(624) Hektor


This object has a more recent orbit available here

Object

Object (624) Hektor
Diameter(1) 225 km
Dynamic class(1) trojans
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 0.023280476 ± 0.000000030
Inclination 18.162464546 ± 0.000001286 °
Longitude of ascending node 342.793766 ± 0.000007 °
Argument of perihelia 185.152932 ± 0.000047 °
Mean anomaly 168.887655 ± 0.000041 °
Orbital period 12.06 yr

Ephemeris & Observations

Ephemeris version NIMAv3
Observation file (documentation) omc_ast_NIMAv3.txt
bsp file 624_Hektor_nima_v3.bsp
Date of first observation 1907-02-11
Date of last observation 2019-05-09
Number of observations used in the fit 2165
Number of rejected observations 70
Number of DES observations 0
Number of MPC observations 1999
Number of unpublished observations 4
RMS of observations 0.116 arcsec

Residuals

residual plot

Residuals in right ascension and declination compared to NIMAv3 ephemeris.
Colours indicate the estimated precision in arcsec used as weights in the fitting process.

Orbit quality

date σα (arcsec) σδ (arcsec)
2019-01 0.011 0.008
2019-07 0.016 0.014
2020-01 0.014 0.013
2020-07 0.019 0.015
2021-01 0.020 0.017
2021-07 0.023 0.011
2022-01 0.028 0.016
2022-07 0.026 0.004
2023-01 0.037 0.004

Ephemeris comparison

residual plot

Difference between NIMAv3 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.