Orbit Fit and Astrometric record for 16RL82

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: 16RL82    
# Created Sun Dec 22 02:10:46 2024
# Orbit generated from Bernstein formalism
# Fitting     19 observations of     20
# Arc:   3.86y
# First observation: 2015/01/19
#  Last observation: 2018/11/29
Preliminary a, adot, b, bdot, g, gdot:
  -0.000666   0.029943  -0.000127   0.009981   0.027173   0.000000
# Chi-squared of fit:     9.17 DOF:     32 RMS:  0.12
# Min/Max residuals:    -0.28    0.22
# Exact a, adot, b, bdot, g, gdot:
  1.639791E-05  2.854122E-02  7.109804E-06  9.570972E-03  2.633149E-02 -4.543331E-03
# Covariance matrix:
  8.4844E-13 -6.2987E-13  5.9928E-14 -1.3482E-13 -3.0073E-13 -3.6768E-12
 -6.2987E-13  7.2186E-13 -1.1142E-13  1.6293E-13  1.4160E-13  4.4472E-12
  5.9928E-14 -1.1142E-13  3.1897E-13 -1.3482E-13  1.1143E-14 -7.0248E-13
 -1.3482E-13  1.6293E-13 -1.3482E-13  9.3504E-14  4.4720E-14  1.0953E-12
 -3.0073E-13  1.4160E-13  1.1143E-14  4.4720E-14  2.7622E-13  1.2166E-12
 -3.6768E-12  4.4472E-12 -7.0248E-13  1.0953E-12  1.2166E-12  2.9892E-11
#      lat0       lon0       xBary       yBary       zBary        JD0
  -13.467355   26.736582   -0.981514    0.006387    0.025806  2457041.554318
# Heliocentric elements and errors
Epoch:              2457040.5000  =  2015/01/18
Mean Anomaly:          343.74451 +/-     0.019
Argument of Peri:      354.97208 +/-     0.039
Long of Asc Node:       62.61677 +/-     0.001
Inclination:            23.00410 +/-     0.000
Eccentricity:         0.30852778 +/-    0.0001
Semi-Major Axis:     52.98482835 +/-    0.0073
Time of Perihelion: 2463401.4682 +/-       7.3
Perihelion:          36.63753700 +/-    0.0082
Aphelion:            69.33211970 +/-    0.0115
Period (y)              385.6874 +/-      0.08
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           32.51589680 +/-    0.0006
Ecliptic Y           17.48175258 +/-    0.0004
Ecliptic Z           -8.84439280 +/-    0.0002
Ecliptic XDOT        -0.00154227 +/-    0.0000
Ecliptic YDOT         0.00254255 +/-    0.0000
Ecliptic ZDOT         0.00107790 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   37.96206662 +/-    0.0006
Geocenter to KBO     37.97734157 +/-    0.0008
# Hcoef:  7.99

The following table shows the complete astrometric record for 16RL82. 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 (16RL82) followed by the observatory code and reference code for the source of the astrometry.

2015 01  19.05354  01 58 31.925  -02 16 18.21  24.5g 16RL82    W84  C~55Zp      
2015 11  08.44094  02 07 17.48   -01 19 38.1   24.1r 16RL82    T09  C~89UA      
2015 11  08.44377  02 07 17.48   -01 19 38.1   24.0r 16RL82    T09  C~89UA      
2015 11  08.45382  02 07 17.41   -01 19 38.1   24.2r 16RL82    T09  C~89UA      
2015 11  08.46679  02 07 17.34   -01 19 38.5   24.1r 16RL82    T09  C~89UA      
2015 11  08.47551  02 07 17.30   -01 19 38.5   24.2r 16RL82    T09  C~89UA      
2016 09  07.51163  02 17 25.63   +00 12 45.8   23.6r 16RL82    T09  C~7xTL      
2016 09  07.53125  02 17 25.57   +00 12 45.3   23.5r 16RL82    T09  C~7xTL      
2016 09  07.59980  02 17 25.36   +00 12 43.7   23.7r 16RL82    T09  C~7xTL      
2016 09  07.60406  02 17 25.35   +00 12 43.7   23.5r 16RL82    T09  C~7xTL      
2016 09  10.30219  02 17 17.306  +00 11 35.01  23.3r 16RL82    W84  C~55Zp      
2016 12  23.05251  02 09 45.903  -00 13 15.13  24.3r 16RL82    W84  C~55Zp      
2017 10  13.24804  02 20 35.491  +01 05 49.72  23.9r 16RL82    W84  C~55Zp      
2017 10  21.22556  02 19 55.139  +01 02 42.25  24.2g 16RL82    W84  C~55Zp      
2017 11  16.18502  02 17 41.187  +00 55 01.50  22.8r 16RL82    W84  C~55Zp      
2017 12  07.03810  02 16 07.846  +00 52 57.41  23.1i 16RL82    W84  C~55Zp      
2018 09  11.33153  02 28 23.045  +02 27 59.25  22.8i 16RL82    W84  C~55Zp      
2018 09  11.33817  02 28 23.020  +02 27 58.96  23.7r 16RL82    W84  C~55Zp      
2018 09  11.33956  02 28 23.010  +02 27 59.23  24.0g 16RL82    W84  C~55Zp      
2018 11  29.17757  02 22 16.220  +02 02 00.86  24.4g 16RL82    W84  C~55Zp      

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     0.15       0.00    -0.28
     2   0.8033   8578.58    -0.10     371.26     0.01
     3   0.8033   8578.58     0.12     371.26    -0.03
     4   0.8033   8577.60    -0.08     371.63     0.21
     5   0.8033   8576.48    -0.20     371.63     0.04
     6   0.8033   8575.91    -0.09     371.85     0.13
     7   1.6358  19128.29     0.03    2301.99    -0.09
     8   1.6358  19127.27     0.00    2301.84    -0.09
     9   1.6360  19123.72    -0.03    2301.47     0.07
    10   1.6360  19123.58     0.04    2301.52     0.15
    11   1.6434  18985.16 (   0.57)   2280.26 (  -0.06)
    12   1.9274  12088.40     0.08    3303.34    -0.08
    13   2.7329  22966.11     0.06    4274.53    -0.19
    14   2.7547  22326.15    -0.03    4314.63     0.15
    15   2.8258  20262.97     0.22    4599.64    -0.07
    16   2.8829  18898.61    -0.06    4983.11     0.18
    17   3.6448  31423.34     0.10    6420.33    -0.08
    18   3.6449  31422.88    -0.02    6420.19    -0.18
    19   3.6449  31422.84     0.01    6420.50     0.14
    20   3.8607  25619.36    -0.21    6911.08     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.

16RL82    quality flag:3

Type:        7:3EEEE   7:3EEEE   7:3EEEE

axisobj        53.614    53.634    53.594
ecceobj         0.315     0.315     0.315
incobj         22.976    22.976    22.976
qmin           36.196    36.256    36.236
qmax           70.747    70.781    70.713
amean          52.968    52.968    52.968
amin           52.364    52.372    52.380
amax           53.717    53.736    53.699
emean           0.287     0.288     0.280
emin            0.250     0.262     0.224
emax            0.317     0.317     0.317
imean          22.676    22.634    22.927
imin           21.768    21.775    21.757
imax           23.854    23.469    24.853
excite_mean     0.481     0.481     0.480
fracstop        1.000     1.000     1.000
cjmean          2.912     2.912     2.912

libcent 0       179.7     182.7     183.0
libamp  0       134.5     138.3     141.8
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       134.1     156.7     114.4
kozaiamp        180.0     180.0     180.0