Orbit Fit and Astrometric record for 22LM14

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: 22LM14    
# Created Wed Dec 25 02:11:17 2024
# Orbit generated from Bernstein formalism
# Fitting     21 observations of     21
# Arc:   2.01y
# First observation: 2021/09/06
#  Last observation: 2023/09/10
Preliminary a, adot, b, bdot, g, gdot:
   0.000034   0.019662  -0.000005  -0.000841   0.021810   0.000000
# Chi-squared of fit:     0.79 DOF:     36 RMS:  0.03
# Min/Max residuals:    -0.09    0.07
# Exact a, adot, b, bdot, g, gdot:
  1.448630E-05  1.969295E-02 -2.064178E-07 -8.439022E-04  2.154259E-02  3.066673E-04
# Covariance matrix:
  4.8791E-13 -8.5241E-13 -1.1030E-14  3.0165E-14 -2.6638E-13 -1.5538E-11
 -8.5241E-13  2.9200E-11  5.6879E-13 -1.4531E-12  1.7991E-12  7.3972E-10
 -1.1030E-14  5.6879E-13  2.3577E-13 -1.8173E-13  3.2819E-14  1.4509E-11
  3.0165E-14 -1.4531E-12 -1.8173E-13  2.2394E-13 -8.5641E-14 -3.7048E-11
 -2.6638E-13  1.7991E-12  3.2819E-14 -8.5641E-14  3.1333E-13  4.3761E-11
 -1.5538E-11  7.3972E-10  1.4509E-11 -3.7048E-11  4.3761E-11  1.8858E-08
#      lat0       lon0       xBary       yBary       zBary        JD0
    0.670758  -74.906908   -0.852488    0.005907   -0.520881  2459463.733371
# Heliocentric elements and errors
Epoch:              2459460.5000  =  2021/09/03
Mean Anomaly:           85.94691 +/-     1.070
Argument of Peri:       75.37996 +/-     0.370
Long of Asc Node:      121.20429 +/-     0.006
Inclination:             2.55036 +/-     0.001
Eccentricity:         0.03131585 +/-    0.0070
Semi-Major Axis:     47.01250597 +/-    0.0317
Time of Perihelion: 2431351.4408 +/-     348.7
Perihelion:          45.54026920 +/-    0.3287
Aphelion:            48.48474273 +/-    0.3289
Period (y)              322.3505 +/-      0.33
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           13.05378006 +/-    0.0003
Ecliptic Y          -45.10041199 +/-    0.0012
Ecliptic Z            0.54344667 +/-    0.0000
Ecliptic XDOT         0.00243169 +/-    0.0000
Ecliptic YDOT         0.00062070 +/-    0.0000
Ecliptic ZDOT        -0.00010697 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   46.95469806 +/-    0.0011
Geocenter to KBO     46.41967698 +/-    0.0012
# Hcoef:  7.65

The following table shows the complete astrometric record for 22LM14. 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 (22LM14) followed by the observatory code and reference code for the source of the astrometry.

2021 09  06.23257  19 05 11.868  -21 55 06.85  25.0r 22LM14    266  C~7umS      
2021 09  06.31280  19 05 11.705  -21 55 07.19  25.0r 22LM14    266  C~7umS      
2021 09  06.39351  19 05 11.542  -21 55 07.52  25.0r 22LM14    266  C~7umS      
2022 06  02.44372  19 16 20.060  -21 38 09.22  24.9r 22LM14    266  C~6IpZ      
2022 06  02.53086  19 16 19.745  -21 38 09.80  24.9r 22LM14    266  C~6IpZ      
2022 06  02.61096  19 16 19.455  -21 38 10.31  24.9r 22LM14    266  C~6IpZ      
2022 06  03.44086  19 16 16.506  -21 38 15.74  24.7r 22LM14    266  C~6IpZ      
2022 06  03.52767  19 16 16.188  -21 38 16.32  24.7r 22LM14    266  C~6IpZ      
2022 06  03.61505  19 16 15.867  -21 38 16.89  24.7r 22LM14    266  C~6IpZ      
2022 06  29.45230  19 14 28.971  -21 41 34.19  24.6r 22LM14    266  C~6IpZ      
2022 06  29.51532  19 14 28.682  -21 41 34.72  24.6r 22LM14    266  C~6IpZ      
2022 06  29.57836  19 14 28.392  -21 41 35.24  24.6r 22LM14    266  C~6IpZ      
2022 06  30.45132  19 14 24.449  -21 41 42.62  24.7r 22LM14    266  C~6IpZ      
2022 06  30.51752  19 14 24.144  -21 41 43.17  24.7r 22LM14    266  C~6IpZ      
2022 06  30.58249  19 14 23.845  -21 41 43.71  24.7r 22LM14    266  C~6IpZ      
2023 09  09.22891  19 14 49.212  -21 44 53.17  23.3V 22LM14    266  C~7umS      
2023 09  09.32430  19 14 49.021  -21 44 53.60  23.3V 22LM14    266  C~7umS      
2023 09  09.41985  19 14 48.831  -21 44 54.02  23.3V 22LM14    266  C~7umS      
2023 09  10.22905  19 14 47.312  -21 44 57.68  23.3V 22LM14    266  C~7umS      
2023 09  10.32490  19 14 47.127  -21 44 58.11  23.3V 22LM14    266  C~7umS      
2023 09  10.42059  19 14 46.945  -21 44 58.51  23.3V 22LM14    266  C~7umS      

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    -0.09
     2   0.0002     -2.29    -0.00      -0.08    -0.08
     3   0.0004     -4.58    -0.00      -0.16    -0.08
     4   0.7371   9368.67     0.02    -112.58     0.07
     5   0.7373   9364.23     0.01    -112.58     0.06
     6   0.7375   9360.14     0.01    -112.57     0.06
     7   0.7398   9318.58    -0.04    -112.63     0.03
     8   0.7400   9314.10    -0.03    -112.63     0.03
     9   0.7403   9309.58    -0.03    -112.61     0.03
    10   0.8110   7803.83    -0.00    -117.52     0.03
    11   0.8112   7799.76     0.01    -117.53     0.02
    12   0.8114   7795.68     0.00    -117.54     0.02
    13   0.8137   7740.15     0.02    -117.90     0.01
    14   0.8139   7735.86     0.02    -117.91     0.02
    15   0.8141   7731.65     0.03    -117.92     0.01
    16   2.0068   8058.74    -0.02    -350.85    -0.04
    17   2.0071   8056.04    -0.00    -350.94    -0.04
    18   2.0074   8053.36     0.00    -351.02    -0.04
    19   2.0096   8031.87    -0.01    -351.96    -0.01
    20   2.0098   8029.26     0.00    -352.06    -0.01
    21   2.0101   8026.69     0.01    -352.13    -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.

22LM14    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        46.501    46.649    46.382
ecceobj         0.031     0.048     0.017
incobj          2.553     2.555     2.552
qmin           44.428    43.851    44.975
qmax           49.254    50.192    48.461
amean          46.749    46.901    46.624
amin           46.379    46.519    46.259
amax           47.133    47.289    46.998
emean           0.033     0.049     0.019
emin            0.020     0.036     0.007
emax            0.045     0.062     0.031
imean           1.243     1.232     1.254
imin            0.931     0.913     0.940
imax            1.545     1.539     1.554
excite_mean     0.039     0.054     0.029
fracstop        1.000     1.000     1.000
cjmean          3.134     3.134     3.133

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       205.9     209.1     199.4
kozaiamp        179.9     180.0     180.0