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469630 (2004 RV305)
Classification: Main-belt Asteroid          SPK-ID: 2469630
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3070096876376003 3.4113e-07  
a 2.535835450301521 3.3436e-08 au
q 1.757309400804097 8.8606e-07 au
i 4.164769637600902 5.0668e-06 deg
node 60.74439072298587 0.00015757 deg
peri 261.0148837832672 0.00016044 deg
M 341.532106546159 1.7505e-05 deg
tp 2459076.164974445027
(2020-Aug-14.66497445)
7.2845e-05 TDB
period 1474.959278289768
4.04
2.9172e-05
7.987e-08
d
yr
n .2440745350050777 4.8273e-09 deg/d
Q 3.314361499798944 4.3701e-08 au
  Orbit Determination Parameters
   # obs. used (total)      178  
   data-arc span      6322 days (17.31 yr)  
   first obs. used      2000-09-24  
   last obs. used      2018-01-15  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .61555  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-13 19:05:05  

Additional Information
 Earth MOID = .75082 au 
 Jupiter MOID = 2.04082 au 
 T_jup = 3.377 
[ 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 17.3   n/a MPO434689  
diameter diameter 2.283 km 0.462 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2017AJ....154..168M)  
geometric albedo albedo 0.037   0.019 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2017AJ....154..168M)  

469630 (2004 RV305)          Discovered 2004-Sep-12 by LINEAR at Socorro
Reference: Last Updated: 2016-08-22

Alternate Designations
 2004 RV305 = 2000 TY34 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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