(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 0.023280514 ± 0.000000072
Inclination 18.162468855 ± 0.000004348 °
Longitude of ascending node 342.793766 ± 0.000014 °
Argument of perihelia 185.152880 ± 0.000103 °
Mean anomaly 168.887706 ± 0.000110 °
Orbital period 12.06 yr

Ephemeris & Observations

Ephemeris version NIMAv2
Observation file (documentation) omc_ast_NIMAv2.txt
bsp file 624_Hektor_nima_v2.bsp
Date of first observation 1907-02-11
Date of last observation 2018-12-30
Number of observations used in the fit 1929
Number of rejected observations 999
Number of DES observations 0
Number of MPC observations 2928
Number of unpublished observations 0
RMS of observations 0.640 arcsec

Residuals

residual plot

Residuals in right ascension and declination compared to NIMAv2 ephemeris.
Colours indicate the estimated precision in arcsec used as weights in the fitting process.

Orbit quality

date σα (arcsec) σδ (arcsec)
2018-01 0.016 0.014
2018-07 0.021 0.020
2019-01 0.016 0.015
2019-07 0.019 0.018
2020-01 0.017 0.016
2020-07 0.020 0.017
2021-01 0.021 0.019
2021-07 0.023 0.016
2022-01 0.028 0.021

Ephemeris comparison

residual plot

Difference between NIMAv2 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.