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Table 6

Heliocentric orbital elements of osculating orbits for comets C/1988 B1 Shoemaker and C/2002 J4 NEAT (Sample B, see also Table A.1).

Epoch T0 q0 e0 ω0 Ω0 i0 1 /aori,0 References

Comet C/1988 B1 Shoemaker
elemnom,i 19870326 19870320.107555 5.03070649 1.00248504 124.217043 325.159660 80.585940 20.0 here
δi ±.009206 ±.00007222 ±.00003544 ±.001331 ±.000038 ±.000139 ±7.0
elemcat,i 19870326 19870320.12030 5.0308257 1.0025188 124.21921 325.15976 80.58578 13 MWC 08
Diffi 0.98 1.17 0.67 1.15 1.86 0.81 0.71
Comet C/2002 J4 NEAT
elemnom,i 20031008 20031003.151072 3.63378023 1.00001831 230.705722 70.881227 46.521834 33.9 here
δ i ±.000235 ±.00000105 ±.00000356 ±.000035 ±.000014 ±.000015 ±1.0
elemcat,i 20031008 20031003.15132 3.6337804 1.0000199 230.70575 70.88122 46.52183 35 MPC 75513
Diffi 0.75 0.11 0.45 0.57 0.35 0.19 0.78

Notes. The successive columns signify (2) epoch, i.e. osculation date, (3) perihelion time [TT], (4) perihelion distance, (5) eccentricity, (6) argument of perihelion (in degrees), equinox 2000.0, (7) longitude of the ascending node (in degrees), equinox 2000.0, (8) inclination (in degrees), equinox 2000.0. In the last line we present for each comet the difference between the nominal and catalogue values of a given element divided by the respective combined error, thus Diff.

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