(83982) Crantor


This object has a more recent orbit available here

Object

Object (83982) Crantor
Diameter(1) 59 km
Dynamic class(1) Centaur
Absolute magnitude 8.80
G slop 0.15
(1) Data from the johnston archive list.

Orbital elements

Epoch (Julian date) 2458600.5
Semi major axis 19.502601 ± 0.000121 au
Eccentricity 0.277353869 ± 0.000002756
Inclination 12.755246498 ± 0.000045782 °
Longitude of ascending node 117.381951 ± 0.000089 °
Argument of perihelia 93.762251 ± 0.000802 °
Mean anomaly 70.311397 ± 0.001041 °
Orbital period 86.13 yr

Ephemeris & Observations

Ephemeris version NIMAv4
Observation file (documentation) omc_ast_NIMAv4.txt
bsp file 83982_Crantor_nima_v4.bsp
Date of first observation 2001-03-19
Date of last observation 2020-08-15
Number of observations used in the fit 311
Number of rejected observations 3
Number of DES observations 0
Number of MPC observations 296
Number of unpublished observations 18
RMS of observations 0.225 arcsec

Residuals

residual plot

Residuals in right ascension and declination compared to NIMAv4 ephemeris.
Colours indicate the estimated precision in arcsec used as weights in the fitting process.

Orbit quality

date σα (arcsec) σδ (arcsec)
2020-01 0.062 0.040
2020-07 0.092 0.046
2021-01 0.079 0.043
2021-07 0.119 0.051
2022-01 0.102 0.047
2022-07 0.150 0.057
2023-01 0.129 0.051
2023-07 0.185 0.064
2024-01 0.160 0.057

Ephemeris comparison

residual plot

Difference between NIMAv4 and JPL20 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.