(624) Hektor


This object has a more recent orbit available here

Object

Object (624) Hektor
Diameter(1) 225 km
Dynamic class(1) trojan
Absolute magnitude 7.30
G slop 0.15
(1) Data from the johnston archive list.

Orbital elements

Epoch (Julian date) 2458600.5
Semi major axis 5.259580 ± 0.000000 au
Eccentricity 0.023280446 ± 0.000000044
Inclination 18.162467398 ± 0.000003875 °
Longitude of ascending node 342.793770 ± 0.000008 °
Argument of perihelia 185.152968 ± 0.000076 °
Mean anomaly 168.887621 ± 0.000079 °
Orbital period 12.06 yr

Ephemeris & Observations

Ephemeris version NIMAv6
Observation file (documentation) omc_ast_NIMAv6.txt
bsp file 624_Hektor_nima_v6.bsp
Date of first observation 1907-02-11
Date of last observation 2022-07-14
Number of observations used in the fit 3618
Number of rejected observations 40
Number of DES observations 0
Number of MPC observations 3650
Number of unpublished observations 8
RMS of observations 6.355 arcsec

Residuals

residual plot

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)
2022-01 0.014 0.014
2022-07 0.014 0.012
2023-01 0.021 0.017
2023-07 0.017 0.013
2024-01 0.026 0.020
2024-07 0.019 0.014
2025-01 0.028 0.024
2025-07 0.022 0.019
2026-01 0.029 0.025

Ephemeris comparison

residual plot

Difference between NIMAv6 and JPL89 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.