Orbit Fit and Astrometric record for 15FO400

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: 15FO400   
# Created Sun Dec 22 02:10:18 2024
# Orbit generated from Bernstein formalism
# Fitting     21 observations of     21
# Arc:   1.22y
# First observation: 2015/03/18
#  Last observation: 2016/06/04
Preliminary a, adot, b, bdot, g, gdot:
   0.000002   0.025190   0.000000   0.000868   0.024978   0.000000
# Chi-squared of fit:     7.50 DOF:     36 RMS:  0.11
# Min/Max residuals:    -0.33    0.27
# Exact a, adot, b, bdot, g, gdot:
  1.587243E-05  2.512912E-02  4.810451E-07  8.684902E-04  2.483574E-02 -1.420322E-03
# Covariance matrix:
  5.0856E-13  1.7723E-11 -4.3399E-15  6.5065E-13  1.7337E-11  6.9970E-10
  1.7723E-11  1.2214E-09 -3.0007E-13  4.4244E-11  1.1813E-09  4.7552E-08
 -4.3399E-15 -3.0007E-13  2.4316E-13 -2.3265E-13 -2.9122E-13 -1.1650E-11
  6.5065E-13  4.4244E-11 -2.3265E-13  1.8879E-12  4.2798E-11  1.7232E-09
  1.7337E-11  1.1813E-09 -2.9122E-13  4.2798E-11  1.1432E-09  4.5992E-08
  6.9970E-10  4.7552E-08 -1.1650E-11  1.7232E-09  4.5992E-08  1.8523E-06
#      lat0       lon0       xBary       yBary       zBary        JD0
    2.000430 -178.204241    0.076575    0.034656   -0.988591  2457099.995551
# Heliocentric elements and errors
Epoch:              2457090.5000  =  2015/03/09
Mean Anomaly:          327.49270 +/-    20.424
Argument of Peri:       83.78851 +/-    26.279
Long of Asc Node:      137.04814 +/-     0.042
Inclination:             2.77742 +/-     0.002
Eccentricity:         0.09709917 +/-    0.0376
Semi-Major Axis:     44.78682369 +/-    0.4377
Time of Perihelion: 2466976.0801 +/-    6209.4
Perihelion:          40.43806017 +/-    1.7312
Aphelion:            49.13558720 +/-    1.7526
Period (y)              299.7323 +/-      4.39
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -41.21447376 +/-    0.0548
Ecliptic Y           -1.21565784 +/-    0.0017
Ecliptic Z            1.40555207 +/-    0.0019
Ecliptic XDOT         0.00024313 +/-    0.0002
Ecliptic YDOT        -0.00276959 +/-    0.0000
Ecliptic ZDOT         0.00009031 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   41.25634797 +/-    0.0547
Geocenter to KBO     40.26455949 +/-    0.0548
# Hcoef:  8.77

The following table shows the complete astrometric record for 15FO400. 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 (15FO400) followed by the observatory code and reference code for the source of the astrometry.

2015 03  18.494773 12 09 46.338  +01 07 16.67  24.7r 15FO400   568  C~2TuJ      
2015 03  18.522848 12 09 46.208  +01 07 17.48  24.8r 15FO400   568  C~2TuJ      
2015 03  18.579625 12 09 45.947  +01 07 19.25  24.6r 15FO400   568  C~2TuJ      
2015 03  20.444244 12 09 37.542  +01 08 15.37  24.1i 15FO400   568  C~2TuJ      
2015 03  20.483035 12 09 37.361  +01 08 16.55  24.3i 15FO400   568  C~2TuJ      
2015 03  20.521711 12 09 37.185  +01 08 17.72  24.2i 15FO400   568  C~2TuJ      
2016 04  02.39692  12 13 58.75   +00 43 17.0   24.5i 15FO400   T09  C~8H7Z      
2016 04  02.43920  12 13 58.55   +00 43 18.2   24.6i 15FO400   T09  C~8H7Z      
2016 04  02.49902  12 13 58.29   +00 43 20.0   24.4i 15FO400   T09  C~8H7Z      
2016 04  02.52059  12 13 58.19   +00 43 20.3   24.4i 15FO400   T09  C~8H7Z      
2016 04  04.35168  12 13 50.05   +00 44 13.3   25.6g 15FO400   T09  C~8H7Z      
2016 04  04.36588  12 13 50.00   +00 44 13.8   26.5g 15FO400   T09  C~8H7Z      
2016 04  04.39376  12 13 49.87   +00 44 14.4   26.4g 15FO400   T09  C~8H7Z      
2016 04  04.41084  12 13 49.80   +00 44 14.9   26.1g 15FO400   T09  C~8H7Z      
2016 04  08.50734  12 13 31.81   +00 46 10.7   24.9r 15FO400   T09  C~8H7Z      
2016 04  08.51367  12 13 31.79   +00 46 10.7   24.7r 15FO400   T09  C~8H7Z      
2016 04  08.52637  12 13 31.72   +00 46 11.0   25.2r 15FO400   T09  C~8H7Z      
2016 06  04.25886  12 10 47.49   +01 02 22.4   24.2z 15FO400   T09  C~8H7Z      
2016 06  04.29197  12 10 47.44   +01 02 22.4   24.5z 15FO400   T09  C~8H7Z      
2016 06  04.30815  12 10 47.40   +01 02 22.6   24.4z 15FO400   T09  C~8H7Z      
2016 06  04.32438  12 10 47.40   +01 02 22.4   24.2z 15FO400   T09  C~8H7Z      

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     0.01
     2   0.0001     -2.11     0.02      -0.03    -0.03
     3   0.0002     -6.41    -0.02       0.04     0.02
     4   0.0053   -144.38     0.01       1.40    -0.01
     5   0.0054   -147.34    -0.03       1.41    -0.01
     6   0.0055   -150.23    -0.01       1.43     0.00
     7   1.0429   4046.48    -0.05     185.13     0.06
     8   1.0430   4043.25    -0.14     185.03    -0.01
     9   1.0431   4038.95    -0.01     185.13     0.13
    10   1.0432   4037.46     0.09     184.81    -0.18
    11   1.0482   3904.31    -0.16     184.85    -0.00
    12   1.0482   3903.42    -0.00     185.01     0.17
    13   1.0483   3901.39     0.02     184.78    -0.04
    14   1.0484   3900.23     0.11     184.83     0.02
    15   1.0596   3606.51    -0.01     183.69     0.09
    16   1.0596   3606.23     0.17     183.57    -0.02
    17   1.0596   3605.15    -0.01     183.43    -0.16
    18   1.2150    958.51     0.27      94.74     0.18
    19   1.2151    957.82     0.06      94.44    -0.02
    20   1.2151    957.19    -0.33      94.38    -0.03
    21   1.2151    957.27    -0.02      94.20    -0.17

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.

15FO400    quality flag:1

Type:        9:5EEEE  SCATNEAR CLASSICAL

axisobj        44.352    46.346    44.166
ecceobj         0.090     0.222     0.069
incobj          2.784     2.779     2.786
qmin           39.854    35.648    40.443
qmax           49.499    58.054    48.489
amean          44.554    46.551    44.372
amin           44.191    46.091    44.028
amax           44.945    47.086    44.742
emean           0.092     0.214     0.070
emin            0.082     0.197     0.054
emax            0.101     0.233     0.084
imean           2.069     2.569     1.996
imin            1.508     1.479     1.324
imax            2.733     3.602     2.684
excite_mean     0.099     0.219     0.078
fracstop        1.000     1.000     1.000
cjmean          3.096     3.073     3.099

libcent 0       182.4    -180.0    -180.0
libamp  0       108.8    -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       177.1     183.0     188.4
kozaiamp        179.9     180.0     180.0