Orbit Fit and Astrometric record for 15FO477

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: 15FO477   
# Created Tue Apr  1 01:10:22 2025
# Orbit generated from Bernstein formalism
# Fitting     20 observations of     20
# Arc:   4.19y
# First observation: 2015/01/25
#  Last observation: 2019/04/05
Preliminary a, adot, b, bdot, g, gdot:
  -0.000068   0.028910  -0.000012   0.004008   0.026643   0.000000
# Chi-squared of fit:    12.22 DOF:     34 RMS:  0.14
# Min/Max residuals:    -0.37    0.24
# Exact a, adot, b, bdot, g, gdot:
  1.749544E-05  2.831822E-02  3.701568E-06  3.914923E-03  2.639479E-02 -2.329845E-03
# Covariance matrix:
  4.5429E-13  1.0011E-13 -7.7238E-15  2.4100E-14  3.7843E-13  1.4366E-12
  1.0011E-13  8.5207E-13 -2.8735E-14  1.4321E-13  4.1713E-13  8.3217E-12
 -7.7238E-15 -2.8735E-14  1.9260E-13 -5.3542E-14 -1.7732E-14 -2.8670E-13
  2.4100E-14  1.4321E-13 -5.3542E-14  4.4248E-14  6.9847E-14  1.4319E-12
  3.7843E-13  4.1713E-13 -1.7732E-14  6.9847E-14  6.0012E-13  4.1054E-12
  1.4366E-12  8.3217E-12 -2.8670E-13  1.4319E-12  4.1054E-12  8.3199E-11
#      lat0       lon0       xBary       yBary       zBary        JD0
    2.198463  176.757964    0.772122    0.023444   -0.606703  2457048.072631
# Heliocentric elements and errors
Epoch:              2457040.5000  =  2015/01/18
Mean Anomaly:          333.30670 +/-     0.061
Argument of Peri:       53.84016 +/-     0.096
Long of Asc Node:      160.40888 +/-     0.001
Inclination:             8.19905 +/-     0.000
Eccentricity:         0.18435778 +/-    0.0002
Semi-Major Axis:     45.60985104 +/-    0.0063
Time of Perihelion: 2465382.8080 +/-      18.9
Perihelion:          37.20132014 +/-    0.0111
Aphelion:            54.01838194 +/-    0.0123
Period (y)              308.0322 +/-      0.06
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -38.36326794 +/-    0.0011
Ecliptic Y            2.94632850 +/-    0.0001
Ecliptic Z            1.45348193 +/-    0.0000
Ecliptic XDOT         0.00008672 +/-    0.0000
Ecliptic YDOT        -0.00295260 +/-    0.0000
Ecliptic ZDOT         0.00039661 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   38.50368539 +/-    0.0011
Geocenter to KBO     37.88625958 +/-    0.0011
# Hcoef:  7.90

The following table shows the complete astrometric record for 15FO477. 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 (15FO477) followed by the observatory code and reference code for the source of the astrometry.

2015 01  25.571853 11 51 35.90   +03 18 22.9         15FO477   T09  C~8AgS      
2015 01  25.629150 11 51 35.75   +03 18 24.2         15FO477   T09  C~8AgS      
2015 03  23.16519  11 47 46.39   +03 46 56.7   23.0R 15FO477   695  C~8AgS      
2015 03  23.22929  11 47 46.07   +03 46 58.8         15FO477   695  C~8AgS      
2015 03  23.28872  11 47 45.79   +03 47 00.7         15FO477   695  C~8AgS      
2015 04  15.20534  11 46 03.00   +03 58 35.9   23.2R 15FO477   695  C~8AgS      
2015 04  15.28229  11 46 02.68   +03 58 38.0         15FO477   695  C~8AgS      
2015 04  15.35550  11 46 02.38   +03 58 39.9         15FO477   695  C~8AgS      
2018 02  11.643203 12 09 55.84   +02 04 44.7         15FO477   T09  C~8AgS      
2018 04  22.367255 12 04 48.45   +02 41 17.3         15FO477   T09  C~8AgS      
2019 02  05.537827 12 16 42.81   +01 34 32.1         15FO477   T09  C~8AgS      
2019 03  03.568727 12 15 06.97   +01 47 19.7         15FO477   T09  C~8AgS      
2019 03  03.608930 12 15 06.79   +01 47 21.1         15FO477   T09  C~8AgS      
2019 04  04.45934  12 12 37.09   +02 05 06.0   24.2g 15FO477   T09  C~8AgS      
2019 04  04.48250  12 12 36.98   +02 05 06.6   24.0g 15FO477   T09  C~8AgS      
2019 04  04.50140  12 12 36.89   +02 05 07.3   24.2g 15FO477   T09  C~8AgS      
2019 04  04.51398  12 12 36.82   +02 05 07.6   24.3g 15FO477   T09  C~8AgS      
2019 04  05.52240  12 12 32.09   +02 05 39.7   23.5r 15FO477   T09  C~8AgS      
2019 04  05.54544  12 12 31.98   +02 05 40.6   23.9r 15FO477   T09  C~8AgS      
2019 04  05.57686  12 12 31.84   +02 05 40.9   23.6r 15FO477   T09  C~8AgS      

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    -0.11       0.00    -0.28
     2   0.0002     -2.58    -0.18       0.30    -0.24
     3   0.1549  -3834.57     0.20     207.45     0.20
     4   0.1551  -3839.81     0.06     207.47     0.12
     5   0.1553  -3844.41     0.18     207.56     0.11
     6   0.2180  -5533.17    -0.07     235.63     0.06
     7   0.2182  -5538.40    -0.09     235.66     0.08
     8   0.2184  -5543.28    -0.03     235.63     0.04
     9   3.0474  16911.50     0.13    2542.38    -0.20
    10   3.2383  11786.78     0.02    2702.21    -0.11
    11   4.0300  23288.80     0.07    3341.68    -0.03
    12   4.1013  21645.08     0.02    3466.10     0.04
    13   4.1014  21642.01    -0.02    3466.30     0.11
    14   4.1886  19134.45    -0.06    3537.81     0.13
    15   4.1887  19132.69     0.01    3537.69     0.01
    16   4.1887  19131.16    -0.02    3537.79     0.10
    17   4.1888  19130.06    -0.12    3537.64    -0.05
    18   4.1915  19051.56    -0.09    3538.50     0.05
    19   4.1916  19049.67    -0.16    3538.66     0.21
    20   4.1917  19047.61     0.24    3538.08    -0.37

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.

15FO477    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        45.160    45.176    45.145
ecceobj         0.177     0.177     0.177
incobj          8.231     8.231     8.231
qmin           36.660    36.665    36.663
qmax           54.536    54.488    54.392
amean          45.382    45.399    45.365
amin           44.990    45.003    44.969
amax           45.838    45.863    45.818
emean           0.173     0.173     0.172
emin            0.156     0.157     0.156
emax            0.190     0.189     0.189
imean           7.625     7.615     7.632
imin            6.700     6.679     6.716
imax            8.555     8.547     8.560
excite_mean     0.218     0.218     0.218
fracstop        1.000     1.000     1.000
cjmean          3.060     3.061     3.060

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       181.4     180.3     181.6
kozaiamp        180.0     180.0     180.0