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JPL Small-Body Database Browser
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80655 (2000 BO3)
Classification: Main-belt Asteroid          SPK-ID: 2080655
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 25 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1184079078701584 6.9131e-08  
a 2.288559217970094 9.5213e-09 au
q 2.017575708933289 1.6095e-07 au
i 7.281370608253922 7.128e-06 deg
node 20.25840868475501 3.1588e-05 deg
peri 352.8310693444976 3.6808e-05 deg
M 305.5844819551417 1.7231e-05 deg
tp 2458791.644552773226
(2019-Nov-04.14455277)
6.031e-05 TDB
period 1264.566459546244
3.46
7.8916e-06
2.161e-08
d
yr
n .2846825465615911 1.7766e-09 deg/d
Q 2.559542727006898 1.0649e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1001  
   data-arc span      8801 days (24.10 yr)  
   first obs. used      1995-10-25  
   last obs. used      2019-11-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .52728  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Dec-14 07:47:13  

Additional Information
 Earth MOID = 1.01759 au 
 Jupiter MOID = 2.90027 au 
 T_jup = 3.580 
[ 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 15.2   n/a MPO502641  
diameter diameter 1.934 km 0.086 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.472   0.059 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

80655 (2000 BO3)          Discovered 2000-Jan-27 by Kobayashi, T. at Oizumi
Reference: 20040504/Numbers.arcLast Updated: 2004-07-16

Alternate Designations
 2000 BO3 = 2002 RV24 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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