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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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 21 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1170750849951468 5.121e-08  
a 2.969435418228829 2.3054e-08 au
q 2.62178851425209 1.5038e-07 au
i 10.29621862101938 5.8624e-06 deg
node 13.80255832687949 2.5014e-05 deg
peri 338.65923448943 3.3123e-05 deg
M 73.51464307990078 2.2546e-05 deg
tp 2458218.836520224904
(2018-Apr-10.33652022)
0.00011709 TDB
period 1868.999793275199
5.12
2.1765e-05
5.959e-08
d
yr
n .1926163936964075 2.2431e-09 deg/d
Q 3.317082322205569 2.5753e-08 au
  Orbit Determination Parameters
   # obs. used (total)      781  
   data-arc span      9897 days (27.10 yr)  
   first obs. used      1992-09-02  
   last obs. used      2019-10-08  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .50929  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-07 06:27:44  

Additional Information
 Earth MOID = 1.61938 au 
 Jupiter MOID = 2.13162 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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