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: 03FH127
# Created Sat Nov 23 02:08:28 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 34 observations of 34
# Arc: 13.18y
# First observation: 2003/03/30
# Last observation: 2016/06/04
# Chi-squared of fit: 74.36 DOF: 62 RMS: 0.26
# Min/Max residuals: -0.38 1.23
# Exact a, adot, b, bdot, g, gdot:
1.157071E-05 2.503255E-02 -3.512537E-06 1.861183E-04 2.481617E-02 -1.034231E-03
# Covariance matrix:
3.1928E-13 2.1707E-12 1.5019E-16 1.6370E-14 1.7412E-12 6.4425E-12
2.1707E-12 3.6788E-11 2.3399E-15 2.7565E-13 2.8464E-11 1.0851E-10
1.5019E-16 2.3399E-15 1.8469E-13 -1.4135E-14 1.9282E-15 6.8967E-15
1.6370E-14 2.7565E-13 -1.4135E-14 3.4834E-15 2.1328E-13 8.1311E-13
1.7412E-12 2.8464E-11 1.9282E-15 2.1328E-13 2.2556E-11 8.3940E-11
6.4425E-12 1.0851E-10 6.8967E-15 8.1311E-13 8.3940E-11 3.2010E-10
# lat0 lon0 xBary yBary zBary JD0
0.251043 165.436601 -0.403537 0.003993 -0.912113 2452728.697483
# Heliocentric elements and errors
Epoch: 2452728.5000 = 2003/03/30
Mean Anomaly: 338.39402 +/- 0.433
Argument of Peri: 55.00847 +/- 0.507
Long of Asc Node: 136.04778 +/- 0.007
Inclination: 0.49137 +/- 0.000
Eccentricity: 0.07487502 +/- 0.0004
Semi-Major Axis: 44.25679454 +/- 0.0161
Time of Perihelion: 2459182.6628 +/- 140.7
Perihelion: 40.94306621 +/- 0.0241
Aphelion: 47.57052288 +/- 0.0257
Period (y) 294.4273 +/- 0.16
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -39.98757631 +/- 0.0075
Ecliptic Y 9.97518221 +/- 0.0020
Ecliptic Z 0.17643337 +/- 0.0000
Ecliptic XDOT -0.00059029 +/- 0.0000
Ecliptic YDOT -0.00270646 +/- 0.0000
Ecliptic ZDOT 0.00002022 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 41.21338642 +/- 0.0073
Geocenter to KBO 40.29637891 +/- 0.0077
# Hcoef: 7.33
The following table shows the complete astrometric record for 03FH127. 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 (03FH127) followed by the observatory code and reference code for the source of the astrometry.
2003 03 30.19674 11 06 45.79 +05 58 18.8 23.4R 03FH127 695 Ch8427 2003 03 30.29353 11 06 45.32 +05 58 21.4 03FH127 695 Ch8427 2003 03 31.28789 11 06 41.17 +05 58 47.9 03FH127 695 Ch8427 2003 04 01.213623 11 06 37.40 +05 59 10.1 22.7V 03FH127 645 C~1jgs 2003 04 01.214038 11 06 37.40 +05 59 10.1 22.6V 03FH127 645 C~1jgs 2003 04 01.214452 11 06 37.40 +05 59 10.1 22.4V 03FH127 645 C~1jgs 2003 04 01.214867 11 06 37.39 +05 59 10.1 22.4V 03FH127 645 C~1jgs 2003 04 01.216940 11 06 37.38 +05 59 10.2 23.0V 03FH127 645 C~1jgs 2003 04 01.217355 11 06 37.38 +05 59 10.2 22.9V 03FH127 645 C~1jgs 2003 04 20.99034 11 05 26.83 +06 06 29.7 21.8R 03FH127 304 Ch8427 2003 04 21.05012 11 05 26.61 +06 06 30.8 03FH127 304 Ch8427 2016 04 02.37971 12 15 58.73 -01 19 15.0 23.8i 03FH127 T09 C~8Ghv 2016 04 02.40651 12 15 58.58 -01 19 14.2 23.3i 03FH127 T09 C~8Ghv 2016 04 02.43374 12 15 58.46 -01 19 13.3 23.2i 03FH127 T09 C~8Ghv 2016 04 02.45821 12 15 58.35 -01 19 12.5 23.4i 03FH127 T09 C~8Ghv 2016 04 02.48284 12 15 58.24 -01 19 12.0 23.4i 03FH127 T09 C~8Ghv 2016 04 02.48823 12 15 58.23 -01 19 11.8 23.3i 03FH127 T09 C~8Ghv 2016 04 04.33742 12 15 49.91 -01 18 17.9 24.5g 03FH127 T09 C~8Ghv 2016 04 04.35952 12 15 49.81 -01 18 17.2 24.6g 03FH127 T09 C~8Ghv 2016 04 04.38088 12 15 49.71 -01 18 16.7 24.7g 03FH127 T09 C~8Ghv 2016 04 04.39802 12 15 49.63 -01 18 16.2 24.4g 03FH127 T09 C~8Ghv 2016 04 04.40435 12 15 49.62 -01 18 15.7 24.6g 03FH127 T09 C~8Ghv 2016 04 08.50164 12 15 31.42 -01 16 18.1 23.6r 03FH127 T09 C~8Ghv 2016 04 08.50945 12 15 31.39 -01 16 17.8 23.5r 03FH127 T09 C~8Ghv 2016 04 08.52214 12 15 31.33 -01 16 17.6 23.8r 03FH127 T09 C~8Ghv 2016 04 08.52425 12 15 31.32 -01 16 17.6 23.8r 03FH127 T09 C~8Ghv 2016 04 15.24211 12 15 02.48 -01 13 11.2 23.3y 03FH127 T09 C~8Ghv 2016 04 15.40002 12 15 01.80 -01 13 06.8 23.4y 03FH127 T09 C~8Ghw 2016 04 15.44590 12 15 01.61 -01 13 05.5 22.9y 03FH127 T09 C~8Ghw 2016 06 04.24512 12 12 43.65 -00 58 27.6 23.4z 03FH127 T09 C~8Ghw 2016 06 04.26496 12 12 43.63 -00 58 27.4 23.1z 03FH127 T09 C~8Ghw 2016 06 04.28119 12 12 43.62 -00 58 27.2 23.1z 03FH127 T09 C~8Ghw 2016 06 04.30006 12 12 43.60 -00 58 27.2 23.2z 03FH127 T09 C~8Ghw 2016 06 04.31896 12 12 43.58 -00 58 27.2 23.6z 03FH127 T09 C~8Ghw
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 1.13 0.00 0.34
2 0.0003 0.00 0.22 0.00 0.43
3 0.0030 0.00 -0.37 0.00 1.23
4 0.0055 0.00 -0.12 0.00 -0.26
5 0.0055 0.00 -0.09 0.00 -0.27
6 0.0055 0.00 -0.07 0.00 -0.28
7 0.0055 0.00 -0.19 0.00 -0.29
8 0.0055 0.00 -0.21 0.00 -0.24
9 0.0055 0.00 -0.19 0.00 -0.25
10 0.0597 0.00 0.18 0.00 -0.20
11 0.0598 0.00 -0.38 0.00 -0.20
12 13.0108 0.00 0.24 0.00 -0.10
13 13.0108 0.00 -0.16 0.00 -0.08
14 13.0109 0.00 -0.08 0.00 0.02
15 13.0110 0.00 -0.05 0.00 0.11
16 13.0111 0.00 -0.00 0.00 -0.11
17 13.0111 0.00 0.22 0.00 -0.07
18 13.0161 0.00 -0.09 0.00 -0.03
19 13.0162 0.00 -0.08 0.00 0.03
20 13.0162 0.00 -0.12 0.00 -0.09
21 13.0163 0.00 -0.14 0.00 -0.09
22 13.0163 0.00 0.14 0.00 0.23
23 13.0275 0.00 0.02 0.00 0.13
24 13.0276 0.00 0.09 0.00 0.20
25 13.0276 0.00 0.04 0.00 0.04
26 13.0276 0.00 0.03 0.00 -0.02
27 13.0460 0.00 -0.02 0.00 -0.07
28 13.0464 0.00 -0.12 0.00 0.07
29 13.0465 0.00 -0.03 0.00 0.13
30 13.1829 0.00 -0.07 0.00 -0.12
31 13.1829 0.00 -0.06 0.00 -0.03
32 13.1830 0.00 0.04 0.00 0.07
33 13.1830 0.00 0.03 0.00 -0.03
34 13.1831 0.00 0.01 0.00 -0.14
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.
03FH127 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