(1172) Aneas
Object
Object |
(1172) Aneas |
Diameter(1) |
118 km |
Dynamic class(1) |
trojan |
Absolute magnitude |
8.30 |
G slop |
0.15 |
Orbital elements
Epoch (Julian date) |
2460600.5 |
Semi major axis |
5.235559 ± 0.000000 au |
Eccentricity |
0.106341541 ± 0.000000035 |
Inclination |
16.655892154 ± 0.000004406 ° |
Longitude of ascending node |
247.254143 ± 0.000008 ° |
Argument of perihelia |
52.162951 ± 0.000024 ° |
Mean anomaly |
75.669860 ± 0.000018 ° |
Orbital period |
11.98 yr |
Ephemeris & Observations
Ephemeris version |
NIMAv8 |
Observation file (documentation) |
omc_ast_NIMAv8.txt |
bsp file |
1172_Aneas_nima_v8.bsp |
Date of first observation |
1930-10-17 |
Date of last observation |
2024-07-13 |
Number of observations used in the fit |
4929 |
Number of rejected observations |
43 |
Number of DES observations |
0 |
Number of MPC observations |
4943 |
Number of unpublished observations |
29 |
RMS of observations |
2.991 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 |
0.024 |
0.017 |
2024-07 |
0.030 |
0.015 |
2025-01 |
0.034 |
0.015 |
2025-07 |
0.032 |
0.010 |
2026-01 |
0.042 |
0.011 |
2026-07 |
0.031 |
0.009 |
2027-01 |
0.043 |
0.013 |
2027-07 |
0.030 |
0.012 |
2028-01 |
0.040 |
0.019 |
Ephemeris comparison
Difference between NIMAv8 and JPL115 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