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24755 (1992 UQ6)
Classification: Main-belt Asteroid          SPK-ID: 2024755
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 33 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1784908399614281 3.711e-08  
a 2.297100857688365 8.2484e-09 au
q 1.887089396123452 8.4593e-08 au
i 6.459181278993309 5.4278e-06 deg
node 334.8044794133028 3.5756e-05 deg
peri 56.81750515986697 3.9025e-05 deg
M 95.28668246031249 1.4813e-05 deg
tp 2459059.912309852549
(2020-Jul-29.41230985)
5.2133e-05 TDB
period 1271.652714990376
3.48
6.8494e-06
1.875e-08
d
yr
n .2830961596324862 1.5248e-09 deg/d
Q 2.707112319253278 9.7207e-09 au
  Orbit Determination Parameters
   # obs. used (total)      1514  
   data-arc span      24200 days (66.26 yr)  
   first obs. used      1955-02-24  
   last obs. used      2021-05-28  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .5026  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Jul-08 05:29:00  

Additional Information
 Earth MOID = .90039 au 
 Jupiter MOID = 2.7703 au 
 T_jup = 3.564 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 14.48   n/a E2021B10  
rotation period rot_per 3.72 h n/a LCDB (Rev. 2020-October); Warner et al., 2009 lower-limit; Incomplete or inconclusive result.
Published Reference List:
[Erasmus, N.; McNeill, A.; Mommert, N.; Trilling, D.E.; et al. (2019) Ap. J. Suppl. Series 242, A15.]

24755 (1992 UQ6)          Discovered 1992-Oct-28 by Ueda, S., Kaneda, H. at Kushiro
Reference: 20010606/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1992 UQ6 = 1999 XG181 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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