Orbit Fit and Astrometric record for 15DT248

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: 15DT248   
# Created Wed Apr 24 01:16:58 2024
# Orbit generated from Bernstein formalism
# Fitting     20 observations of     20
# Arc:  10.10d
# First observation: 2015/02/17
#  Last observation: 2015/02/27
Preliminary a, adot, b, bdot, g, gdot:
  -0.000002   0.110557   0.000000   0.026398   0.065576   0.000000
# Chi-squared of fit:    16.83 DOF:     34 RMS:  0.16
# Min/Max residuals:    -0.35    0.38
# Exact a, adot, b, bdot, g, gdot:
  2.552791E-05  1.032953E-01  6.099061E-06  2.674040E-02  6.452193E-02  2.974040E-02
# Covariance matrix:
  1.1600E-12  3.5550E-09  2.7216E-13 -1.3515E-10  5.6642E-10  9.9794E-11
  3.5550E-09  1.3952E-05  1.1130E-09 -5.4288E-07  2.1962E-06 -1.6140E-05
  2.7216E-13  1.1130E-09  2.3112E-13 -5.1485E-11  1.7459E-10 -1.7542E-09
 -1.3515E-10 -5.4288E-07 -5.1485E-11  2.2136E-08 -8.5285E-08  7.6295E-07
  5.6642E-10  2.1962E-06  1.7459E-10 -8.5285E-08  3.4602E-07 -2.3260E-06
  9.9794E-11 -1.6140E-05 -1.7542E-09  7.6295E-07 -2.3260E-06  1.8192E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
  -18.226059  145.266934   -0.043044   -0.307655   -0.934923  2457070.555374
# Heliocentric elements and errors
Epoch:              2457070.5000  =  2015/02/17
Mean Anomaly:           33.93071 +/-     6.198
Argument of Peri:      241.47956 +/-    12.674
Long of Asc Node:      194.67292 +/-     1.111
Inclination:            22.16543 +/-     0.345
Eccentricity:         0.35327389 +/-    0.1259
Semi-Major Axis:     21.36368458 +/-    2.1037
Time of Perihelion: 2453671.0934 +/-     365.4
Perihelion:          13.81645262 +/-    3.0145
Aphelion:            28.91091655 +/-    3.9168
Period (y)               98.7467 +/-     14.59
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -12.93463660 +/-    0.1103
Ecliptic Y            8.91306411 +/-    0.0765
Ecliptic Z           -4.84741353 +/-    0.0442
Ecliptic XDOT        -0.00377768 +/-    0.0004
Ecliptic YDOT        -0.00272254 +/-    0.0004
Ecliptic ZDOT         0.00068314 +/-    0.0002
# Distances at JD0 (AU)
Heliocenter to KBO   16.43912874 +/-    0.0971
Geocenter to KBO     15.49860612 +/-    0.1413
# Hcoef: 11.60

The following table shows the complete astrometric record for 15DT248. 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 (15DT248) followed by the observatory code and reference code for the source of the astrometry.

2015 02  17.054596 09 25 59.79   -04 06 40.5   23.6r 15DT248   W84  C~5PvV      
2015 02  17.12194  09 25 59.08   -04 06 35.8   23.9g 15DT248   W84  C~2iOV      
2015 02  17.20722  09 25 58.14   -04 06 29.5   23.8g 15DT248   W84  C~2iOV      
2015 02  17.27585  09 25 57.41   -04 06 24.5   24.4g 15DT248   W84  C~2iOV      
2015 02  18.05075  09 25 49.29   -04 05 26.9   24.0g 15DT248   W84  C~2iOV      
2015 02  18.11851  09 25 48.57   -04 05 21.9   24.3g 15DT248   W84  C~2iOV      
2015 02  18.18617  09 25 47.84   -04 05 16.9   24.5g 15DT248   W84  C~2iOV      
2015 02  18.25467  09 25 47.11   -04 05 11.5         15DT248   W84  C~2iOV      
2015 02  18.32507  09 25 46.37   -04 05 06.5         15DT248   W84  C~2iOV      
2015 02  19.04743  09 25 38.85   -04 04 12.5   24.1g 15DT248   W84  C~2iOV      
2015 02  19.18419  09 25 37.38   -04 04 01.9   24.1g 15DT248   W84  C~2iOV      
2015 02  19.25293  09 25 36.67   -04 03 56.9   24.1g 15DT248   W84  C~2iOV      
2015 02  19.32206  09 25 35.94   -04 03 51.9   24.3g 15DT248   W84  C~2iOV      
2015 02  22.04005  09 25 07.77   -04 00 21.5         15DT248   W84  C~2iOV      
2015 02  22.10764  09 25 07.08   -04 00 16.5         15DT248   W84  C~2iOV      
2015 02  22.17516  09 25 06.37   -04 00 11.5         15DT248   W84  C~2iOV      
2015 02  22.24395  09 25 05.66   -04 00 05.5         15DT248   W84  C~2iOV      
2015 02  27.03560  09 24 17.37   -03 53 38.0         15DT248   W84  C~2iOV      
2015 02  27.08376  09 24 16.90   -03 53 34.0         15DT248   W84  C~2iOV      
2015 02  27.15145  09 24 16.19   -03 53 28.4         15DT248   W84  C~2iOV      

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    -0.04       0.00     0.09
     2   0.0002    -11.58     0.21       0.96    -0.06
     3   0.0004    -26.93    -0.13       2.30    -0.14
     4   0.0006    -38.89    -0.01       3.45    -0.15
     5   0.0027   -172.54    -0.13      18.04     0.09
     6   0.0029   -184.36    -0.07      19.24     0.08
     7   0.0031   -196.32    -0.13      20.38     0.01
     8   0.0033   -208.40    -0.18      21.90     0.30
     9   0.0035   -220.50     0.06      22.99     0.10
    10   0.0055   -344.50     0.16      37.13    -0.13
    11   0.0058   -368.76    -0.13      39.93     0.06
    12   0.0060   -380.43     0.25      41.17    -0.02
    13   0.0062   -392.39     0.38      42.31    -0.24
    14   0.0136   -859.59    -0.34     102.86     0.16
    15   0.0138   -870.98    -0.01     104.19    -0.05
    16   0.0140   -882.66     0.05     105.43    -0.35
    17   0.0142   -894.66     0.01     107.61     0.25
    18   0.0273  -1704.46     0.02     236.56     0.00
    19   0.0275  -1712.42     0.21     238.03     0.08
    20   0.0276  -1724.30    -0.18     239.83    -0.08

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.

15DT248    quality flag:0

Type:      ERR2LARGE ERR2LARGE ERR2LARGE

axisobj         0.000     0.000     0.000
ecceobj        -1.000    -1.000    -1.000
incobj         -1.000    -1.000    -1.000
qmin            0.000     0.000     0.000
qmax            0.000     0.000     0.000
amean           0.000     0.000     0.000
amin            0.000     0.000     0.000
amax            0.000     0.000     0.000
emean           0.000     0.000     0.000
emin            0.000     0.000     0.000
emax            0.000     0.000     0.000
imean           0.000     0.000     0.000
imin            0.000     0.000     0.000
imax            0.000     0.000     0.000
excite_mean     0.000     0.000     0.000
fracstop        0.000     0.000     0.000
cjmean          0.000     0.000     0.000

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         0.0       0.0       0.0
kozaiamp          0.0       0.0       0.0