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52318 (1992 BC3)
Classification: Main-belt Asteroid          SPK-ID: 2052318
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 19 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1869525009328971 6.2227e-08  
a 2.434667061104713 1.195e-08 au
q 1.97949996509224 1.4851e-07 au
i 10.36038956621594 6.3929e-06 deg
node 312.3400278375135 2.4696e-05 deg
peri 212.4925457353897 2.7769e-05 deg
M 33.23864077357582 1.1573e-05 deg
tp 2458472.385421454419
(2018-Dec-19.88542145)
4.4387e-05 TDB
period 1387.57925122723
3.80
1.0216e-05
2.797e-08
d
yr
n .2594446405000663 1.9102e-09 deg/d
Q 2.889834157117185 1.4185e-08 au
  Orbit Determination Parameters
   # obs. used (total)      717  
   data-arc span      10432 days (28.56 yr)  
   first obs. used      1990-10-17  
   last obs. used      2019-05-10  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .57818  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-May-30 04:46:57  

Additional Information
 Earth MOID = .99686 au 
 Jupiter MOID = 2.13994 au 
 T_jup = 3.459 
[ 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 15.4   n/a MPO324779  
diameter diameter 3.713 km 1.063 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2016AJ....152...63N)  
geometric albedo albedo 0.072   0.059 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2015ApJ...814..117N)  

52318 (1992 BC3)          Discovered 1992-Jan-26 by Spacewatch at Kitt Peak
Reference: 20030216/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1992 BC3 = 2000 JV63 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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