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: 612029 # Created Wed Apr 16 01:07:42 2025 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 54 observations of 54 # Arc: 27.09y # First observation: 1995/04/26 # Last observation: 2022/05/29 # Chi-squared of fit: 456.53 DOF: 102 RMS: 0.51 # Min/Max residuals: -1.94 1.10 # Exact a, adot, b, bdot, g, gdot: 1.551527E-05 3.601857E-02 2.063605E-06 3.041986E-03 3.120720E-02 -7.607095E-03 # Covariance matrix: 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 # lat0 lon0 xBary yBary zBary JD0 -0.024370 -174.475853 -0.493630 -0.000363 -0.873471 2449833.532868 # Heliocentric elements and errors Epoch: 2449834.5000 = 1995/04/27 Mean Anomaly: 322.75177 +/- 0.000 Argument of Peri: 59.95984 +/- 0.000 Long of Asc Node: 186.67893 +/- 0.000 Inclination: 4.80759 +/- 0.000 Eccentricity: 0.25538729 +/- 0.0000 Semi-Major Axis: 39.68113710 +/- 0.0000 Time of Perihelion: 2459281.1474 +/- 0.0 Perihelion: 29.54707916 +/- 0.0000 Aphelion: 49.81519505 +/- 0.0000 Period (y) 249.9680 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X -32.71514638 +/- 0.0000 Ecliptic Y -3.66816545 +/- 0.0000 Ecliptic Z -0.01359821 +/- 0.0000 Ecliptic XDOT 0.00097556 +/- 0.0000 Ecliptic YDOT -0.00308177 +/- 0.0000 Ecliptic ZDOT 0.00026698 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 32.92026772 +/- 0.0000 Geocenter to KBO 32.04405240 +/- 0.0000 # Hcoef: 7.70
The following table shows the complete astrometric record for 612029. 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 (612029) followed by the observatory code and reference code for the source of the astrometry.
1995 04 26.03216 12 20 14.67 -02 13 00.8 23.1R 612029 807 C25290 1995 04 26.08712 12 20 14.40 -02 12 59.9 612029 807 C25290 1995 04 26.22696 12 20 13.76 -02 12 55.1 612029 807 C25290 1995 04 29.08141 12 20 00.89 -02 11 26.2 612029 807 C25290 1995 04 29.12764 12 20 00.64 -02 11 24.7 612029 807 C25290 1995 04 29.13859 12 20 00.58 -02 11 24.5 612029 807 C25290 1995 04 30.07257 12 19 56.48 -02 10 55.8 612029 807 C25290 1995 04 30.15451 12 19 56.12 -02 10 53.3 612029 807 C25290 1995 05 29.2762 12 18 23.78 -02 00 01.7 612029 568 A25268 1995 05 29.3259 12 18 23.71 -02 00 00.9 612029 568 A25268 1996 01 23.51602 12 35 02.24 -03 39 49.3 612029 675 C26660 1996 01 24.54596 12 35 00.74 -03 39 37.9 612029 675 C26660 1996 04 09.21942 12 29 32.42 -03 02 00.5 612029 675 C27019 1996 04 09.28684 12 29 32.07 -03 01 57.8 612029 675 C27019 1997 02 07.48095 12 42 28.36 -04 15 14.7 612029 697 C29057 1997 02 08.48575 12 42 25.51 -04 14 53.5 612029 697 C29057 1997 02 08.52943 12 42 25.34 -04 14 52.9 612029 697 C29057 1997 03 04.06538 12 40 52.69 -04 04 09.9 612029 950 C30063 1997 03 05.06227 12 40 47.93 -04 03 36.8 612029 950 C30063 1998 05 23.94595 12 42 25.83 -03 59 58.2 612029 950 Ca1684 1998 05 23.97733 12 42 25.72 -03 59 57.7 612029 950 Ca1684 1998 05 24.00590 12 42 25.63 -03 59 57.2 612029 950 Ca1684 1998 05 24.93269 12 42 22.91 -03 59 38.4 612029 950 Ca1684 1998 05 24.98981 12 42 22.67 -03 59 37.3 612029 950 Ca1684 1999 03 10.27373 12 56 54.82 -05 21 34.7 612029 829 Cb7364 1999 03 10.32535 12 56 54.56 -05 21 32.0 612029 829 Cb7364 1999 05 23.19262 12 50 41.09 -04 40 25.5 612029 697 Cb0719 1999 05 23.25778 12 50 40.85 -04 40 23.6 23.1R 612029 697 Cb0719 2001 12 23.969850 13 23 25.255 -07 33 03.30 612029 250 S~8qqs 2001 12 23.973323 13 23 25.262 -07 33 03.38 612029 250 S~8qqs 2001 12 23.976100 13 23 25.265 -07 33 03.46 612029 250 S~8qqs 2001 12 23.979573 13 23 25.279 -07 33 03.58 612029 250 S~8qqs 2001 12 23.982350 13 23 25.285 -07 33 03.65 612029 250 S~8qqs 2001 12 23.985823 13 23 25.298 -07 33 03.72 612029 250 S~8qqs 2004 04 26.33202 13 36 03.65 -08 16 06.1 22.6g 612029 568 C~0Uq7 2004 04 26.35319 13 36 03.51 -08 16 05.1 22.5g 612029 568 C~0Uq7 2004 04 26.37961 13 36 03.36 -08 16 04.3 22.6g 612029 568 C~0Uq7 2004 04 27.32697 13 35 57.94 -08 15 31.4 22.9g 612029 568 C~0Uq7 2004 06 20.27381 13 32 17.83 -07 54 17.1 22.7i 612029 568 C~0Uq7 2004 06 20.32279 13 32 17.75 -07 54 16.6 22.9i 612029 568 C~0Uq7 2004 06 20.37510 13 32 17.66 -07 54 15.9 22.9i 612029 568 C~0Uq7 2013 05 08.418557 15 01 34.738 -13 47 40.09 612029 250 S~8qqs 2013 05 08.424471 15 01 34.694 -13 47 40.05 612029 250 S~8qqs 2016 06 08.20956 15 29 19.970 -15 08 13.60 22.3R 612029 G37 C~2bkL 2016 06 08.23206 15 29 19.835 -15 08 13.02 612029 G37 C~2bkL 2020 07 18.30161 16 08 21.608 -16 42 28.64 22.5w 612029 F51 C~3yxG 2020 07 18.31349 16 08 21.540 -16 42 28.60 22.7w 612029 F51 C~3yxG 2020 07 18.32534 16 08 21.515 -16 42 28.55 22.4w 612029 F51 C~3yxG 2022 05 29.06854 16 34 33.148 -17 30 11.19 22.2r 612029 269 C~8kmj 2022 05 29.07082 16 34 33.133 -17 30 11.16 22.7g 612029 269 C~8kmj 2022 05 29.07374 16 34 33.115 -17 30 11.08 21.7z 612029 269 C~8kmj 2022 05 29.07949 16 34 33.074 -17 30 11.03 21.9z 612029 269 C~8kmj 2022 05 29.08262 16 34 33.051 -17 30 10.99 22.7g 612029 269 C~8kmj 2022 05 29.08480 16 34 33.037 -17 30 10.95 22.4r 612029 269 C~8kmj
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 0.48 0.00 -0.32
2 0.0002 0.00 0.30 0.00 -1.16
3 0.0005 0.00 0.54 0.00 -0.79
4 0.0083 0.00 0.27 0.00 -0.51
5 0.0085 0.00 -0.34 0.00 -0.41
6 0.0085 0.00 -0.50 0.00 -0.55
7 0.0111 0.00 -0.71 0.00 -0.09
8 0.0113 0.00 -0.64 0.00 -0.05
9 0.0910 0.00 0.70 0.00 -1.25
10 0.0912 0.00 1.10 0.00 -1.14
11 0.7460 0.00 -0.64 0.00 -0.07
12 0.7488 0.00 -0.95 0.00 -0.24
13 0.9560 0.00 -0.07 0.00 -0.62
14 0.9562 0.00 0.25 0.00 -0.39
15 1.7890 0.00 0.28 0.00 -0.26
16 1.7918 0.00 0.79 0.00 0.23
17 1.7919 0.00 0.21 0.00 -0.09
18 1.8564 0.00 -1.94 0.00 0.13
19 1.8591 0.00 -1.31 0.00 0.46
20 3.0771 0.00 0.16 0.00 0.70
21 3.0772 0.00 -0.03 0.00 0.56
22 3.0773 0.00 -0.05 0.00 0.49
23 3.0798 0.00 0.20 0.00 0.85
24 3.0800 0.00 -0.82 0.00 0.83
25 3.8720 0.00 -0.67 0.00 -0.13
26 3.8721 0.00 -0.68 0.00 0.84
27 4.0744 0.00 0.32 0.00 0.40
28 4.0745 0.00 0.05 0.00 0.88
29 6.6638 0.00 0.33 0.00 -0.02
30 6.6638 0.00 0.24 0.00 -0.04
31 6.6638 0.00 0.12 0.00 -0.06
32 6.6638 0.00 0.13 0.00 -0.12
33 6.6638 0.00 0.06 0.00 -0.14
34 6.6638 0.00 0.06 0.00 -0.14
35 9.0029 0.00 0.53 0.00 0.21
36 9.0029 0.00 0.29 0.00 0.48
37 9.0030 0.00 0.36 0.00 0.36
38 9.0056 0.00 0.58 0.00 0.51
39 9.1533 0.00 0.32 0.00 0.46
40 9.1534 0.00 0.42 0.00 0.54
41 9.1536 0.00 0.44 0.00 0.78
42 18.0353 0.00 0.11 0.00 -0.03
43 18.0353 0.00 0.01 0.00 -0.16
44 21.1203 0.00 -0.30 0.00 -0.14
45 21.1203 0.00 -0.33 0.00 0.01
46 25.2300 0.00 -0.15 0.00 -0.12
47 25.2301 0.00 -0.55 0.00 -0.12
48 25.2301 0.00 -0.31 0.00 -0.11
49 27.0911 0.00 0.15 0.00 -0.23
50 27.0911 0.00 0.16 0.00 -0.23
51 27.0911 0.00 0.19 0.00 -0.20
52 27.0912 0.00 0.15 0.00 -0.23
53 27.0912 0.00 0.13 0.00 -0.24
54 27.0912 0.00 0.14 0.00 -0.24
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.
612029 quality flag:3 Type: 3:2E 3:2E 3:2E axisobj 39.253 39.253 39.253 ecceobj 0.248 0.248 0.248 incobj 4.827 4.827 4.827 qmin 28.600 28.595 28.604 qmax 50.791 50.749 50.825 amean 39.455 39.455 39.455 amin 39.016 39.012 39.016 amax 39.957 39.949 39.965 emean 0.240 0.240 0.240 emin 0.202 0.201 0.202 emax 0.274 0.274 0.274 imean 6.556 6.550 6.558 imin 3.839 3.837 3.842 imax 9.636 9.631 9.639 excite_mean 0.268 0.268 0.268 fracstop 1.000 1.000 1.000 cjmean 2.969 2.969 2.969 libcent 0 180.1 179.6 179.3 libamp 0 72.2 71.0 71.9 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 134.4 134.3 134.4 kozaiamp 179.9 179.9 180.0