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46584 (1992 RN6)
Classification: Main-belt Asteroid          SPK-ID: 2046584
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 25 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1173853729418973 4.8693e-08  
a 2.968912682212092 2.2055e-08 au
q 2.620405759778697 1.4064e-07 au
i 10.29691344450659 4.8914e-06 deg
node 13.7852248209233 2.4302e-05 deg
peri 338.640418914361 3.1116e-05 deg
M 150.5790875066465 2.1135e-05 deg
tp 2458218.950077316848
(2018-Apr-10.45007732)
0.00010851 TDB
period 1868.506290114924
5.12
2.0821e-05
5.7e-08
d
yr
n .192667266845464 2.1469e-09 deg/d
Q 3.317419604645487 2.4644e-08 au
  Orbit Determination Parameters
   # obs. used (total)      977  
   data-arc span      10100 days (27.65 yr)  
   first obs. used      1992-09-02  
   last obs. used      2020-04-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .47859  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-May-20 09:33:53  

Additional Information
 Earth MOID = 1.61889 au 
 Jupiter MOID = 2.13486 au 
 T_jup = 3.229 
[ 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 14.3   n/a MPO459173  
diameter diameter 4.853 km 0.578 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.248   0.050 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

46584 (1992 RN6)          Discovered 1992-Sep-02 by Elst, E. W. at La Silla
Reference: 20020921/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1992 RN6 = 2000 DS102 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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