Table 1.
Values of the heliocentric osculating orbital elements of 2024 PT5 and their respective 1σ uncertainties.
| Orbital parameter | Value ± 1σ uncertainty | |
|---|---|---|
| Semimajor axis, a (au) | = | 1.012305060 ± 0.000000009 |
| Eccentricity, e | = | 0.021476703 ± 0.000000006 |
| Inclination, i (°) | = | 1.5205167 ± 0.0000004 |
| Longitude of the ascending node, Ω (°) | = | 305.572360 ± 0.000007 |
| Argument of perihelion, ω (°) | = | 116.24844 ± 0.00003 |
| Mean anomaly, M (°) | = | 323.67725 ± 0.00003 |
| Perihelion distance, q (au) | = | 0.990564084 ± 0.000000005 |
| Aphelion distance, Q (au) | = | 1.034046035 ± 0.000000009 |
| Absolute magnitude, H (mag) | = | 27.4 ± 0.5 |
Notes. The orbital solution of 2024 PT5 is referred to epoch JD 2460600.5 (2024-Oct.-17.0) TDB (Barycentric Dynamical Time, J2000.0 ecliptic and equinox), and is based on 358 observations with an observational timespan of 172 days (solution date 2025-Jan.-20 05:57:37 PST). Source: JPL’s SBDB.
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