Orbit Fit and Astrometric record for 23BF9

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: 23BF9     
# Created Tue May  7 01:18:16 2024
# Orbit generated from Bernstein formalism
# Fitting     22 observations of     22
# Arc:   6.01d
# First observation: 2023/01/17
#  Last observation: 2023/01/23
Preliminary a, adot, b, bdot, g, gdot:
  -0.000000   0.094279  -0.000001   0.008457   0.049301   0.000000
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# WARNING Fitting with energy constraint
# Chi-squared of fit:     8.70 DOF:     39 RMS:  0.11
# Min/Max residuals:    -0.31    0.30
# Exact a, adot, b, bdot, g, gdot:
  2.271598E-05  7.781248E-02  2.584792E-06  1.186275E-02  5.395272E-02  1.424006E-03
# Covariance matrix:
  5.3461E-12  1.7543E-08 -1.6254E-12 -3.6244E-09 -4.9428E-09 -2.5952E-07
  1.7543E-08  6.1019E-05 -5.6086E-09 -1.2579E-05 -1.7135E-05 -8.6756E-04
 -1.6254E-12 -5.6086E-09  7.2000E-13  1.1382E-09  1.5764E-09  8.0985E-08
 -3.6244E-09 -1.2579E-05  1.1382E-09  2.5959E-06  3.5329E-06  1.7930E-04
 -4.9428E-09 -1.7135E-05  1.5764E-09  3.5329E-06  4.8133E-06  2.4486E-04
 -2.5952E-07 -8.6756E-04  8.0985E-08  1.7930E-04  2.4486E-04  1.3424E-02
#      lat0       lon0       xBary       yBary       zBary        JD0
    8.496303   -7.374735   -0.815608   -0.082503    0.551125  2459961.725770
# Heliocentric elements and errors
Epoch:              2459960.5000  =  2023/01/16
Mean Anomaly:          107.56482 +/-   172.081
Argument of Peri:      292.18466 +/-   181.535
Long of Asc Node:      308.94826 +/-     7.770
Inclination:            12.01036 +/-     1.503
Eccentricity:         0.06753807 +/-    1.4568
Semi-Major Axis:     17.58197893 +/-    5.1476
Time of Perihelion: 2451914.7262 +/-   12377.0
Perihelion:          16.39452593 +/-   26.0588
Aphelion:            18.76943193 +/-   26.1958
Period (y)               73.7242 +/-     32.38
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           17.74081616 +/-    0.7393
Ecliptic Y           -1.47211897 +/-    0.0956
Ecliptic Z            2.73843465 +/-    0.1113
Ecliptic XDOT         0.00048836 +/-    0.0057
Ecliptic YDOT         0.00392716 +/-    0.0013
Ecliptic ZDOT         0.00060600 +/-    0.0009
# Distances at JD0 (AU)
Heliocenter to KBO   18.01118310 +/-    0.7284
Geocenter to KBO     18.53474826 +/-    0.7537
# Hcoef: 10.71

The following table shows the complete astrometric record for 23BF9. 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 (23BF9) followed by the observatory code and reference code for the source of the astrometry.

2023 01  17.224969 23 19 28.814  +04 52 45.34  23.4r 23BF9     T09  C~6DMH      
2023 01  17.239167 23 19 28.954  +04 52 45.73  23.6r 23BF9     T09  C~6DMH      
2023 01  17.253308 23 19 29.093  +04 52 46.49  23.7r 23BF9     T09  C~6DMH      
2023 01  17.267465 23 19 29.232  +04 52 47.06  23.6r 23BF9     T09  C~6DMH      
2023 01  18.229936 23 19 38.736  +04 53 30.41  23.4V 23BF9     T09  C~6DMH      
2023 01  18.241207 23 19 38.837  +04 53 30.48  23.5V 23BF9     T09  C~6DMH      
2023 01  18.252514 23 19 38.945  +04 53 31.20  23.5V 23BF9     T09  C~6DMH      
2023 01  20.226139 23 19 58.863  +04 55 03.64  22.9G 23BF9     T14  C~6DMH      
2023 01  20.227696 23 19 58.874  +04 55 04.05  23.5G 23BF9     T14  C~6DMH      
2023 01  20.229251 23 19 58.914  +04 55 04.11  23.4G 23BF9     T14  C~6DMH      
2023 01  20.230808 23 19 58.904  +04 55 04.18  23.1G 23BF9     T14  C~6DMH      
2023 01  20.239033 23 19 58.989  +04 55 04.46  23.5G 23BF9     T14  C~6DMH      
2023 01  20.240592 23 19 58.999  +04 55 04.64  23.9G 23BF9     T14  C~6DMH      
2023 01  20.242158 23 19 59.038  +04 55 04.81  23.4G 23BF9     T14  C~6DMH      
2023 01  20.243923 23 19 59.047  +04 55 04.84  22.7G 23BF9     T14  C~6DMH      
2023 01  21.231696 23 20 09.223  +04 55 52.90  24.1r 23BF9     T09  C~6DMH      
2023 01  21.240161 23 20 09.305  +04 55 53.33  23.5r 23BF9     T09  C~6DMH      
2023 01  21.248601 23 20 09.391  +04 55 53.83  23.7r 23BF9     T09  C~6DMH      
2023 01  21.257078 23 20 09.485  +04 55 54.19  23.5r 23BF9     T09  C~6DMH      
2023 01  23.232092 23 20 30.268  +04 57 34.35  23.0G 23BF9     T14  C~6DMH      
2023 01  23.233651 23 20 30.285  +04 57 34.44  23.3G 23BF9     T14  C~6DMH      
2023 01  23.235207 23 20 30.294  +04 57 34.52  23.0G 23BF9     T14  C~6DMH      

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     0.02       0.00     0.18
     2   0.0000      2.08    -0.04      -0.47    -0.05
     3   0.0001      4.28     0.04      -0.59     0.07
     4   0.0001      6.42     0.04      -0.89     0.01
     5   0.0028    154.02     0.14     -17.32     0.04
     6   0.0028    155.43    -0.17     -17.85    -0.31
     7   0.0028    157.20    -0.13     -17.83    -0.10
     8   0.0082    467.15    -0.09     -50.76    -0.23
     9   0.0082    467.47    -0.02     -50.45     0.11
    10   0.0082    468.04     0.30     -50.63    -0.05
    11   0.0082    467.93    -0.05     -50.51     0.10
    12   0.0083    469.21    -0.07     -50.75    -0.02
    13   0.0083    469.41    -0.11     -50.65     0.12
    14   0.0083    470.02     0.24     -50.72     0.07
    15   0.0083    470.15     0.10     -50.75     0.07
    16   0.0110    628.84    -0.04     -66.79    -0.04
    17   0.0110    630.13    -0.10     -66.88     0.00
    18   0.0110    631.51    -0.08     -66.93     0.09
    19   0.0110    632.94    -0.01     -67.16    -0.01
    20   0.0164    957.82     0.04     -98.04    -0.04
    21   0.0165    958.09     0.05     -98.06    -0.03
    22   0.0165    958.24    -0.05     -98.04     0.01

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.

23BF9    quality flag:0

Type:      ERR2LARGE ERR2LARGE ERR2LARGE

axisobj         0.000     0.000     0.000
ecceobj        -1.000    -1.000    -1.000
incobj         -1.000    -1.000    -1.000
qmin            0.000     0.000     0.000
qmax            0.000     0.000     0.000
amean           0.000     0.000     0.000
amin            0.000     0.000     0.000
amax            0.000     0.000     0.000
emean           0.000     0.000     0.000
emin            0.000     0.000     0.000
emax            0.000     0.000     0.000
imean           0.000     0.000     0.000
imin            0.000     0.000     0.000
imax            0.000     0.000     0.000
excite_mean     0.000     0.000     0.000
fracstop        0.000     0.000     0.000
cjmean          0.000     0.000     0.000

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         0.0       0.0       0.0
kozaiamp          0.0       0.0       0.0