Orbit Fit and Astrometric record for 14RR86

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: 14RR86    
# Created Fri Apr 26 01:16:10 2024
# Orbit generated from Bernstein formalism
# Fitting      8 observations of      8
# Arc:   3.13y
# First observation: 2014/09/04
#  Last observation: 2017/10/22
Preliminary a, adot, b, bdot, g, gdot:
   0.000026   0.023787  -0.000006   0.008069   0.025602   0.000000
# Chi-squared of fit:     3.05 DOF:     10 RMS:  0.11
# Min/Max residuals:    -0.22    0.19
# Exact a, adot, b, bdot, g, gdot:
  1.449035E-05  2.406471E-02  4.713309E-06  8.171835E-03  2.584728E-02  1.480805E-03
# Covariance matrix:
  7.3560E-13 -2.0820E-13 -2.3135E-13 -6.8032E-14  1.3558E-12 -2.1058E-12
 -2.0820E-13  2.8688E-12 -2.7301E-13  1.2934E-12  8.2409E-13  4.3820E-11
 -2.3135E-13 -2.7301E-13  4.7404E-13 -2.2854E-13 -8.6964E-13 -3.9780E-12
 -6.8032E-14  1.2934E-12 -2.2854E-13  7.1333E-13  3.0675E-13  2.0553E-11
  1.3558E-12  8.2409E-13 -8.6964E-13  3.0675E-13  4.7786E-12  1.1044E-11
 -2.1058E-12  4.3820E-11 -3.9780E-12  2.0553E-11  1.1044E-11  6.9601E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
  -31.095484  -46.222291   -0.466613   -0.463243   -0.768308  2456904.593728
# Heliocentric elements and errors
Epoch:              2456900.5000  =  2014/08/31
Mean Anomaly:          111.22210 +/-     0.446
Argument of Peri:      179.66913 +/-     0.416
Long of Asc Node:       10.08215 +/-     0.001
Inclination:            35.46479 +/-     0.000
Eccentricity:         0.08097357 +/-    0.0008
Semi-Major Axis:     38.13431802 +/-    0.0138
Time of Perihelion: 2430326.2507 +/-     105.6
Perihelion:          35.04644597 +/-    0.0347
Aphelion:            41.22219007 +/-    0.0356
Period (y)              235.4953 +/-      0.13
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           23.87682791 +/-    0.0019
Ecliptic Y          -24.24367224 +/-    0.0020
Ecliptic Z          -19.98128304 +/-    0.0017
Ecliptic XDOT         0.00223791 +/-    0.0000
Ecliptic YDOT         0.00133940 +/-    0.0000
Ecliptic ZDOT         0.00066032 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   39.46023601 +/-    0.0019
Geocenter to KBO     38.68878756 +/-    0.0033
# Hcoef:  7.85

The following table shows the complete astrometric record for 14RR86. 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 (14RR86) followed by the observatory code and reference code for the source of the astrometry.

2014 09  04.09295  21 54 20.775  -46 02 12.41  23.9i 14RR86    W84  C~52Tx      
2014 09  26.08772  21 52 02.935  -45 58 53.86  23.5r 14RR86    W84  C~52Tx      
2014 09  26.08909  21 52 02.914  -45 58 53.87  24.0i 14RR86    W84  C~52Tx      
2014 10  23.15410  21 50 13.536  -45 44 33.61  24.1r 14RR86    W84  C~52Tx      
2014 10  26.06808  21 50 07.025  -45 42 25.37  23.2i 14RR86    W84  C~52Tx      
2016 09  24.09468  22 04 09.352  -44 01 40.16  24.0r 14RR86    W84  C~52Tx      
2017 09  23.13340  22 09 56.219  -43 01 33.99  23.4i 14RR86    W84  C~52Tx      
2017 10  22.02665  22 07 46.799  -42 49 57.26  23.8r 14RR86    W84  C~52Tx      

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     0.05       0.00     0.06
     2   0.0602  -1242.38     0.19     747.12     0.09
     3   0.0602  -1242.58     0.05     747.19     0.11
     4   0.1343  -1963.03    -0.22    1982.84    -0.06
     5   0.1423  -1976.68    -0.10    2127.45    -0.18
     6   2.0561   8663.00     0.06    4037.09    -0.09
     7   3.0528  13640.09    -0.12    5666.31     0.06
     8   3.1319  12662.57     0.08    6916.67     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.

14RR86    quality flag:3

Type:       SCATEXTD  SCATEXTD  SCATEXTD

axisobj        38.204    38.247    38.161
ecceobj         0.077     0.078     0.077
incobj         35.430    35.430    35.430
qmin           34.372    34.351    34.119
qmax           42.587    42.560    42.685
amean          38.347    38.350    38.271
amin           38.034    38.058    37.983
amax           38.670    38.666    38.574
emean           0.087     0.086     0.087
emin            0.071     0.071     0.070
emax            0.102     0.101     0.107
imean          35.417    35.425    35.398
imin           35.119    35.104    35.018
imax           35.792    35.815    35.786
excite_mean     0.586     0.586     0.586
fracstop        1.000     1.000     1.000
cjmean          2.618     2.618     2.618

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       180.8     180.9     181.0
kozaiamp        179.9     180.0     180.0