Orbit Fit and Astrometric record for 15FQ493

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: 15FQ493   
# Created Sun Feb 23 02:10:20 2025
# Orbit generated from Bernstein formalism
# Fitting     21 observations of     21
# Arc:  65.88d
# First observation: 2015/03/18
#  Last observation: 2015/05/23
Preliminary a, adot, b, bdot, g, gdot:
  -0.000000   0.041150  -0.000002  -0.013989   0.030396   0.000000
# WARNING Fitting with energy constraint
# Chi-squared of fit:    11.97 DOF:     37 RMS:  0.13
# Min/Max residuals:    -0.25    0.28
# Exact a, adot, b, bdot, g, gdot:
  1.719616E-05  3.201097E-02 -7.595849E-06 -1.414868E-02  2.894454E-02 -4.307410E-03
# Covariance matrix:
  4.0701E-13  3.8678E-10 -8.4557E-14  7.3442E-12  6.0555E-11 -3.8879E-09
  3.8678E-10  8.8470E-07 -2.2221E-10  1.9203E-08  1.3423E-07 -9.7990E-06
 -8.4557E-14 -2.2221E-10  1.5648E-13 -5.7015E-12 -3.3553E-11  2.4989E-09
  7.3442E-12  1.9203E-08 -5.7015E-12  4.4585E-10  2.9000E-09 -2.1583E-07
  6.0555E-11  1.3423E-07 -3.3553E-11  2.9000E-09  2.0389E-08 -1.4816E-06
 -3.8879E-09 -9.7990E-06  2.4989E-09 -2.1583E-07 -1.4816E-06  1.0973E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.559314  178.817422    0.025331   -0.009554   -0.991785  2457099.980898
# Heliocentric elements and errors
Epoch:              2457090.5000  =  2015/03/09
Mean Anomaly:          347.93845 +/-    21.925
Argument of Peri:      208.16448 +/-    53.289
Long of Asc Node:      357.54381 +/-     0.038
Inclination:            23.80901 +/-     0.650
Eccentricity:         0.35895951 +/-    0.2181
Semi-Major Axis:     53.87187625 +/-   11.2292
Time of Perihelion: 2461929.3504 +/-    8664.8
Perihelion:          34.53405385 +/-   13.7795
Aphelion:            73.20969864 +/-   19.2595
Period (y)              395.4134 +/-    123.63
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -35.53405842 +/-    0.1704
Ecliptic Y            0.75863526 +/-    0.0035
Ecliptic Z           -0.33750170 +/-    0.0017
Ecliptic XDOT         0.00035448 +/-    0.0010
Ecliptic YDOT        -0.00304171 +/-    0.0001
Ecliptic ZDOT        -0.00133419 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   35.54375814 +/-    0.1703
Geocenter to KBO     34.54883190 +/-    0.1704
# Hcoef:  9.08

The following table shows the complete astrometric record for 15FQ493. 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 (15FQ493) followed by the observatory code and reference code for the source of the astrometry.

2015 03  18.48012  11 54 46.21   -00 02 34.1   24.7r 15FQ493   T09  C~8eRn      
2015 03  18.51214  11 54 46.04   -00 02 33.4   24.6r 15FQ493   T09  C~8eRn      
2015 03  18.54052  11 54 45.87   -00 02 32.7   24.6r 15FQ493   T09  C~8eRn      
2015 03  18.56877  11 54 45.72   -00 02 31.4   24.6r 15FQ493   T09  C~8eRn      
2015 03  20.46619  11 54 35.45   -00 01 41.5   24.4i 15FQ493   T09  C~8eRn      
2015 03  20.54104  11 54 35.03   -00 01 39.6   24.3i 15FQ493   T09  C~8eRn      
2015 03  22.47957  11 54 24.55   -00 00 48.2   24.1i 15FQ493   T09  C~8eRn      
2015 03  22.48791  11 54 24.51   -00 00 47.9   24.1i 15FQ493   T09  C~8eRn      
2015 03  22.51564  11 54 24.36   -00 00 47.1   24.2i 15FQ493   T09  C~8eRn      
2015 03  25.45755  11 54 08.47   +00 00 30.4   25.4g 15FQ493   T09  C~8eRn      
2015 03  25.48926  11 54 08.30   +00 00 31.3   24.9g 15FQ493   T09  C~8eRn      
2015 03  25.51747  11 54 08.14   +00 00 32.3   25.1g 15FQ493   T09  C~8eRn      
2015 03  25.54970  11 54 07.97   +00 00 33.0   24.9g 15FQ493   T09  C~8eRn      
2015 03  29.38231  11 53 47.47   +00 02 13.4   24.2y 15FQ493   T09  C~8eRn      
2015 03  29.38505  11 53 47.47   +00 02 13.7   23.9y 15FQ493   T09  C~8eRn      
2015 03  29.38774  11 53 47.46   +00 02 13.7   24.0y 15FQ493   T09  C~8eRn      
2015 03  29.39311  11 53 47.44   +00 02 13.9   24.6y 15FQ493   T09  C~8eRn      
2015 03  29.42099  11 53 47.26   +00 02 14.6   23.9y 15FQ493   T09  C~8eRn      
2015 05  23.28008  11 50 11.76   +00 18 18.6   24.1z 15FQ493   T09  C~8eRn      
2015 05  23.33557  11 50 11.67   +00 18 19.0   24.2z 15FQ493   T09  C~8eRn      
2015 05  23.36165  11 50 11.61   +00 18 19.1   24.6z 15FQ493   T09  C~8eRn      

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     0.06       0.00    -0.03
     2   0.0001     -2.62     0.21      -0.37    -0.12
     3   0.0002     -5.24     0.04      -0.74    -0.25
     4   0.0002     -7.82    -0.11      -0.45     0.28
     5   0.0054   -169.01    -0.02     -15.93    -0.03
     6   0.0056   -175.54    -0.09     -16.69    -0.15
     7   0.0109   -340.22     0.00     -32.05    -0.05
     8   0.0110   -340.89     0.05     -32.01     0.06
     9   0.0110   -343.27     0.06     -32.17     0.13
    10   0.0191   -592.78    -0.08     -55.85    -0.22
    11   0.0192   -595.48    -0.05     -56.04    -0.14
    12   0.0193   -598.08    -0.24     -56.08     0.07
    13   0.0194   -600.70    -0.09     -56.45    -0.04
    14   0.0298   -922.77    -0.05     -86.62    -0.11
    15   0.0299   -922.89     0.06     -86.35     0.19
    16   0.0299   -923.03     0.15     -86.41     0.15
    17   0.0299   -923.38     0.25     -86.34     0.26
    18   0.0300   -926.14    -0.14     -86.77     0.06
    19   0.1802  -4276.00    -0.07    -487.83    -0.15
    20   0.1803  -4277.39     0.10    -488.00     0.08
    21   0.1804  -4278.26    -0.03    -488.27     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.

15FQ493    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