Orbit Fit and Astrometric record for 17DO177

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: 17DO177   
# Created Sun Dec 22 02:10:59 2024
# Orbit generated from Bernstein formalism
# Fitting     22 observations of     22
# Arc:  60.86d
# First observation: 2017/01/23
#  Last observation: 2017/03/25
Preliminary a, adot, b, bdot, g, gdot:
  -0.000038   0.042317   0.000013  -0.007549   0.032387   0.000000
# Chi-squared of fit:    12.75 DOF:     38 RMS:  0.13
# Min/Max residuals:    -0.35    0.26
# Exact a, adot, b, bdot, g, gdot:
  1.794397E-05  3.486548E-02 -3.724639E-06 -7.521560E-03  3.118570E-02  3.339657E-03
# Covariance matrix:
  4.8110E-13  2.2695E-12  2.2233E-14 -3.0567E-13  1.6878E-12  2.0165E-10
  2.2695E-12  2.9062E-08  6.2501E-11 -1.0254E-10  4.6112E-09 -4.0050E-08
  2.2233E-14  6.2501E-11  4.6437E-13 -2.7758E-12  9.9978E-12 -6.9835E-11
 -3.0567E-13 -1.0254E-10 -2.7758E-12  2.5356E-11 -1.8048E-11 -2.5577E-10
  1.6878E-12  4.6112E-09  9.9978E-12 -1.8048E-11  7.3790E-10 -5.0869E-09
  2.0165E-10 -4.0050E-08 -6.9835E-11 -2.5577E-10 -5.0869E-09  3.4178E-07
#      lat0       lon0       xBary       yBary       zBary        JD0
   -8.385333  152.792786    0.488871   -0.124681   -0.847121  2457776.921781
# Heliocentric elements and errors
Epoch:              2457770.5000  =  2017/01/17
Mean Anomaly:           31.92313 +/-     5.180
Argument of Peri:      173.07719 +/-     7.173
Long of Asc Node:      298.84994 +/-     0.126
Inclination:            14.72693 +/-     0.048
Eccentricity:         0.12812764 +/-    0.0110
Semi-Major Axis:     36.70865994 +/-    0.2434
Time of Perihelion: 2450566.8229 +/-    1166.7
Perihelion:          32.00526597 +/-    0.4552
Aphelion:            41.41205391 +/-    0.4874
Period (y)              222.4134 +/-      2.21
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -28.75485821 +/-    0.0246
Ecliptic Y           15.32581361 +/-    0.0126
Ecliptic Z           -4.67632500 +/-    0.0041
Ecliptic XDOT        -0.00156897 +/-    0.0000
Ecliptic YDOT        -0.00264035 +/-    0.0000
Ecliptic ZDOT        -0.00069609 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   32.91793507 +/-    0.0223
Geocenter to KBO     32.06597789 +/-    0.0279
# Hcoef:  9.49

The following table shows the complete astrometric record for 17DO177. 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 (17DO177) followed by the observatory code and reference code for the source of the astrometry.

2017 01  23.42098  10 06 57.04   +02 38 37.8   24.9r 17DO177   T09  C~8HKf      
2017 01  23.45863  10 06 56.85   +02 38 38.4   24.5r 17DO177   T09  C~8HKf      
2017 01  23.49339  10 06 56.66   +02 38 38.9   24.3i 17DO177   T09  C~8HKf      
2017 02  21.34603  10 04 12.92   +02 49 43.6   23.7z 17DO177   T09  C~8HKf      
2017 02  21.37159  10 04 12.78   +02 49 44.1   23.8z 17DO177   T09  C~8HKf      
2017 02  21.41923  10 04 12.50   +02 49 45.6   23.8z 17DO177   T09  C~8HKf      
2017 02  23.33107  10 04 01.27   +02 50 40.2   25.8g 17DO177   T09  C~8HKf      
2017 02  23.47842  10 04 00.36   +02 50 44.8   25.5r 17DO177   T09  C~8HKf      
2017 02  23.49203  10 04 00.30   +02 50 45.1   25.2r 17DO177   T09  C~8HKf      
2017 03  04.28899  10 03 09.52   +02 55 07.7   24.2z 17DO177   T09  C~8HKf      
2017 03  04.31448  10 03 09.37   +02 55 08.7   24.0z 17DO177   T09  C~8HKf      
2017 03  04.34002  10 03 09.22   +02 55 09.2   23.8z 17DO177   T09  C~8HKf      
2017 03  04.45244  10 03 08.59   +02 55 12.9   24.2i 17DO177   T09  C~8HKf      
2017 03  04.47432  10 03 08.46   +02 55 13.5   24.4i 17DO177   T09  C~8HKf      
2017 03  04.49602  10 03 08.33   +02 55 14.1   24.7i 17DO177   T09  C~8HKf      
2017 03  22.28126  10 01 35.07   +03 04 21.8   24.9g 17DO177   T09  C~8HKf      
2017 03  22.29509  10 01 35.01   +03 04 22.5   25.3g 17DO177   T09  C~8HKf      
2017 03  22.48627  10 01 34.09   +03 04 28.0   24.5z 17DO177   T09  C~8HKf      
2017 03  25.24382  10 01 21.35   +03 05 51.4   24.6r 17DO177   T09  C~8HKf      
2017 03  25.25752  10 01 21.27   +03 05 52.0   25.0r 17DO177   T09  C~8HKf      
2017 03  25.27122  10 01 21.22   +03 05 52.4   24.6r 17DO177   T09  C~8HKf      
2017 03  25.28496  10 01 21.17   +03 05 52.9   24.9r 17DO177   T09  C~8HKf      

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    -0.05       0.00    -0.02
     2   0.0001     -2.87     0.05      -0.45     0.02
     3   0.0002     -5.71    -0.03      -0.99    -0.07
     4   0.0792  -2535.61    -0.06    -247.48     0.18
     5   0.0793  -2537.75     0.20    -247.76     0.03
     6   0.0794  -2542.21     0.22    -247.84     0.19
     7   0.0846  -2718.92     0.20    -256.26    -0.18
     8   0.0850  -2733.30    -0.35    -256.77    -0.04
     9   0.0851  -2734.25    -0.02    -256.81    -0.02
    10   0.1092  -3538.88    -0.03    -280.08    -0.10
    11   0.1092  -3541.34    -0.16    -279.94     0.09
    12   0.1093  -3543.62    -0.10    -280.27    -0.19
    13   0.1096  -3553.76     0.05    -280.14     0.15
    14   0.1097  -3555.79     0.02    -280.27     0.07
    15   0.1097  -3557.83    -0.03    -280.39    -0.02
    16   0.1584  -5058.89     0.02    -261.46    -0.26
    17   0.1585  -5059.97     0.01    -261.12     0.04
    18   0.1590  -5074.82     0.17    -260.84    -0.23
    19   0.1665  -5282.93     0.06    -250.18    -0.05
    20   0.1666  -5284.26    -0.24    -250.04     0.04
    21   0.1666  -5285.10    -0.05    -249.93     0.10
    22   0.1666  -5285.98     0.11    -249.73     0.26

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.

17DO177    quality flag:1

Type:           4:3E  SCATNEAR  CENTAURS

axisobj        36.627    37.595    35.732
ecceobj         0.128     0.157     0.106
incobj         14.724    14.613    14.866
qmin           31.413    31.369    29.059
qmax           41.783    44.475    42.441
amean          36.478    37.694    35.835
amin           36.124    37.244    35.225
amax           36.869    38.174    36.473
emean           0.108     0.107     0.092
emin            0.081     0.047     0.023
emax            0.136     0.169     0.181
imean          16.441    19.681    17.706
imin           14.844    16.145    15.202
imax           17.825    22.103    20.057
excite_mean     0.303     0.354     0.319
fracstop        1.000     1.000     1.000
cjmean          2.924     2.889     2.911

libcent 0       178.3    -180.0    -180.0
libamp  0        91.3    -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       180.2     178.1     185.9
kozaiamp        180.0     180.0     180.0