(617) Patroclus
Object
Object |
(617) Patroclus |
Diameter(1) |
140 km |
Dynamic class(1) |
trojan |
Absolute magnitude |
8.23 |
G slop |
0.15 |
Orbital elements
Epoch (Julian date) |
2459800.5 |
Semi major axis |
5.210104 ± 0.000000 au |
Eccentricity |
0.139867900 ± 0.000000054 |
Inclination |
22.062062404 ± 0.000005440 ° |
Longitude of ascending node |
44.358470 ± 0.000014 ° |
Argument of perihelia |
308.184386 ± 0.000026 ° |
Mean anomaly |
303.031905 ± 0.000026 ° |
Orbital period |
11.89 yr |
Ephemeris & Observations
Ephemeris version |
NIMAv6 |
Observation file (documentation) |
omc_ast_NIMAv6.txt |
bsp file |
617_Patroclus_nima_v6.bsp |
Date of first observation |
1906-10-17 |
Date of last observation |
2023-07-01 |
Number of observations used in the fit |
5134 |
Number of rejected observations |
27 |
Number of DES observations |
0 |
Number of MPC observations |
5161 |
Number of unpublished observations |
0 |
RMS of observations |
1.531 arcsec |
Residuals
Residuals in right ascension and declination compared to NIMAv6 ephemeris.
Colours indicate the estimated precision in arcsec used as weights in the fitting process.
Orbit quality
date |
σα (arcsec) |
σδ (arcsec) |
2023-01 |
0.034 |
0.017 |
2023-07 |
0.051 |
0.033 |
2024-01 |
0.040 |
0.025 |
2024-07 |
0.045 |
0.041 |
2025-01 |
0.044 |
0.039 |
2025-07 |
0.040 |
0.035 |
2026-01 |
0.048 |
0.044 |
2026-07 |
0.039 |
0.025 |
2027-01 |
0.053 |
0.032 |
Ephemeris comparison
Difference between NIMAv6 and JPL82 in right ascension (weighted by cos δ) and in declination.
Gray area represents the 1-σ uncertainty of NIMA ephemeris. Green dots represent the DES observations.
Previous NIMA versions