Orbit Fit and Astrometric record for 95YY3

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: 95YY3     
# Created Wed Nov 27 02:07:52 2024
# Orbit generated from Bernstein formalism
# Fitting     21 observations of     21
# Arc:   0.72y
# First observation: 1995/12/24
#  Last observation: 1996/09/13
Preliminary a, adot, b, bdot, g, gdot:
  -0.000003   0.041072  -0.000002   0.000252   0.033016   0.000000
# Chi-squared of fit:   481.74 DOF:     36 RMS:  0.85
# Min/Max residuals:    -2.40    1.60
# Exact a, adot, b, bdot, g, gdot:
  2.000425E-05  4.043776E-02 -1.226373E-06  2.496433E-04  3.310478E-02 -3.036594E-02
# Covariance matrix:
  3.0932E-13  5.7982E-11 -2.2690E-14  2.6924E-13  1.5950E-11  1.1567E-09
  5.7982E-11  3.1831E-08 -1.2091E-11  1.4584E-10  8.4101E-09  6.2427E-07
 -2.2690E-14 -1.2091E-11  9.6575E-14 -2.4690E-13 -3.1978E-12 -2.3723E-10
  2.6924E-13  1.4584E-10 -2.4690E-13  2.3817E-12  3.8549E-11  2.8608E-09
  1.5950E-11  8.4101E-09 -3.1978E-12  3.8549E-11  2.2252E-09  1.6503E-07
  1.1567E-09  6.2427E-07 -2.3723E-10  2.8608E-09  1.6503E-07  1.2246E-05
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.269161   62.378113   -0.494005   -0.004114   -0.859255  2450075.832758
# Heliocentric elements and errors
Epoch:              2450070.5000  =  1995/12/19
Mean Anomaly:          357.21887 +/-     3.674
Argument of Peri:       40.94121 +/-     1.661
Long of Asc Node:       99.53829 +/-     0.146
Inclination:             0.44261 +/-     0.002
Eccentricity:         0.89216696 +/-    0.1007
Semi-Major Axis:    182.34149616 +/-  160.4915
Time of Perihelion: 2457018.2714 +/-     302.9
Perihelion:          19.66243723 +/-   25.2320
Aphelion:           345.02055510 +/-  304.2313
Period (y)             2462.2745 +/-   3250.83
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           13.96861082 +/-    0.0200
Ecliptic Y           27.74724370 +/-    0.0381
Ecliptic Z           -0.14193609 +/-    0.0002
Ecliptic XDOT        -0.00412002 +/-    0.0001
Ecliptic YDOT        -0.00067273 +/-    0.0003
Ecliptic ZDOT         0.00003225 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   31.06528234 +/-    0.0352
Geocenter to KBO     30.20711659 +/-    0.0430
# Hcoef:  8.50

The following table shows the complete astrometric record for 95YY3. 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 (95YY3) followed by the observatory code and reference code for the source of the astrometry.

1995 12  24.33205  04 01 26.13   +20 22 22.1   23.0R 95YY3     568  C26263      
1995 12  24.35745  04 01 25.97   +20 22 21.7   23.0R 95YY3     568  C26263      
1995 12  24.37531  04 01 25.87   +20 22 21.5   23.0R 95YY3     568  C26263      
1995 12  25.29590  04 01 20.75   +20 22 06.4   23.0R 95YY3     568  C26263      
1995 12  25.31176  04 01 20.67   +20 22 06.4   23.0R 95YY3     568  C26263      
1995 12  25.32571  04 01 20.57   +20 22 06.1   23.0R 95YY3     568  C26263      
1995 12  27.45651  04 01 08.97   +20 21 32.5   23.0R 95YY3     568  C26263      
1995 12  27.47286  04 01 08.87   +20 21 32.0   23.0R 95YY3     568  C26263      
1996 01  20.21134  03 59 28.40   +20 17 02.6         95YY3     711  C27070      
1996 01  21.13715  03 59 25.82   +20 16 54.7         95YY3     711  C27070      
1996 01  21.19957  03 59 25.73   +20 16 54.0         95YY3     711  C27070      
1996 01  21.20087  03 59 25.69   +20 16 55.4         95YY3     675  C26660      
1996 01  21.27806  03 59 25.50   +20 16 53.0         95YY3     711  C27070      
1996 01  22.16962  03 59 23.08   +20 16 46.4         95YY3     711  C27070      
1996 01  22.23699  03 59 22.78   +20 16 46.7         95YY3     711  C27070      
1996 01  22.30343  03 59 22.62   +20 16 46.4         95YY3     711  C27070      
1996 01  24.12365  03 59 18.04   +20 16 34.7         95YY3     675  C26660      
1996 01  24.21181  03 59 17.87   +20 16 34.2         95YY3     675  C26660      
1996 01  24.32038  03 59 17.57   +20 16 33.7         95YY3     675  C26660      
1996 09  12.5785   04 20 00.73   +21 11 41.5   24. R 95YY3     568  C27786      
1996 09  13.5135   04 20 00.15   +21 11 40.1         95YY3     568  C27786      

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    -0.14       0.00     0.28
     2   0.0001     -2.28    -0.33       0.05     0.31
     3   0.0001     -3.70    -0.28       0.13     0.38
     4   0.0026    -77.26    -0.12      -0.50    -0.62
     5   0.0027    -78.37     0.06      -0.28    -0.41
     6   0.0027    -79.80    -0.24      -0.30    -0.44
     7   0.0086   -246.35     0.62      -1.10    -2.19
     8   0.0086   -247.83     0.42      -1.32    -2.40
     9   0.0736  -1686.47    -0.64      15.03     1.43
    10   0.0761  -1723.62    -0.22      14.54     0.39
    11   0.0763  -1725.00     0.98      14.10    -0.09
    12   0.0763  -1725.27     0.71      15.59     1.41
    13   0.0765  -1728.37     0.82      13.77    -0.46
    14   0.0790  -1763.06     0.59      14.10    -0.67
    15   0.0791  -1767.13    -0.84      15.24     0.42
    16   0.0793  -1769.40    -0.53      15.40     0.55
    17   0.0843  -1834.88    -0.63      16.81     0.87
    18   0.0845  -1837.33     0.08      16.80     0.79
    19   0.0848  -1841.56    -0.32      17.15     1.09
    20   0.7207  15939.51     1.60      53.87    -0.45
    21   0.7233  15931.23    -1.59      53.86    -0.11

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.

95YY3    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