Orbit Fit and Astrometric record for 16EW397

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: 16EW397   
# Created Tue Jan 21 02:10:52 2025
# Orbit generated from Bernstein formalism
# Fitting     20 observations of     20
# Arc:  55.58d
# First observation: 2016/02/12
#  Last observation: 2016/04/08
Preliminary a, adot, b, bdot, g, gdot:
  -0.000002   0.030122  -0.000001   0.006818   0.027880   0.000000
# Chi-squared of fit:     5.94 DOF:     34 RMS:  0.10
# Min/Max residuals:    -0.30    0.22
# Exact a, adot, b, bdot, g, gdot:
  1.769418E-05  3.071801E-02  2.774978E-06  6.797360E-03  2.789660E-02 -1.684478E-03
# Covariance matrix:
  3.8202E-13  6.3389E-11  2.9163E-14  8.4881E-13  1.2486E-11  5.0817E-10
  6.3389E-11  1.7141E-07  8.4551E-11  1.4266E-09  2.9889E-08  5.2066E-07
  2.9163E-14  8.4551E-11  2.7669E-13 -1.2909E-12  1.4717E-11  2.4903E-10
  8.4881E-13  1.4266E-09 -1.2909E-12  3.7019E-11  2.5149E-10  5.1057E-09
  1.2486E-11  2.9889E-08  1.4717E-11  2.5149E-10  5.2219E-09  9.3548E-08
  5.0817E-10  5.2066E-07  2.4903E-10  5.1057E-09  9.3548E-08  2.3660E-06
#      lat0       lon0       xBary       yBary       zBary        JD0
   -3.146930  176.175717    0.541524   -0.045016   -0.821760  2457431.059209
# Heliocentric elements and errors
Epoch:              2457430.5000  =  2016/02/12
Mean Anomaly:          344.60629 +/-    11.024
Argument of Peri:        9.39512 +/-    17.278
Long of Asc Node:      189.02515 +/-     0.180
Inclination:            12.78851 +/-     0.162
Eccentricity:         0.20144492 +/-    0.0129
Semi-Major Axis:     45.29346017 +/-    0.8272
Time of Perihelion: 2462191.4378 +/-    3406.9
Perihelion:          36.16932282 +/-    0.8828
Aphelion:            54.41759752 +/-    1.1536
Period (y)              304.8326 +/-      8.35
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -36.50176492 +/-    0.0925
Ecliptic Y            2.98013124 +/-    0.0062
Ecliptic Z           -1.96776471 +/-    0.0051
Ecliptic XDOT        -0.00007330 +/-    0.0002
Ecliptic YDOT        -0.00302358 +/-    0.0000
Ecliptic ZDOT         0.00067520 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   36.67604289 +/-    0.0921
Geocenter to KBO     35.84666669 +/-    0.0929
# Hcoef:  7.21

The following table shows the complete astrometric record for 16EW397. 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 (16EW397) followed by the observatory code and reference code for the source of the astrometry.

2016 02  12.55842  11 40 57.89   -01 22 05.3   22.6y 16EW397   T09  C~8SZf      
2016 02  12.58759  11 40 57.77   -01 22 04.7   23.1y 16EW397   T09  C~8SZf      
2016 02  12.61467  11 40 57.66   -01 22 04.1   22.9y 16EW397   T09  C~8SZf      
2016 02  12.62813  11 40 57.59   -01 22 03.9   22.4y 16EW397   T09  C~8SZf      
2016 03  04.47095  11 39 23.77   -01 11 16.6   22.6i 16EW397   T09  C~8SZf      
2016 03  04.47636  11 39 23.74   -01 11 16.3   22.5i 16EW397   T09  C~8SZf      
2016 03  04.47910  11 39 23.73   -01 11 16.1   22.6i 16EW397   T09  C~8SZf      
2016 03  04.48179  11 39 23.72   -01 11 16.3   22.6i 16EW397   T09  C~8SZf      
2016 03  04.49868  11 39 23.63   -01 11 15.6   22.5i 16EW397   T09  C~8SZf      
2016 03  04.50136  11 39 23.62   -01 11 15.5   22.5i 16EW397   T09  C~8SZf      
2016 03  04.52178  11 39 23.52   -01 11 14.9   22.5i 16EW397   T09  C~8SZf      
2016 03  28.134845 11 37 27.727  -00 57 06.59  22.8V 16EW397   W84  C~8Wk6      
2016 03  28.138013 11 37 27.710  -00 57 06.55  22.9V 16EW397   W84  C~8Wk6      
2016 03  28.144416 11 37 27.674  -00 57 06.26  22.9V 16EW397   W84  C~8Wk6      
2016 04  04.28576  11 36 54.33   -00 52 49.9   22.8g 16EW397   T09  C~8SZf      
2016 04  04.29925  11 36 54.27   -00 52 49.4   23.2g 16EW397   T09  C~8SZf      
2016 04  04.31200  11 36 54.22   -00 52 48.9   23.3g 16EW397   T09  C~8SZf      
2016 04  04.31412  11 36 54.21   -00 52 48.9   23.4g 16EW397   T09  C~8SZf      
2016 04  08.142143 11 36 37.106  -00 50 34.22  23.3g 16EW397   W84  C~8Wk6      
2016 04  08.143315 11 36 37.116  -00 50 34.08  23.0g 16EW397   W84  C~8Wk6      

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    -0.06       0.00     0.22
     2   0.0001     -1.89     0.02      -0.16     0.05
     3   0.0002     -3.64     0.08      -0.27    -0.06
     4   0.0002     -4.68    -0.05      -0.50    -0.30
     5   0.0573  -1553.02     0.02      34.92    -0.02
     6   0.0573  -1553.55    -0.07      35.01     0.06
     7   0.0573  -1553.77    -0.06      35.14     0.18
     8   0.0573  -1553.83     0.10      34.89    -0.07
     9   0.0573  -1555.34    -0.04      35.00     0.00
    10   0.0573  -1555.52     0.01      35.03     0.03
    11   0.0574  -1557.14     0.06      34.99    -0.06
    12   0.1220  -3488.12     0.07     123.70     0.06
    13   0.1221  -3488.36     0.08     123.64    -0.01
    14   0.1221  -3488.98    -0.01     123.69     0.01
    15   0.1416  -4049.95    -0.17     160.27    -0.09
    16   0.1417  -4050.97    -0.15     160.37    -0.06
    17   0.1417  -4051.86    -0.04     160.53     0.04
    18   0.1417  -4052.00    -0.02     160.47    -0.03
    19   0.1522  -4341.04     0.04     182.14    -0.08
    20   0.1522  -4340.96     0.21     182.33     0.11

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.

16EW397    quality flag:1

Type:       SCATEXTD  SCATNEAR     5:3EE

axisobj        44.797    49.825    42.044
ecceobj         0.192     0.277     0.174
incobj         12.843    12.336    13.329
qmin           35.246    34.944    33.065
qmax           55.019    65.881    52.280
amean          44.958    50.062    42.327
amin           44.556    49.482    41.863
amax           45.415    50.723    42.839
emean           0.195     0.282     0.187
emin            0.178     0.265     0.149
emax            0.214     0.301     0.221
imean          12.720    12.039    13.269
imin           11.870    11.113    12.332
imax           13.633    13.028    14.766
excite_mean     0.294     0.351     0.296
fracstop        1.000     1.000     1.000
cjmean          3.008     3.021     2.978

libcent 0      -180.0    -180.0     180.3
libamp  0      -180.0    -180.0      86.0
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       173.6     173.1     184.0
kozaiamp        180.0     179.9     180.0