(15094) Polymele
Object
Object |
(15094) Polymele |
Diameter(1) |
21 km |
Dynamic class(1) |
trojan |
Absolute magnitude |
11.76 |
G slop |
0.15 |
Orbital elements
Epoch (Julian date) |
2457274.253817529 |
Semi major axis |
5.161315 ± 0.000000 au |
Eccentricity |
0.094949586 ± 0.000000023 |
Inclination |
12.998738846 ± 0.000002290 ° |
Longitude of ascending node |
50.339857 ± 0.000006 ° |
Argument of perihelia |
5.076132 ± 0.000017 ° |
Mean anomaly |
175.152645 ± 0.000020 ° |
Orbital period |
11.73 yr |
Ephemeris & Observations
Ephemeris version |
NIMAv5 |
Observation file (documentation) |
omc_ast_NIMAv5.txt |
bsp file |
15094_Polymele_nima_v5.bsp |
Date of first observation |
1951-11-30 |
Date of last observation |
2022-12-27 |
Number of observations used in the fit |
1818 |
Number of rejected observations |
7 |
Number of DES observations |
0 |
Number of MPC observations |
1493 |
Number of unpublished observations |
3 |
RMS of observations |
0.125 arcsec |
Residuals
Residuals in right ascension and declination compared to NIMAv5 ephemeris.
Colours indicate the estimated precision in arcsec used as weights in the fitting process.
Orbit quality
date |
σα (arcsec) |
σδ (arcsec) |
2022-01 |
0.012 |
0.007 |
2022-07 |
0.006 |
0.003 |
2023-01 |
0.008 |
0.006 |
2023-07 |
0.007 |
0.005 |
2024-01 |
0.014 |
0.010 |
2024-07 |
0.012 |
0.008 |
2025-01 |
0.018 |
0.012 |
2025-07 |
0.016 |
0.011 |
2026-01 |
0.019 |
0.013 |
Ephemeris comparison
Difference between NIMAv5 and JPL16 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