Orbit Fit and Astrometric record for 15RS245

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: 15RS245   
# Created Sun Apr 21 01:17:19 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     22 observations of     22
# Arc:   7.13y
# First observation: 2015/09/12
#  Last observation: 2022/10/29
# Chi-squared of fit:    15.20 DOF:     38 RMS:  0.15
# Min/Max residuals:    -0.53    0.24
# Exact a, adot, b, bdot, g, gdot:
  1.649858E-05  2.982564E-02  3.145933E-07 -1.840074E-03  2.765227E-02  9.996547E-04
# Covariance matrix:
  3.4486E-13 -1.9727E-13 -1.1293E-14  1.3449E-14  3.6260E-14 -7.8098E-13
 -1.9727E-13  4.6061E-13  4.2213E-14 -3.1232E-14  3.8466E-13  2.0510E-12
 -1.1293E-14  4.2213E-14  1.3872E-13 -3.9679E-14  4.1565E-14  1.9546E-13
  1.3449E-14 -3.1232E-14 -3.9679E-14  2.1972E-14 -2.4838E-14 -1.4576E-13
  3.6260E-14  3.8466E-13  4.1565E-14 -2.4838E-14  5.4035E-13  1.7497E-12
 -7.8098E-13  2.0510E-12  1.9546E-13 -1.4576E-13  1.7497E-12  9.5489E-12
#      lat0       lon0       xBary       yBary       zBary        JD0
  -16.169073   38.514004    0.767102   -0.182783   -0.631061  2457277.811391
# Heliocentric elements and errors
Epoch:              2457278.5000  =  2015/09/13
Mean Anomaly:            6.36102 +/-     0.061
Argument of Peri:      248.91958 +/-     0.073
Long of Asc Node:      141.29770 +/-     0.001
Inclination:            16.34413 +/-     0.000
Eccentricity:         0.08755131 +/-    0.0001
Semi-Major Axis:     40.30217378 +/-    0.0033
Time of Perihelion: 2455627.2414 +/-      15.8
Perihelion:          36.77366555 +/-    0.0037
Aphelion:            43.83068200 +/-    0.0042
Period (y)              255.8591 +/-      0.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           28.16477889 +/-    0.0007
Ecliptic Y           21.43709109 +/-    0.0006
Ecliptic Z          -10.07053145 +/-    0.0003
Ecliptic XDOT        -0.00180602 +/-    0.0000
Ecliptic YDOT         0.00233179 +/-    0.0000
Ecliptic ZDOT        -0.00020249 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   36.79971149 +/-    0.0007
Geocenter to KBO     36.16339950 +/-    0.0010
# Hcoef:  8.18

The following table shows the complete astrometric record for 15RS245. 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 (15RS245) followed by the observatory code and reference code for the source of the astrometry.

2015 09  12.310602 02 45 04.55   -01 00 29.1   23.7r 15RS245   W84  C~2B04      
2015 09  12.316921 02 45 04.52   -01 00 29.3   23.1z 15RS245   W84  C~2B04      
2015 10  16.303206 02 42 53.89   -01 20 20.2   23.6z 15RS245   W84  C~2B04      
2016 09  22.287778 02 51 10.21   -00 40 57.1   23.6z 15RS245   W84  C~2B04      
2016 10  05.178484 02 50 21.06   -00 48 30.7   23.9r 15RS245   W84  C~2B04      
2016 10  10.173299 02 49 59.13   -00 51 21.0   23.9r 15RS245   W84  C~2B04      
2016 10  10.175648 02 49 59.12   -00 51 21.1   23.8i 15RS245   W84  C~2B04      
2016 10  10.179618 02 49 59.08   -00 51 21.2   23.5z 15RS245   W84  C~2B04      
2016 11  10.096308 02 47 23.19   -01 06 03.4   23.5i 15RS245   W84  C~2B04      
2016 12  01.082419 02 45 37.91   -01 11 26.4   23.2i 15RS245   W84  C~2B04      
2016 12  17.173704 02 44 30.91   -01 12 13.1   23.6i 15RS245   W84  C~2B04      
2016 12  24.046597 02 44 07.94   -01 11 37.7   24.2r 15RS245   W84  C~2B04      
2016 12  24.048958 02 44 07.93   -01 11 37.6   24.0i 15RS245   W84  C~2B04      
2016 12  24.052940 02 44 07.92   -01 11 37.5   23.4z 15RS245   W84  C~2B04      
2017 11  14.196326 02 53 42.727  -00 41 20.92  23.6i 15RS245   W84  C~2g4S      
2017 11  14.200301 02 53 42.711  -00 41 21.35  23.6z 15RS245   W84  C~2g4S      
2017 12  07.097552 02 51 50.011  -00 46 09.54  24.1r 15RS245   W84  C~2g4S      
2017 12  07.099914 02 51 49.986  -00 46 09.57  23.7i 15RS245   W84  C~2g4S      
2017 12  26.082471 02 50 38.031  -00 45 39.10  23.5i 15RS245   W84  C~2g4S      
2017 12  26.086441 02 50 38.024  -00 45 39.05  23.6z 15RS245   W84  C~2g4S      
2022 10  29.378380 03 28 20.988  +01 35 03.39  24.3G 15RS245   G37  C~5z6Q      
2022 10  29.426420 03 28 20.758  +01 35 02.14        15RS245   G37  C~5z6Q      

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     0.20       0.00    -0.23
     2   0.0000      0.00    -0.00       0.00    -0.21
     3   0.0931      0.00    -0.00       0.00     0.13
     4   1.0294      0.00     0.07       0.00    -0.09
     5   1.0647      0.00     0.05       0.00    -0.14
     6   1.0783      0.00     0.07       0.00     0.11
     7   1.0783      0.00     0.08       0.00     0.09
     8   1.0784      0.00    -0.25       0.00     0.12
     9   1.1630      0.00    -0.09       0.00     0.20
    10   1.2205      0.00    -0.18       0.00    -0.53
    11   1.2645      0.00    -0.12       0.00     0.24
    12   1.2833      0.00     0.06       0.00     0.03
    13   1.2833      0.00     0.02       0.00     0.12
    14   1.2833      0.00     0.06       0.00     0.19
    15   2.1735      0.00     0.02       0.00     0.15
    16   2.1736      0.00     0.10       0.00    -0.20
    17   2.2362      0.00     0.06       0.00     0.06
    18   2.2362      0.00    -0.15       0.00     0.05
    19   2.2882      0.00     0.03       0.00     0.02
    20   2.2882      0.00     0.11       0.00     0.03
    21   7.1295      0.00    -0.11       0.00    -0.07
    22   7.1297      0.00     0.11       0.00    -0.03

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.

15RS245    quality flag:3

Type:       SCATEXTD  SCATEXTD  SCATEXTD

axisobj        40.733    40.732    40.733
ecceobj         0.097     0.097     0.097
incobj         16.324    16.324    16.324
qmin           35.933    35.799    35.979
qmax           45.147    45.186    45.122
amean          40.424    40.425    40.424
amin           40.082    40.060    40.087
amax           40.792    40.787    40.784
emean           0.094     0.090     0.092
emin            0.081     0.064     0.075
emax            0.108     0.111     0.107
imean          15.324    15.274    15.362
imin           14.295    14.258    14.316
imax           16.771    16.800    16.816
excite_mean     0.280     0.278     0.280
fracstop        1.000     1.000     1.000
cjmean          2.971     2.973     2.971

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       184.1     182.9     180.2
kozaiamp        180.0     180.0     180.0