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: 15RV245
# Created Wed Apr 24 01:17:21 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 34 observations of 34
# Arc: 5.25y
# First observation: 2015/06/23
# Last observation: 2020/09/21
# Chi-squared of fit: 6.93 DOF: 62 RMS: 0.08
# Min/Max residuals: -0.24 0.22
# Exact a, adot, b, bdot, g, gdot:
1.965398E-05 6.181708E-02 5.577438E-06 1.723567E-02 5.033300E-02 3.840570E-02
# Covariance matrix:
1.1245E-13 -1.8288E-14 -1.8137E-15 -1.9451E-15 7.1507E-14 -1.0178E-14
-1.8288E-14 3.4218E-13 -3.9587E-14 9.3821E-14 1.9064E-13 1.2421E-12
-1.8137E-15 -3.9587E-14 6.4894E-14 -3.5874E-14 -2.5748E-14 -1.5789E-13
-1.9451E-15 9.3821E-14 -3.5874E-14 6.0744E-14 5.2938E-14 3.7813E-13
7.1507E-14 1.9064E-13 -2.5748E-14 5.2938E-14 2.0528E-13 7.2101E-13
-1.0178E-14 1.2421E-12 -1.5789E-13 3.7813E-13 7.2101E-13 4.9963E-12
# lat0 lon0 xBary yBary zBary JD0
2.136820 10.724183 1.004037 -0.005779 0.157473 2457197.102368
# Heliocentric elements and errors
Epoch: 2457196.5000 = 2015/06/23
Mean Anomaly: 51.09374 +/- 0.003
Argument of Peri: 260.65101 +/- 0.002
Long of Asc Node: 359.97636 +/- 0.000
Inclination: 15.41692 +/- 0.000
Eccentricity: 0.47905568 +/- 0.0000
Semi-Major Axis: 21.92672160 +/- 0.0008
Time of Perihelion: 2451873.8954 +/- 0.5
Perihelion: 11.42260103 +/- 0.0007
Aphelion: 32.43084217 +/- 0.0013
Period (y) 102.6760 +/- 0.01
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X 19.53562293 +/- 0.0002
Ecliptic Y 2.67884059 +/- 0.0000
Ecliptic Z 0.74095008 +/- 0.0000
Ecliptic XDOT 0.00138864 +/- 0.0000
Ecliptic YDOT 0.00367952 +/- 0.0000
Ecliptic ZDOT 0.00101484 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 19.73213510 +/- 0.0002
Geocenter to KBO 19.86746375 +/- 0.0002
# Hcoef: 10.14
The following table shows the complete astrometric record for 15RV245. 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 (15RV245) followed by the observatory code and reference code for the source of the astrometry.
2015 06 23.60159 00 36 03.636 +06 12 36.77 22.6r 15RV245 568 C~2Gdr 2015 07 14.55013 00 36 36.879 +06 22 24.67 22.9r 15RV245 568 C~2Gdr 2015 07 19.52115 00 36 33.010 +06 23 30.24 22.8r 15RV245 568 C~2Gdr 2015 08 13.48810 00 35 07.928 +06 21 51.70 23.6r 15RV245 568 C~2Gds 2015 08 13.54153 00 35 07.612 +06 21 50.72 23.1r 15RV245 568 C~2Gds 2015 08 13.56200 00 35 07.521 +06 21 50.32 23.1r 15RV245 568 C~2Gds 2015 08 19.55072 00 34 32.079 +06 19 45.89 23.2r 15RV245 568 C~2Gds 2015 08 19.59211 00 34 31.809 +06 19 44.68 23.8r 15RV245 568 C~2Gds 2015 08 19.62083 00 34 31.640 +06 19 44.05 23.0r 15RV245 568 C~2Gds 2015 08 20.42524 00 34 26.507 +06 19 24.45 22.7r 15RV245 568 C~2Gds 2015 08 20.47472 00 34 26.177 +06 19 23.24 22.7r 15RV245 568 C~2Gds 2015 09 07.56844 00 32 09.496 +06 09 33.42 23.5w 15RV245 568 C~2Gds 2015 09 09.39585 00 31 53.871 +06 08 19.69 23.2r 15RV245 568 C~2Gds 2015 09 09.43729 00 31 53.504 +06 08 18.06 23.2r 15RV245 568 C~2Gds 2015 09 09.47825 00 31 53.143 +06 08 16.35 23.2r 15RV245 568 C~2Gds 2015 09 10.50253 00 31 44.240 +06 07 34.02 23.5w 15RV245 568 C~2Gds 2015 09 18.46210 00 30 32.702 +06 01 44.62 23.4w 15RV245 568 C~2Gds 2015 10 08.34456 00 27 25.291 +05 45 31.35 23.3w 15RV245 568 C~2Gds 2015 10 08.39722 00 27 24.794 +05 45 28.72 22.3w 15RV245 568 C~2Gds 2015 10 09.31422 00 27 16.203 +05 44 42.46 22.7w 15RV245 568 C~2Gds 2015 11 10.43470 00 22 52.237 +05 20 14.45 23.7w 15RV245 568 C~2Gds 2015 12 08.23353 00 20 53.982 +05 09 00.93 23.4w 15RV245 568 C~2Gds 2016 01 01.29622 00 21 05.747 +05 10 53.53 23.8w 15RV245 568 C~2Gds 2016 09 05.57499 00 44 09.356 +08 29 28.60 15RV245 568 C~2Gds 2016 09 06.52410 00 44 01.804 +08 28 55.95 15RV245 568 C~2Gds 2016 09 06.56619 00 44 01.461 +08 28 54.42 15RV245 568 C~2Gds 2016 09 27.47990 00 40 58.618 +08 14 25.77 23.5w 15RV245 568 C~2Gds 2016 12 25.26669 00 32 24.738 +07 24 40.20 15RV245 568 C~2Gds 2016 12 26.24341 00 32 25.707 +07 24 44.24 15RV245 568 C~2Gds 2016 12 29.23147 00 32 29.778 +07 25 03.67 15RV245 568 C~2Gds 2017 01 02.30911 00 32 37.994 +07 25 47.04 15RV245 568 C~2Gds 2017 01 27.27188 00 34 32.121 +07 37 11.01 24.2w 15RV245 568 C~2Gds 2020 09 21.344390 01 23 48.363 +16 02 52.10 24.4G 15RV245 G37 C~4AD9 2020 09 21.401200 01 23 47.915 +16 02 50.44 15RV245 G37 C~4AD9
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 -0.03 0.00 -0.05
2 0.0574 0.00 -0.09 0.00 -0.08
3 0.0710 0.00 0.03 0.00 0.01
4 0.1393 0.00 -0.02 0.00 0.09
5 0.1395 0.00 -0.24 0.00 0.05
6 0.1395 0.00 0.13 0.00 0.01
7 0.1559 0.00 -0.14 0.00 0.22
8 0.1560 0.00 -0.14 0.00 -0.00
9 0.1561 0.00 0.14 0.00 0.06
10 0.1583 0.00 -0.03 0.00 -0.02
11 0.1584 0.00 -0.07 0.00 -0.02
12 0.2080 0.00 0.07 0.00 0.09
13 0.2130 0.00 0.04 0.00 0.01
14 0.2131 0.00 0.01 0.00 0.07
15 0.2132 0.00 0.02 0.00 0.04
16 0.2160 0.00 0.01 0.00 0.00
17 0.2378 0.00 0.13 0.00 -0.04
18 0.2922 0.00 0.00 0.00 -0.10
19 0.2924 0.00 0.11 0.00 -0.08
20 0.2949 0.00 0.10 0.00 -0.07
21 0.3828 0.00 -0.05 0.00 -0.00
22 0.4590 0.00 0.12 0.00 -0.07
23 0.5248 0.00 0.04 0.00 -0.12
24 1.2046 0.00 0.07 0.00 -0.01
25 1.2072 0.00 0.04 0.00 0.06
26 1.2073 0.00 0.06 0.00 0.00
27 1.2646 0.00 0.13 0.00 -0.02
28 1.5076 0.00 -0.10 0.00 -0.04
29 1.5103 0.00 -0.11 0.00 -0.04
30 1.5185 0.00 0.00 0.00 0.08
31 1.5297 0.00 0.07 0.00 0.09
32 1.5980 0.00 -0.07 0.00 -0.03
33 5.2478 0.00 -0.04 0.00 -0.01
34 5.2479 0.00 0.02 0.00 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.
15RV245 quality flag:3 Type: CENTAURR CENTAURR CENTAURR axisobj 21.861 21.861 21.861 ecceobj 0.477 0.477 0.477 incobj 15.406 15.406 15.406 qmin 10.920 11.326 11.344 qmax 36.427 33.175 33.490 amean 22.214 21.578 21.339 amin 20.777 20.686 20.440 amax 24.005 22.359 22.494 emean 0.486 0.467 0.457 emin 0.450 0.423 0.416 emax 0.517 0.487 0.489 imean 17.640 16.860 17.420 imin 15.902 15.902 15.902 imax 19.893 19.415 19.458 excite_mean 0.573 0.550 0.547 fracstop 0.013 0.004 0.005 cjmean 2.787 2.824 2.837 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 175.8 301.6 282.4 kozaiamp 178.4 43.0 178.3