Orbit Fit and Astrometric record for 22LW15

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: 22LW15    
# Created Wed Nov 27 02:11:11 2024
# Orbit generated from Bernstein formalism
# Fitting      6 observations of      6
# Arc:  26.14d
# First observation: 2022/06/03
#  Last observation: 2022/06/29
Preliminary a, adot, b, bdot, g, gdot:
   0.000000   0.025838  -0.000000  -0.007464   0.028182   0.000000
# WARNING Fitting with energy constraint
# WARNING MRQMIN stopped after  21 iterations -- oscilliatory solution
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# Chi-squared of fit:     0.04 DOF:      7 RMS:  0.01
# Min/Max residuals:    -0.02    0.03
# Exact a, adot, b, bdot, g, gdot:
  1.509560E-05  2.730791E-02 -4.153238E-06 -7.443793E-03  2.834412E-02  1.014533E-02
# Covariance matrix:
  2.1707E-10  4.0733E-07 -1.9823E-12 -2.5598E-09  7.0805E-08 -6.4029E-07
  4.0733E-07  7.6610E-04 -3.7279E-09 -4.8134E-06  1.3316E-04 -1.2061E-03
 -1.9823E-12 -3.7279E-09  5.0342E-13  1.6653E-11 -6.4815E-10  5.7711E-09
 -2.5598E-09 -4.8134E-06  1.6653E-11  3.0563E-08 -8.3708E-07  7.3283E-06
  7.0805E-08  1.3316E-04 -6.4815E-10 -8.3708E-07  2.3148E-05 -2.0884E-04
 -6.4029E-07 -1.2061E-03  5.7711E-09  7.3283E-06 -2.0884E-04  2.3844E-03
#      lat0       lon0       xBary       yBary       zBary        JD0
    0.984575  -72.219003    0.593133    0.013888   -0.823757  2459733.941661
# Heliocentric elements and errors
Epoch:              2459730.5000  =  2022/05/31
Mean Anomaly:           66.24487 +/-    88.065
Argument of Peri:       72.80180 +/-   158.896
Long of Asc Node:      110.40906 +/-     3.227
Inclination:            15.14532 +/-    13.775
Eccentricity:         0.32112188 +/-    1.7015
Semi-Major Axis:     37.24427356 +/-   19.2871
Time of Perihelion: 2444453.5218 +/-   16481.2
Perihelion:          25.28432226 +/-   64.7112
Aphelion:            49.20422486 +/-   68.3035
Period (y)              227.2990 +/-    176.56
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           10.46868594 +/-    1.8281
Ecliptic Y          -34.55789076 +/-    5.7019
Ecliptic Z            0.60616564 +/-    0.1029
Ecliptic XDOT         0.00281648 +/-    0.0010
Ecliptic YDOT        -0.00013026 +/-    0.0053
Ecliptic ZDOT        -0.00070219 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   36.11382887 +/-    5.4819
Geocenter to KBO     35.28068147 +/-    5.9887
# Hcoef:  9.46

The following table shows the complete astrometric record for 22LW15. 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 (22LW15) followed by the observatory code and reference code for the source of the astrometry.

2022 06  03.44086  19 16 30.724  -21 16 54.29  24.2r 22LW15    266  C~6Ipb      
2022 06  03.52767  19 16 30.316  -21 16 55.32  24.2r 22LW15    266  C~6Ipb      
2022 06  03.61505  19 16 29.903  -21 16 56.34  24.2r 22LW15    266  C~6Ipb      
2022 06  29.45230  19 14 12.761  -21 22 37.45  25.7r 22LW15    266  C~6Ipb      
2022 06  29.51532  19 14 12.389  -21 22 38.35  25.7r 22LW15    266  C~6Ipb      
2022 06  29.57836  19 14 12.019  -21 22 39.23  25.7r 22LW15    266  C~6Ipb      

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     0.03       0.00     0.00
     2   0.0002     -5.79     0.01      -0.28    -0.00
     3   0.0005    -11.64    -0.02      -0.54    -0.01
     4   0.0712  -1955.87    -0.01     -92.50     0.00
     5   0.0714  -1961.14     0.00     -92.73    -0.00
     6   0.0716  -1966.38     0.03     -92.95    -0.00

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.

22LW15    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