Orbit Fit and Astrometric record for 17DO164

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: 17DO164   
# Created Sun Dec 22 02:10:57 2024
# Orbit generated from Bernstein formalism
# Fitting     22 observations of     23
# Arc:   1.93y
# First observation: 2015/03/30
#  Last observation: 2017/03/04
Preliminary a, adot, b, bdot, g, gdot:
  -0.000045   0.017423  -0.000001   0.009929   0.022298   0.000000
# Chi-squared of fit:     6.16 DOF:     38 RMS:  0.09
# Min/Max residuals:    -0.16    0.25
# Exact a, adot, b, bdot, g, gdot:
  1.219624E-05  1.753808E-02  6.727886E-06  1.003253E-02  2.267741E-02  2.591303E-03
# Covariance matrix:
  6.9699E-13 -8.4490E-13  6.0056E-14 -2.5716E-13 -3.3744E-13 -1.2360E-11
 -8.4490E-13  3.6948E-12 -4.6679E-13  2.0280E-12  3.9198E-12  9.7060E-11
  6.0056E-14 -4.6679E-13  6.2074E-13 -5.9279E-13 -5.7189E-13 -1.3415E-11
 -2.5716E-13  2.0280E-12 -5.9279E-13  1.4216E-12  2.5010E-12  5.8436E-11
 -3.3744E-13  3.9198E-12 -5.7189E-13  2.5010E-12  5.5313E-12  1.1947E-10
 -1.2360E-11  9.7060E-11 -1.3415E-11  5.8436E-11  1.1947E-10  2.7947E-09
#      lat0       lon0       xBary       yBary       zBary        JD0
    2.263196 -173.543723   -0.046988    0.039397   -0.993647  2457111.853967
# Heliocentric elements and errors
Epoch:              2457110.5000  =  2015/03/29
Mean Anomaly:          112.68053 +/-     0.560
Argument of Peri:      237.26614 +/-     0.525
Long of Asc Node:      182.64407 +/-     0.000
Inclination:            29.78859 +/-     0.001
Eccentricity:         0.14864495 +/-    0.0019
Semi-Major Axis:     41.96893916 +/-    0.0177
Time of Perihelion: 2426026.5081 +/-     153.3
Perihelion:          35.73046837 +/-    0.0821
Aphelion:            48.20740995 +/-    0.0833
Period (y)              271.8944 +/-      0.17
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -44.76883159 +/-    0.0045
Ecliptic Y           -5.11326507 +/-    0.0005
Ecliptic Z            1.74169278 +/-    0.0002
Ecliptic XDOT        -0.00002832 +/-    0.0000
Ecliptic YDOT        -0.00213957 +/-    0.0000
Ecliptic ZDOT         0.00122273 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   45.09353896 +/-    0.0045
Geocenter to KBO     44.09674388 +/-    0.0046
# Hcoef:  7.85

The following table shows the complete astrometric record for 17DO164. 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 (17DO164) followed by the observatory code and reference code for the source of the astrometry.

2015 03  30.353189 12 27 17.46   -00 29 05.4         17DO164   T09  C~83F2      
2015 03  30.392045 12 27 17.29   -00 29 04.1         17DO164   T09  C~83F2      
2016 04  04.439690 12 31 29.20   -00 18 09.4         17DO164   T09  C~83F2      
2016 04  04.543002 12 31 28.77   -00 18 06.2         17DO164   T09  C~83F2      
2016 06  05.314338 12 28 24.29   +00 05 25.2         17DO164   T09  C~83F2      
2016 06  05.328496 12 28 24.27   +00 05 25.4         17DO164   T09  C~83F2      
2017 01  30.63419  12 39 39.98   -00 42 18.7   23.9z 17DO164   T09  C~81Bw      
2017 01  30.65438  12 39 39.93   -00 42 18.0   23.9z 17DO164   T09  C~81Bw      
2017 01  30.65709  12 39 39.92   -00 42 18.0   24.0z 17DO164   T09  C~81Bw      
2017 01  30.65979  12 39 39.93   -00 42 18.0   24.1z 17DO164   T09  C~81Bw      
2017 02  02.65568  12 39 34.52   -00 41 12.8   23.8i 17DO164   T09  C~81Bw      
2017 02  02.66205  12 39 34.52   -00 41 12.6   23.7i 17DO164   T09  C~81Bw      
2017 02  02.66476  12 39 34.51   -00 41 12.6   24.0i 17DO164   T09  C~81Bw      
2017 02  02.66749  12 39 34.50   -00 41 12.5   24.1i 17DO164   T09  C~81Bw      
2017 02  23.53862  12 38 40.04   -00 32 02.6   24.8r 17DO164   T09  C~81Bw      
2017 02  23.54142  12 38 40.04   -00 32 02.6   24.7r 17DO164   T09  C~81Bw      
2017 02  23.56764  12 38 39.95   -00 32 02.0   24.9r 17DO164   T09  C~81Bw      
2017 02  23.61010  12 38 39.82   -00 32 00.8   24.5r 17DO164   T09  C~81Bw      
2017 02  23.63983  12 38 39.71   -00 31 59.8   24.5r 17DO164   T09  C~81Bw      
2017 03  04.53892  12 38 09.00   -00 27 26.1   24.3y 17DO164   T09  C~81Bw      
2017 03  04.59319  12 38 08.80   -00 27 24.4   24.4y 17DO164   T09  C~81Bw      
2017 03  04.62835  12 38 08.64   -00 27 22.6   24.6y 17DO164   T09  C~81Bw      
2017 03  04.63107  12 38 08.66   -00 27 23.1   24.3y 17DO164   T09  C~81Bw      

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     0.01       0.00     0.06
     2   0.0001     -2.86    -0.07       0.19     0.04
     3   1.0160   3209.73     0.01    2095.14    -0.05
     4   1.0163   3202.54     0.13    2095.53    -0.15
     5   1.1854    102.40     0.02    2298.31    -0.01
     6   1.1854    102.04    -0.04    2298.37     0.03
     7   1.8406  10555.09     0.20    3674.30    -0.13
     8   1.8407  10554.12    -0.11    3674.65     0.03
     9   1.8407  10553.98    -0.16    3674.59    -0.05
    10   1.8407  10554.12     0.07    3674.65    -0.02
    11   1.8489  10453.56    -0.09    3702.52    -0.11
    12   1.8489  10453.48     0.06    3702.70     0.02
    13   1.8489  10453.35     0.02    3702.64    -0.06
    14   1.8489  10453.17    -0.06    3702.68    -0.05
    15   1.9061   9483.22    -0.10    3885.24     0.18
    16   1.9061   9483.22     0.06    3885.24     0.16
    17   1.9061   9481.74     0.08    3885.26    -0.02
    18   1.9062   9479.47     0.25    3885.59    -0.02
    19   1.9063   9477.56     0.04    3885.86     0.02
    20   1.9307   8945.15    -0.12    3955.28     0.02
    21   1.9308   8941.72    -0.09    3955.66     0.01
    22   1.9309   8938.80 (  -0.77)   3956.37 (   0.46)
    23   1.9309   8939.27    -0.12    3956.03     0.10

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.

17DO164    quality flag:3

Type:       SCATEXTD  SCATEXTD  SCATEXTD

axisobj        41.678    41.729    41.630
ecceobj         0.153     0.157     0.149
incobj         29.937    29.937    29.937
qmin           34.606    34.637    34.885
qmax           49.368    49.426    49.005
amean          41.805    41.870    41.807
amin           41.459    41.538    41.456
amax           42.216    42.232    42.190
emean           0.151     0.152     0.144
emin            0.133     0.135     0.130
emax            0.171     0.170     0.163
imean          29.625    29.695    29.692
imin           29.199    29.270    29.256
imax           30.095    30.171    30.104
excite_mean     0.517     0.518     0.516
fracstop        1.000     1.000     1.000
cjmean          2.746     2.745     2.747

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       181.0     178.6     177.8
kozaiamp        179.9     179.9     180.0