Orbit Fit and Astrometric record for 17BZ236

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: 17BZ236   
# Created Sun Dec 22 02:10:55 2024
# Orbit generated from Bernstein formalism
# Fitting     35 observations of     35
# Arc:   4.05y
# First observation: 2015/03/16
#  Last observation: 2019/04/03
Preliminary a, adot, b, bdot, g, gdot:
  -0.002272   0.037530  -0.000771   0.012859   0.028615   0.000000
# Chi-squared of fit:    12.23 DOF:     64 RMS:  0.10
# Min/Max residuals:    -0.25    0.24
# Exact a, adot, b, bdot, g, gdot:
  1.869834E-05  3.520394E-02  6.953598E-06  1.208148E-02  2.901920E-02 -1.400664E-02
# Covariance matrix:
  5.7221E-13 -5.5035E-13  1.2987E-13 -1.5306E-13  8.8385E-15 -2.8506E-12
 -5.5035E-13  6.0938E-13 -1.5815E-13  1.8656E-13  1.4874E-14  3.4739E-12
  1.2987E-13 -1.5815E-13  2.3905E-13 -1.5013E-13 -1.1345E-14 -1.0087E-12
 -1.5306E-13  1.8656E-13 -1.5013E-13  1.2429E-13  1.4358E-14  1.1910E-12
  8.8385E-15  1.4874E-14 -1.1345E-14  1.4358E-14  1.4890E-13  2.6483E-13
 -2.8506E-12  3.4739E-12 -1.0087E-12  1.1910E-12  2.6483E-13  2.2176E-11
#      lat0       lon0       xBary       yBary       zBary        JD0
    0.592415 -176.943410    0.133299    0.010292   -0.982532  2457097.954950
# Heliocentric elements and errors
Epoch:              2457090.5000  =  2015/03/09
Mean Anomaly:          354.28209 +/-     0.003
Argument of Peri:       51.31426 +/-     0.012
Long of Asc Node:      181.16172 +/-     0.000
Inclination:            18.94405 +/-     0.000
Eccentricity:         0.73567832 +/-    0.0001
Semi-Major Axis:    114.14664999 +/-    0.0433
Time of Perihelion: 2464165.5242 +/-       1.1
Perihelion:          30.17143478 +/-    0.0176
Aphelion:           198.12186519 +/-    0.0763
Period (y)             1219.5594 +/-      0.69
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -35.40046239 +/-    0.0005
Ecliptic Y           -1.75686550 +/-    0.0000
Ecliptic Z            0.35654680 +/-    0.0000
Ecliptic XDOT         0.00150496 +/-    0.0000
Ecliptic YDOT        -0.00325130 +/-    0.0000
Ecliptic ZDOT         0.00112621 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   35.44582400 +/-    0.0005
Geocenter to KBO     34.45994912 +/-    0.0005
# Hcoef:  9.23

The following table shows the complete astrometric record for 17BZ236. 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 (17BZ236) followed by the observatory code and reference code for the source of the astrometry.

2015 03  16.454172 12 12 09.64   -00 40 18.1         17BZ236   T09  C~86uk      
2015 03  16.554822 12 12 09.14   -00 40 14.1         17BZ236   T09  C~86uk      
2016 04  02.379703 12 19 20.63   -00 38 45.8         17BZ236   T09  C~86uk      
2016 04  02.38998  12 19 20.56   -00 38 45.3   24.2i 17BZ236   T09  C~89UT      
2016 04  02.40920  12 19 20.47   -00 38 44.6   24.3i 17BZ236   T09  C~89UT      
2016 04  02.46633  12 19 20.17   -00 38 42.3   24.4i 17BZ236   T09  C~89UT      
2016 04  02.51252  12 19 19.95   -00 38 40.4   23.8i 17BZ236   T09  C~89UT      
2016 04  02.51521  12 19 19.95   -00 38 40.3   24.0i 17BZ236   T09  C~89UT      
2016 04  04.34598  12 19 10.99   -00 37 28.8   25.2g 17BZ236   T09  C~89UT      
2016 04  04.36164  12 19 10.89   -00 37 28.3   25.3g 17BZ236   T09  C~89UT      
2016 04  04.38727  12 19 10.78   -00 37 27.5   25.3g 17BZ236   T09  C~89UT      
2016 04  04.40435  12 19 10.68   -00 37 26.7   25.9g 17BZ236   T09  C~89UT      
2016 04  04.40648  12 19 10.68   -00 37 26.7   25.0g 17BZ236   T09  C~89UT      
2016 06  04.251947 12 15 52.14   -00 09 57.4         17BZ236   T09  C~86uk      
2016 06  04.270359 12 15 52.14   -00 09 57.2         17BZ236   T09  C~86uk      
2016 06  04.335164 12 15 52.06   -00 09 56.5         17BZ236   T09  C~86uk      
2016 06  05.339160 12 15 51.32   -00 09 46.6         17BZ236   T09  C~86uk      
2017 01  23.607577 12 32 34.07   -01 28 03.3         17BZ236   T09  C~86uk      
2017 01  23.618266 12 32 34.05   -01 28 03.2         17BZ236   T09  C~86uk      
2017 01  28.59808  12 32 26.75   -01 26 21.4   24.4z 17BZ236   T09  C~81Bp      
2017 01  28.61959  12 32 26.70   -01 26 21.0   24.1z 17BZ236   T09  C~81Bp      
2017 01  28.65069  12 32 26.64   -01 26 20.2   24.5z 17BZ236   T09  C~81Bp      
2017 01  28.65336  12 32 26.63   -01 26 20.0   24.6z 17BZ236   T09  C~81Bp      
2017 02  02.60942  12 32 16.88   -01 24 23.3   24.8i 17BZ236   T09  C~81Bp      
2017 02  02.63614  12 32 16.81   -01 24 22.6   24.4i 17BZ236   T09  C~81Bp      
2017 02  02.64454  12 32 16.80   -01 24 22.6   24.2i 17BZ236   T09  C~81Bp      
2017 02  02.65294  12 32 16.76   -01 24 22.3   24.3i 17BZ236   T09  C~81Bp      
2017 02  23.52167  12 31 11.87   -01 13 47.4   24.5r 17BZ236   T09  C~81Bp      
2017 02  23.52446  12 31 11.86   -01 13 47.3   24.5r 17BZ236   T09  C~81Bp      
2017 02  23.56346  12 31 11.70   -01 13 45.8   24.5r 17BZ236   T09  C~81Bp      
2017 02  23.59748  12 31 11.56   -01 13 44.8   24.4r 17BZ236   T09  C~81Bp      
2017 02  23.62726  12 31 11.44   -01 13 43.7   24.9r 17BZ236   T09  C~81Bp      
2017 02  23.63774  12 31 11.41   -01 13 43.3   24.5r 17BZ236   T09  C~81Bp      
2019 04  03.445387 12 46 39.84   -01 09 48.6         17BZ236   T09  C~86uk      
2019 04  03.474912 12 46 39.68   -01 09 47.4         17BZ236   T09  C~86uk      

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     0.10       0.00    -0.08
     2   0.0003     -8.47     0.06       0.69    -0.03
     3   1.0484   5898.25     0.14    2652.42     0.00
     4   1.0484   5897.08    -0.15    2652.46    -0.02
     5   1.0485   5895.57    -0.04    2652.57    -0.03
     6   1.0486   5890.52    -0.25    2652.90    -0.05
     7   1.0488   5886.73    -0.13    2653.33     0.10
     8   1.0488   5886.69     0.06    2653.42     0.18
     9   1.0538   5734.83     0.07    2665.68     0.24
    10   1.0538   5733.25    -0.19    2665.55     0.01
    11   1.0539   5731.42     0.13    2665.63    -0.07
    12   1.0539   5729.72    -0.13    2665.77    -0.03
    13   1.0539   5729.72     0.05    2665.77    -0.04
    14   1.2205   2340.01    -0.04    2996.80    -0.19
    15   1.2206   2339.93     0.18    2996.99    -0.08
    16   1.2208   2338.55    -0.13    2997.15    -0.17
    17   1.2235   2324.43     0.15    3001.83    -0.06
    18   1.8594  18042.51     0.10    4664.62     0.05
    19   1.8595  18042.20     0.06    4664.59    -0.08
    20   1.8731  17900.33     0.14    4714.84     0.02
    21   1.8731  17899.47     0.02    4714.91    -0.11
    22   1.8732  17898.32    -0.07    4715.29    -0.02
    23   1.8732  17898.10    -0.20    4715.41     0.08
    24   1.8868  17716.31     0.04    4764.75     0.17
    25   1.8869  17715.06    -0.09    4764.98     0.15
    26   1.8869  17714.92     0.13    4764.92     0.01
    27   1.8869  17714.24    -0.19    4764.96    -0.03
    28   1.9441  16561.28     0.05    4962.43     0.03
    29   1.9441  16561.10     0.07    4962.46     0.04
    30   1.9442  16558.28    -0.03    4962.89     0.14
    31   1.9443  16555.94    -0.00    4962.98    -0.07
    32   1.9443  16553.84    -0.04    4963.27    -0.02
    33   1.9444  16553.27     0.12    4963.46     0.08
    34   4.0493  29432.51     0.04   10758.53    -0.05
    35   4.0493  29429.77    -0.03   10758.68    -0.08

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.

17BZ236    quality flag:2

Type:       CENTAURR  CENTAURS  CENTAURS

axisobj       110.526   110.617   110.435
ecceobj         0.728     0.728     0.727
incobj         19.019    19.019    19.020
qmin           28.455    28.729    28.565
qmax          212.727   214.456   237.317
amean         113.652   110.892   118.996
amin          104.822    99.489   106.180
amax          121.256   122.826   134.189
emean           0.737     0.726     0.744
emin            0.702     0.686     0.700
emax            0.754     0.752     0.772
imean          17.943    18.921    18.689
imin           16.535    17.148    16.675
imax           20.479    21.590    22.028
excite_mean     0.799     0.795     0.811
fracstop        0.529     1.000     1.000
cjmean          2.762     2.766     2.765

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       114.0     155.0     172.2
kozaiamp         62.0     108.1     114.3