03
# Covariance matrix:
  3.0909E-13 -8.7450E-12  2.0699E-14  1.6881E-13 -6.6874E-13  1.3073E-10
 -8.7450E-12  4.6556E-09 -2.4240E-11  3.7716E-11  8.0225E-10 -2.6006E-09
  2.0699E-14 -2.4240E-11  2.9741E-13 -1.2551E-12 -4.2882E-12 -5.7340E-12
  1.6881E-13  3.7716E-11 -1.2551E-12  1.1357E-11  7.7139E-12  2.0693E-10
 -6.6874E-13  8.0225E-10 -4.2882E-12  7.7139E-12  1.4201E-10  2.0586E-10
  1.3073E-10 -2.6006E-09 -5.7340E-12  2.0693E-10  2.0586E-10  1.2597E-07
#      lat0       lon0       xBary       yBary       zBary        JD0
   10.241886 -150.175524    0.671207    0.129364   -0.715183  2457455.125619
# Heliocentric elements and errors
Epoch:              2457450.5000  =  2016/03/03
Mean Anomaly:           43.83571 +/-     3.139
Argument of Peri:      340.20717 +/-     4.603
Long of Asc Node:      175.64625 +/-     0.072
Inclination:            17.93904 +/-     0.032
Eccentricity:         0.11871815 +/-    0.0124
Semi-Major Axis:     44.42627531 +/-    0.2120
Time of Perihelion: 2444280.5581 +/-     938.2
Perihelion:          39.15207027 +/-    0.5800
Aphelion:            49.70048035 +/-    0.5981
Period (y)              296.1202 +/-      2.12
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -35.32176596 +/-    0.0165
Ecliptic Y          -19.47572245 +/-    0.0094
Ecliptic Z            7.15504668 +/-    0.0034
Ecliptic XDOT         0.00118993 +/-    0.0000
Ecliptic YDOT        -0.00241033 +/-    0.0000
Ecliptic ZDOT         0.00074883 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   40.96493145 +/-    0.0149
Geocenter to KBO     40.23988929 +/-    0.0193
# Hcoef:  7.37

The following table shows the complete astrometric record for 16GR368. 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 (16GR368) followed by the observatory code and reference code for the source of the astrometry.

2016 03  07.62483  14 05 20.05   -01 48 28.3   24.3g 16GR368   T09  C~89Tc      
2016 03  07.63768  14 05 20.02   -01 48 27.8   24.1g 16GR368   T09  C~89Tc      
2016 03  07.63983  14 05 20.00   -01 48 27.6   24.0g 16GR368   T09  C~89Tc      
2016 03  16.48552  14 04 52.17   -01 43 46.0   23.1z 16GR368   T09  C~89Tc      
2016 03  16.53802  14 04 51.99   -01 43 44.2   22.9z 16GR368   T09  C~89Tc      
2016 03  16.56263  14 04 51.90   -01 43 43.5   23.0z 16GR368   T09  C~89Tc      
2016 03  16.58446  14 04 51.82   -01 43 42.7   23.2z 16GR368   T09  C~89Tc      
2016 04  08.52969  14 03 20.28   -01 31 16.7   23.3r 16GR368   T09  C~89Tc      
2016 04  08.55612  14 03 20.16   -01 31 15.8   23.3r 16GR368   T09  C~89Tc      
2016 04  08.56457  14 03 20.12   -01 31 15.5   23.2r 16GR368   T09  C~89Tc      
2016 04  11.42730  14 03 07.42   -01 29 45.3   23.7i 16GR368   T09  C~89Tc      
2016 04  11.45409  14 03 07.29   -01 29 44.7   23.4i 16GR368   T09  C~89Tc      
2016 04  11.50036  14 03 07.08   -01 29 43.2   23.0i 16GR368   T09  C~89Tc      
2016 04  11.54095  14 03 06.90   -01 29 42.0   23.2i 16GR368   T09  C~89Tc      
2016 04  14.51577  14 02 53.51   -01 28 10.1   23.8y 16GR368   T09  C~89Tc      
2016 04  14.57188  14 02 53.25   -01 28 08.1   23.1y 16GR368   T09  C~89Tc      
2016 04  14.59074  14 02 53.17   -01 28 08.1   23.4y 16GR368   T09  C~89Tc      
2016 06  05.36438  13 59 19.09   -01 09 42.5   23.5r 16GR368   T09  C~89Tc      
2016 06  05.38004  13 59 19.05   -01 09 42.2   23.4r 16GR368   T09  C~89Tc      
2016 06  05.40559  13 59 18.97   -01 09 42.2   23.3r 16GR368   T09  C~89Tc      
2016 06  05.40987  13 59 18.96   -01 09 42.0   23.3r 16GR368   T09  C~89Tc      

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     0.13       0.00    -0.22
     2   0.0000     -0.59     0.20       0.31    -0.09
     3   0.0000     -0.95    -0.04       0.40    -0.03
     4   0.0243   -489.77    -0.10     120.60     0.02
     5   0.0244   -492.92    -0.07     121.36     0.14
     6   0.0245   -494.43    -0.09     121.55     0.03
     7   0.0245   -495.83    -0.16     121.89     0.10
     8   0.0874  -2041.65    -0.01     347.89     0.03
     9   0.0874  -2043.65    -0.05     348.11     0.08
    10   0.0874  -2044.31    -0.09     348.18     0.10
    11   0.0953  -2254.21     0.03     367.03     0.23
    12   0.0954  -2256.25     0.00     366.92    -0.03
    13   0.0955  -2259.72    -0.00     367.24     0.03
    14   0.0956  -2262.67     0.09     367.44    -0.01
    15   0.1037  -2482.87     0.05     384.30    -0.12
    16   0.1039  -2487.22    -0.08     384.83     0.14
    17   0.1039  -2488.34     0.21     384.42    -0.37
    18   0.2457  -5884.44    -0.10     311.95    -0.09
    19   0.2457  -5885.11    -0.03     312.03     0.11
    20   0.2458  -5886.23     0.05     311.61    -0.11
    21   0.2458  -5886.44     0.05     311.75     0.06

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.

16GR368    quality flag:3

Type:       SCATEXTD  SCATEXTD  SCATEXTD

axisobj        43.908    44.634    43.257
ecceobj         0.111     0.140     0.084
incobj         18.020    17.955    18.092
qmin           38.230    37.543    38.818
qmax           50.438    52.605    48.519
amean          44.187    44.910    43.537
amin           43.815    44.536    43.195
amax           44.580    45.336    43.906
emean           0.117     0.146     0.090
emin            0.105     0.132     0.078
emax            0.132     0.161     0.105
imean          17.669    17.557    17.797
imin           17.203    17.088    17.394
imax           18.137    18.035    18.184
excite_mean     0.325     0.335     0.319
fracstop        1.000     1.000     1.000
cjmean          2.974     2.974     2.972

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       182.0     174.3     176.1
kozaiamp        180.0     180.0     180.0