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67531 (2000 RV92)
Classification: Main-belt Asteroid          SPK-ID: 2067531
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 26 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1507539364861488 3.7819e-08  
a 2.441220474752168 7.9242e-09 au
q 2.073196878352693 9.3961e-08 au
i 3.418386497408409 3.9949e-06 deg
node 307.7693206437327 6.383e-05 deg
peri 230.9995585538309 6.4935e-05 deg
M 301.9767248971282 1.3277e-05 deg
tp 2459425.047730757015
(2021-Jul-29.54773076)
5.1885e-05 TDB
period 1393.185457546235
3.81
6.7834e-06
1.857e-08
d
yr
n .2584006300453742 1.2581e-09 deg/d
Q 2.809244071151642 9.1188e-09 au
  Orbit Determination Parameters
   # obs. used (total)      1404  
   data-arc span      12416 days (33.99 yr)  
   first obs. used      1987-03-22  
   last obs. used      2021-03-19  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .48563  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-May-04 07:04:40  

Additional Information
 Earth MOID = 1.07857 au 
 Jupiter MOID = 2.16545 au 
 T_jup = 3.483 
[ 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 14.78   n/a MPCxxxxx  
diameter diameter 3.134 km 0.165 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.285   0.101 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

67531 (2000 RV92)          Discovered 2000-Sep-03 by LINEAR at Socorro
Reference: 20030910/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 2000 RV92 = 1987 FL1 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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