Orbit Fit and Astrometric record for 17EJ52

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: 17EJ52    
# Created Thu Oct 31 01:10:35 2024
# Orbit generated from Bernstein formalism
# Fitting     22 observations of     22
# Arc:   2.28y
# First observation: 2017/01/26
#  Last observation: 2019/05/09
Preliminary a, adot, b, bdot, g, gdot:
  -0.000005   0.016640   0.000040   0.021201   0.025228   0.000000
# Chi-squared of fit:    13.12 DOF:     38 RMS:  0.14
# Min/Max residuals:    -0.29    0.21
# Exact a, adot, b, bdot, g, gdot:
  1.107636E-05  1.665173E-02  1.380266E-05  2.148982E-02  2.522586E-02 -1.153764E-03
# Covariance matrix:
  1.6690E-13  3.7456E-14 -1.6566E-14  1.6616E-13  1.8902E-13  3.3505E-12
  3.7456E-14  2.1617E-13 -3.9941E-14  3.8926E-13  2.5976E-13  7.6568E-12
 -1.6566E-14 -3.9941E-14  1.2798E-13 -3.0825E-13 -5.0661E-14 -4.9081E-12
  1.6616E-13  3.8926E-13 -3.0825E-13  2.5080E-12  5.0607E-13  4.6574E-11
  1.8902E-13  2.5976E-13 -5.0661E-14  5.0607E-13  5.4234E-13  1.0169E-11
  3.3505E-12  7.6568E-12 -4.9081E-12  4.6574E-11  1.0169E-11  8.9414E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
  -13.375297  151.306836    0.417893   -0.206436   -0.868946  2457780.035371
# Heliocentric elements and errors
Epoch:              2457780.5000  =  2017/01/27
Mean Anomaly:          349.50619 +/-     0.236
Argument of Peri:      359.60882 +/-     0.365
Long of Asc Node:      160.72371 +/-     0.000
Inclination:            53.18690 +/-     0.001
Eccentricity:         0.20091029 +/-    0.0003
Semi-Major Axis:     50.37073265 +/-    0.0073
Time of Perihelion: 2461586.7434 +/-      85.5
Perihelion:          40.25073407 +/-    0.0161
Aphelion:            60.49073122 +/-    0.0173
Period (y)              357.4996 +/-      0.08
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -34.41720884 +/-    0.0010
Ecliptic Y           19.30750385 +/-    0.0005
Ecliptic Z           -9.16977803 +/-    0.0003
Ecliptic XDOT        -0.00123127 +/-    0.0000
Ecliptic YDOT        -0.00139149 +/-    0.0000
Ecliptic ZDOT         0.00229801 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   40.51430363 +/-    0.0009
Geocenter to KBO     39.64185488 +/-    0.0012
# Hcoef:  8.17

The following table shows the complete astrometric record for 17EJ52. 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 (17EJ52) followed by the observatory code and reference code for the source of the astrometry.

2017 01  26.53457  09 54 28.16   -01 30 54.2   23.7z 17EJ52    T09  C~7zpr      
2017 01  26.58033  09 54 27.95   -01 30 52.6   23.9z 17EJ52    T09  C~7zpr      
2017 01  26.59379  09 54 27.88   -01 30 52.5   23.5z 17EJ52    T09  C~7zpr      
2017 01  26.60454  09 54 27.85   -01 30 52.5   24.4z 17EJ52    T09  C~7zpr      
2017 02  02.373291 09 53 56.82   -01 27 27.2   23.5r 17EJ52    T09  C~81Bz      
2017 02  02.419471 09 53 56.60   -01 27 25.8   23.5r 17EJ52    T09  C~81Bz      
2017 03  06.37214  09 51 25.24   -01 06 54.2   24.2i 17EJ52    T09  C~7zpr      
2017 03  06.43229  09 51 24.95   -01 06 51.5   24.3i 17EJ52    T09  C~7zpr      
2017 03  06.44111  09 51 24.90   -01 06 51.3   24.7i 17EJ52    T09  C~7zpr      
2017 03  06.45254  09 51 24.86   -01 06 50.8   24.8i 17EJ52    T09  C~7zpr      
2017 03  06.45793  09 51 24.84   -01 06 50.8   24.7i 17EJ52    T09  C~7zpr      
2017 03  06.46334  09 51 24.81   -01 06 50.5   24.5i 17EJ52    T09  C~7zpr      
2017 03  22.238164 09 50 19.61   -00 55 14.7         17EJ52    T09  C~81Bz      
2017 03  22.245952 09 50 19.58   -00 55 14.5         17EJ52    T09  C~81Bz      
2017 03  22.252233 09 50 19.55   -00 55 14.2         17EJ52    T09  C~81Bz      
2018 01  17.499524 10 00 25.85   -00 45 45.3   23.6i 17EJ52    T09  C~81Bz      
2018 01  17.609722 10 00 25.40   -00 45 42.6   23.8i 17EJ52    T09  C~81Bz      
2019 05  09.252585 09 59 13.60   +01 13 43.5   23.7i 17EJ52    T09  C~81Bz      
2019 05  09.280721 09 59 13.61   +01 13 44.4         17EJ52    T09  C~81Bz      
2019 05  09.331772 09 59 13.59   +01 13 45.8         17EJ52    T09  C~81Bz      
2019 05  09.353382 09 59 13.58   +01 13 46.5         17EJ52    T09  C~81Bz      
2019 05  09.375023 09 59 13.58   +01 13 47.1   23.8i 17EJ52    T09  C~81Bz      

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    -0.07
     2   0.0001     -3.51    -0.25       0.40     0.20
     3   0.0002     -4.53    -0.28       0.13    -0.11
     4   0.0002     -4.95     0.10      -0.03    -0.29
     5   0.0187   -512.64     0.18      29.93     0.04
     6   0.0188   -516.22     0.21      30.09    -0.03
     7   0.1063  -3073.47     0.06     391.49     0.20
     8   0.1065  -3078.49    -0.19     392.50     0.21
     9   0.1065  -3079.26    -0.26     392.42    -0.01
    10   0.1066  -3080.00    -0.09     392.68     0.06
    11   0.1066  -3080.28     0.05     392.58    -0.14
    12   0.1066  -3080.81    -0.04     392.70    -0.10
    13   0.1498  -4240.51     0.17     703.09     0.10
    14   0.1498  -4241.00     0.21     703.12    -0.04
    15   0.1498  -4241.53     0.12     703.25    -0.05
    16   0.9746   4083.73     0.14    4411.01    -0.01
    17   0.9749   4076.45     0.12    4411.18     0.07
    18   2.2799    565.74    -0.09   10760.49    -0.02
    19   2.2799    565.57     0.11   10761.39     0.12
    20   2.2801    564.80     0.00   10762.60    -0.05
    21   2.2801    564.41    -0.10   10763.21    -0.03
    22   2.2802    564.20    -0.04   10763.77    -0.05

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.

17EJ52    quality flag:3

Type:       SCATEXTD  SCATEXTD  SCATEXTD

axisobj        50.349    50.372    50.327
ecceobj         0.198     0.199     0.198
incobj         53.327    53.329    53.324
qmin           38.946    38.957    38.930
qmax           62.053    62.104    61.963
amean          50.250    50.272    50.209
amin           49.804    49.834    49.751
amax           50.759    50.797    50.724
emean           0.207     0.207     0.207
emin            0.192     0.192     0.192
emax            0.222     0.223     0.222
imean          52.257    52.259    52.254
imin           52.003    51.994    51.992
imax           52.567    52.575    52.576
excite_mean     0.817     0.817     0.817
fracstop        1.000     1.000     1.000
cjmean          2.146     2.146     2.146

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        58.1      58.7      57.7
kozaiamp        180.0     180.0     180.0