Open Access
Table 3
Orbital elements of 2021 GM1.
| Six-parameter solution | Unit | |
|---|---|---|
| Semi-major axis (a) | 0.968020575 ± 1.43 × 10−8 | au |
| Eccentricity (e) | 0.041997691 ± 1.58 × 10−8 | / |
| Inclination (i) | 1.598736270 ± 4.09 × 10−7 | deg |
| Long. of Asc. Node (Ω) | 193.321099298 ± 1.95 × 10−6 | deg |
| Argument of Perihelion (ω) | 207.383938594 ± 8.52 × 10−6 | deg |
| Mean anomaly (M) | 162.303893236 ± 1.00 × 10−5 | deg |
| Normalized residuals rms | 0.776 | / |
| Seven-parameter solution | ||
| Semi-major axis (a) | 0.968020505 ± 1.38 × 10−8 | au |
| Eccentricity (e) | 0.041997755 ± 1.49 × 10−8 | / |
| Inclination (i) | 1.598740133 ± 5.18 × 10−7 | deg |
| Long. of Asc. Node (Ω) | 193.321107921 ± 2.15 × 10−6 | deg |
| Argument of Perihelion (ω) | 207.383858669 ± 1.14 × 10−5 | deg |
| Mean anomaly (M) | 162.303967843 ± 1.23 × 10−5 | deg |
| Area-to-mass (A/m) | 0.2564 ± 0.0257 | m2 t−1 |
| Normalized residuals rms | 0.622 | / |
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