C/1999 J2 LINEAR
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C/1999 J2 was discovered by B. Skiff of Lowell Observatory Near-Earth Object Search (LONEOS) team on 13 May 1999, 0.92 yr before perihelion passage.
This comet made its closest approach to the Earth on 11 May 2000 (6.515 au), about one month after perihelion.
Solution given here is based on data spanning over 4.1 yr in a range of heliocentric distances: 7.42 au – 7.110 au (perihelion) – 10.1 au.
This Oort spike comet suffers small planetary perturbations during its passage through the planetary system that lead to escape of the comet from the solar system on hiperbolic orbit (see future barycentric orbit).
See also Królikowska 2014 and Królikowska and Dybczyński 2017.
This comet made its closest approach to the Earth on 11 May 2000 (6.515 au), about one month after perihelion.
Solution given here is based on data spanning over 4.1 yr in a range of heliocentric distances: 7.42 au – 7.110 au (perihelion) – 10.1 au.
This Oort spike comet suffers small planetary perturbations during its passage through the planetary system that lead to escape of the comet from the solar system on hiperbolic orbit (see future barycentric orbit).
See also Królikowska 2014 and Królikowska and Dybczyński 2017.
solution description | ||
---|---|---|
number of observations | 1001 | |
data interval | 1999 05 12 – 2003 05 29 | |
data type | perihelion within the observation arc (FULL) | |
data arc selection | entire data set (STD) | |
range of heliocentric distances | 7.42 au – 7.11 au (perihelion) – 10.1 au | |
detectability of NG effects in the comet's motion | NG effects not determinable | |
type of model of motion | GR - gravitational orbit | |
data weighting | YES | |
number of residuals | 1974 | |
RMS [arcseconds] | 0.53 | |
orbit quality class | 1a+ |
next orbit statistics, both Galactic and stellar perturbations were taken into account | ||
---|---|---|
no. of returning VCs in the swarm | 0 | |
no. of escaping VCs in the swarm | 5001 | |
no. of hyperbolas among escaping VCs in the swarm | 5001 | * |
next reciprocal semi-major axis [10-6 au-1] | -86.88 – -86.04 – -85.26 | |
next perihelion distance [au] | 331.4 – 332.8 – 334.3 | |
synchronous stop epoch [Myr] | 1.61 | S |
percentage of VCs with qnext > 20 | 100 |
next orbit statistics, here only the Galactic tide has been included | ||
---|---|---|
no. of returning VCs in the swarm | 0 | |
no. of escaping VCs in the swarm | 5001 | |
no. of hyperbolas among escaping VCs in the swarm | 5001 | * |
next reciprocal semi-major axis [10-6 au-1] | -86.57 – -85.73 – -84.95 | |
next perihelion distance [au] | 13.51 – 13.57 – 13.64 | |
synchronous stop epoch [Myr] | 1.63 | S |
percentage of VCs with 10 < qnext < 20 | 100 |