(15094) Polymele
Object
Object |
(15094) Polymele |
Diameter(1) |
21 km |
Dynamic class(1) |
trojan |
Absolute magnitude |
11.83 |
G slop |
0.15 |
Orbital elements
Epoch (Julian date) |
2460800.5 |
Semi major axis |
5.188279 ± 0.000000 au |
Eccentricity |
0.096524495 ± 0.000000023 |
Inclination |
12.980176360 ± 0.000002254 ° |
Longitude of ascending node |
50.321431 ± 0.000006 ° |
Argument of perihelia |
5.662379 ± 0.000016 ° |
Mean anomaly |
110.264326 ± 0.000013 ° |
Orbital period |
11.82 yr |
Ephemeris & Observations
Ephemeris version |
NIMAv8 |
Observation file (documentation) |
omc_ast_NIMAv8.txt |
bsp file |
15094_Polymele_nima_v8.bsp |
Date of first observation |
1951-11-30 |
Date of last observation |
2025-05-28 |
Number of observations used in the fit |
2365 |
Number of rejected observations |
7 |
Number of DES observations |
0 |
Number of MPC observations |
2040 |
Number of unpublished observations |
3 |
RMS of observations |
0.125 arcsec |
Residuals
Residuals in right ascension and declination compared to NIMAv8 ephemeris.
Colours indicate the estimated precision in arcsec used as weights in the fitting process.
Orbit quality
date |
σα (arcsec) |
σδ (arcsec) |
2024-01 |
0.014 |
0.009 |
2024-07 |
0.012 |
0.008 |
2025-01 |
0.017 |
0.012 |
2025-07 |
0.016 |
0.011 |
2026-01 |
0.018 |
0.013 |
2026-07 |
0.019 |
0.013 |
2027-01 |
0.019 |
0.011 |
2027-07 |
0.023 |
0.014 |
2028-01 |
0.020 |
0.008 |
Ephemeris comparison
Difference between NIMAv8 and JPL21 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