Orbit Fit and Astrometric record for 14YD100

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: 14YD100   
# Created Sun Dec 22 02:10:15 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     22 observations of     22
# Arc:  10.00y
# First observation: 2014/11/24
#  Last observation: 2024/11/24
# Chi-squared of fit:    12.45 DOF:     38 RMS:  0.13
# Min/Max residuals:    -0.25    0.25
# Exact a, adot, b, bdot, g, gdot:
  2.029291E-05  4.523118E-02 -5.894267E-06 -1.417581E-02  3.600423E-02 -5.441818E-03
# Covariance matrix:
  2.2571E-13 -1.7291E-13 -6.2597E-14  4.7079E-14  2.1261E-13 -2.9131E-13
 -1.7291E-13  2.1458E-13  8.5101E-14 -6.2666E-14 -3.0519E-13  3.8676E-13
 -6.2597E-14  8.5101E-14  1.4362E-13 -4.2942E-14 -1.3806E-13  1.5717E-13
  4.7079E-14 -6.2666E-14 -4.2942E-14  2.5851E-14  9.0459E-14 -1.1688E-13
  2.1261E-13 -3.0519E-13 -1.3806E-13  9.0459E-14  6.3032E-13 -5.4976E-13
 -2.9131E-13  3.8676E-13  1.5717E-13 -1.1688E-13 -5.4976E-13  7.2226E-13
#      lat0       lon0       xBary       yBary       zBary        JD0
  -19.516501   51.392805   -0.175134   -0.324609   -0.916310  2456985.856878
# Heliocentric elements and errors
Epoch:              2456986.5000  =  2014/11/25
Mean Anomaly:          344.82867 +/-     0.007
Argument of Peri:      257.91517 +/-     0.011
Long of Asc Node:      185.56049 +/-     0.000
Inclination:            25.33488 +/-     0.000
Eccentricity:         0.29795557 +/-    0.0001
Semi-Major Axis:     39.70742288 +/-    0.0064
Time of Perihelion: 2460837.9754 +/-      21.3
Perihelion:          27.87637489 +/-    0.0057
Aphelion:            51.53847087 +/-    0.0090
Period (y)              250.2164 +/-      0.06
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           16.80150505 +/-    0.0004
Ecliptic Y           21.32745159 +/-    0.0004
Ecliptic Z           -9.27904474 +/-    0.0002
Ecliptic XDOT        -0.00316007 +/-    0.0000
Ecliptic YDOT         0.00155495 +/-    0.0000
Ecliptic ZDOT        -0.00087768 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   28.69242405 +/-    0.0004
Geocenter to KBO     27.77461998 +/-    0.0006
# Hcoef:  7.73

The following table shows the complete astrometric record for 14YD100. 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 (14YD100) followed by the observatory code and reference code for the source of the astrometry.

2014 11  24.3561   03 35 53.27   -00 46 30.9   22.7w 14YD100   F51  C~77rr      
2014 11  24.37113  03 35 53.16   -00 46 31.3   22.7w 14YD100   F51  C~77rr      
2014 11  24.38627  03 35 53.08   -00 46 31.5   22.4w 14YD100   F51  C~77rr      
2014 12  18.35636  03 33 26.54   -00 52 18.2   22.6w 14YD100   F51  C~77rr      
2014 12  18.36926  03 33 26.49   -00 52 18.1   22.5w 14YD100   F51  C~77rr      
2014 12  18.38216  03 33 26.40   -00 52 18.4   22.5w 14YD100   F51  C~77rr      
2014 12  18.39513  03 33 26.35   -00 52 18.1   22.7w 14YD100   F51  C~77rr      
2015 01  19.2779   03 31 23.97   -00 46 35.3   22.6w 14YD100   F51  C~77rr      
2015 01  19.29057  03 31 23.95   -00 46 34.9   22.8w 14YD100   F51  C~77rr      
2015 01  19.30309  03 31 23.93   -00 46 34.6   22.4w 14YD100   F51  C~77rr      
2017 09  19.59747  04 14 05.39   -00 24 26.9   22.7w 14YD100   F51  C~77rr      
2017 09  19.61449  04 14 05.36   -00 24 27.9   22.7w 14YD100   F51  C~77rr      
2017 09  19.623    04 14 05.36   -00 24 28.0   22.2w 14YD100   F51  C~77rr      
2017 10  01.60449  04 13 40.02   -00 34 59.0   22.4w 14YD100   F51  C~77rr      
2017 10  01.6117   04 13 40.01   -00 34 59.5   22.4w 14YD100   F51  C~77rr      
2017 10  01.61895  04 13 39.98   -00 34 59.6   22.4w 14YD100   F51  C~77rr      
2017 10  01.62616  04 13 39.94   -00 35 00.1   22.4w 14YD100   F51  C~77rr      
2017 10  30.51344  04 11 31.26   -00 58 32.5   22.6w 14YD100   F51  C~77rr      
2017 10  30.53866  04 11 31.13   -00 58 33.7   22.4w 14YD100   F51  C~77rr      
2017 10  30.55128  04 11 31.06   -00 58 34.4   22.5w 14YD100   F51  C~77rr      
2024 11  24.430430 05 28 23.063  -02 10 47.01  22.3G 14YD100   G37  C~8STS      
2024 11  24.479900 05 28 22.749  -02 10 48.45        14YD100   G37  C~8STS      

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    -0.07       0.00    -0.09
     2   0.0000      0.00    -0.21       0.00    -0.11
     3   0.0001      0.00     0.10       0.00     0.06
     4   0.0657      0.00    -0.14       0.00    -0.05
     5   0.0657      0.00     0.19       0.00     0.10
     6   0.0658      0.00    -0.09       0.00    -0.16
     7   0.0658      0.00     0.24       0.00     0.19
     8   0.1531      0.00    -0.11       0.00    -0.13
     9   0.1531      0.00    -0.01       0.00    -0.03
    10   0.1532      0.00     0.08       0.00    -0.04
    11   2.8206      0.00    -0.02       0.00    -0.15
    12   2.8207      0.00    -0.10       0.00    -0.25
    13   2.8207      0.00     0.09       0.00     0.09
    14   2.8535      0.00     0.03       0.00     0.07
    15   2.8535      0.00     0.21       0.00    -0.06
    16   2.8536      0.00     0.08       0.00     0.23
    17   2.8536      0.00    -0.19       0.00     0.10
    18   2.9327      0.00    -0.21       0.00     0.25
    19   2.9327      0.00     0.07       0.00     0.14
    20   2.9328      0.00     0.14       0.00    -0.02
    21  10.0016      0.00    -0.08       0.00     0.00
    22  10.0017      0.00     0.06       0.00    -0.12

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.

14YD100    quality flag:3

Type:           3:2E      3:2E      3:2E

axisobj        39.963    39.962    39.963
ecceobj         0.300     0.300     0.300
incobj         25.257    25.257    25.257
qmin           27.130    27.119    27.169
qmax           52.320    52.577    52.329
amean          39.454    39.454    39.454
amin           38.975    38.971    38.995
amax           40.056    40.030    39.994
emean           0.261     0.262     0.261
emin            0.192     0.192     0.193
emax            0.309     0.313     0.309
imean          25.974    25.958    25.988
imin           24.518    24.499    24.556
imax           27.841    27.847    27.837
excite_mean     0.511     0.511     0.511
fracstop        1.000     1.000     1.000
cjmean          2.748     2.749     2.748

libcent 0       179.0     179.7     179.8
libamp  0       100.9      98.8     101.3
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       273.3     273.6     273.3
kozaiamp         46.9      47.7      46.6