Orbit Fit and Astrometric record for 17BE241

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: 17BE241   
# Created Wed Nov 27 02:10:46 2024
# Orbit generated from Bernstein formalism
# Fitting      8 observations of      8
# Arc:  31.03d
# First observation: 2017/01/23
#  Last observation: 2017/02/23
Preliminary a, adot, b, bdot, g, gdot:
  -0.000001   0.020988   0.000000  -0.001382   0.023160   0.000000
# WARNING Fitting with energy constraint
# WARNING MRQMIN stopped after  14 iterations -- oscilliatory solution
# Chi-squared of fit:     5.13 DOF:     11 RMS:  0.14
# Min/Max residuals:    -0.20    0.41
# Exact a, adot, b, bdot, g, gdot:
  1.397549E-05  2.128153E-02 -5.354302E-07 -1.391725E-03  2.305632E-02 -5.297386E-03
# Covariance matrix:
  2.2945E-10  3.4008E-07 -1.0901E-11 -1.5859E-08  8.2451E-08  7.8533E-07
  3.4008E-07  5.0485E-04 -1.6183E-08 -2.3543E-05  1.2240E-04  1.1657E-03
 -1.0901E-11 -1.6183E-08  8.8045E-13  7.5042E-10 -3.9235E-09 -3.7383E-08
 -1.5859E-08 -2.3543E-05  7.5042E-10  1.0980E-06 -5.7080E-06 -5.4380E-05
  8.2451E-08  1.2240E-04 -3.9235E-09 -5.7080E-06  2.9676E-05  2.8340E-04
  7.8533E-07  1.1657E-03 -3.7383E-08 -5.4380E-05  2.8340E-04  3.2097E-03
#      lat0       lon0       xBary       yBary       zBary        JD0
    2.353453 -172.667861    0.886719    0.017874   -0.430738  2457777.108391
# Heliocentric elements and errors
Epoch:              2457770.5000  =  2017/01/17
Mean Anomaly:          287.95013 +/-   134.749
Argument of Peri:      250.00204 +/-   217.334
Long of Asc Node:       38.26499 +/-     9.429
Inclination:             4.37920 +/-     1.188
Eccentricity:         0.26091494 +/-    2.6229
Semi-Major Axis:     44.43108940 +/-   23.3654
Time of Perihelion: 2479420.5844 +/-   36712.5
Perihelion:          32.83835416 +/-  117.8108
Aphelion:            56.02382463 +/-  120.2047
Period (y)              296.1683 +/-    233.62
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -43.52511242 +/-   10.1553
Ecliptic Y           -4.71075437 +/-    1.3062
Ecliptic Z            1.78098840 +/-    0.4208
Ecliptic XDOT         0.00094198 +/-    0.0066
Ecliptic YDOT        -0.00243379 +/-    0.0029
Ecliptic ZDOT        -0.00019101 +/-    0.0002
# Distances at JD0 (AU)
Heliocenter to KBO   43.81550567 +/-   10.0890
Geocenter to KBO     43.37205490 +/-   10.2476
# Hcoef:  9.08

The following table shows the complete astrometric record for 17BE241. 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 (17BE241) followed by the observatory code and reference code for the source of the astrometry.

2017 01  23.60759  12 30 38.99   -00 44 51.1   25.1i 17BE241   T09  C~86ul      
2017 01  23.61026  12 30 38.97   -00 44 51.0   25.1i 17BE241   T09  C~86ul      
2017 01  23.62432  12 30 38.96   -00 44 51.0   24.8i 17BE241   T09  C~86ul      
2017 01  23.64653  12 30 38.93   -00 44 50.1   25.4i 17BE241   T09  C~86ul      
2017 02  23.53583  12 29 19.97   -00 35 22.9   25.7r 17BE241   T09  C~86um      
2017 02  23.56346  12 29 19.86   -00 35 22.4   26.0r 17BE241   T09  C~86um      
2017 02  23.60592  12 29 19.71   -00 35 21.2   25.7r 17BE241   T09  C~86um      
2017 02  23.63774  12 29 19.60   -00 35 20.6   25.2r 17BE241   T09  C~86um      

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     0.13       0.00    -0.09
     2   0.0000     -0.32    -0.12      -0.03    -0.12
     3   0.0000     -0.45     0.10      -0.09    -0.20
     4   0.0001     -1.22    -0.11       0.56     0.41
     5   0.0847  -1313.27     0.05      54.42     0.09
     6   0.0848  -1314.98    -0.03      54.23    -0.12
     7   0.0849  -1317.53    -0.07      54.44     0.07
     8   0.0850  -1319.28     0.06      54.34    -0.05

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.