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JPL Small-Body Database Browser
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447406 (2006 BV161)
Classification: Main-belt Asteroid          SPK-ID: 2447406
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

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For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer was implemented using two-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances.


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Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1691272718121986 7.6487e-08  
a 2.352831522717603 1.9456e-08 au
q 1.954903546246634 1.8581e-07 au
i 2.819938402045089 7.2101e-06 deg
node 43.75395275931418 0.00012634 deg
peri 129.0679299017208 0.00012722 deg
M 211.0773360296575 1.5059e-05 deg
tp 2459145.809379400606
(2020-Oct-23.30937940)
5.7416e-05 TDB
period 1318.210212941886
3.61
1.6351e-05
4.477e-08
d
yr
n .2730975655214946 3.3874e-09 deg/d
Q 2.750759499188572 2.2746e-08 au
  Orbit Determination Parameters
   # obs. used (total)      157  
   data-arc span      5052 days (13.83 yr)  
   first obs. used      2006-01-26  
   last obs. used      2019-11-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .60151  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Dec-05 02:20:24  

Additional Information
 Earth MOID = .961966 au 
 Jupiter MOID = 2.21549 au 
 T_jup = 3.535 
[ 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 17.6   n/a MPO456119  

447406 (2006 BV161)          Discovered 2006-Jan-26 by CSS at Catalina
Reference: Last Updated: 2015-10-28

Alternate Designations
 2006 BV161 = 2008 UO134 = 2008 VB64 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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