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65767 (1995 BZ11)
Classification: Main-belt Asteroid          SPK-ID: 2065767
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 19 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1780106317801383 4.2774e-08  
a 2.281785480815004 1.002e-08 au
q 1.875603405788379 9.7937e-08 au
i 4.184447754363938 4.1876e-06 deg
node 124.3586826168869 5.5676e-05 deg
peri 213.4895325589242 5.669e-05 deg
M 291.2298242313992 9.437e-06 deg
tp 2459240.996233425136
(2021-Jan-26.49623343)
3.3031e-05 TDB
period 1258.9562708749
3.45
8.2923e-06
2.27e-08
d
yr
n .2859511551976474 1.8835e-09 deg/d
Q 2.687967555841629 1.1803e-08 au
  Orbit Determination Parameters
   # obs. used (total)      853  
   data-arc span      9128 days (24.99 yr)  
   first obs. used      1995-01-29  
   last obs. used      2020-01-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .55809  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-23 14:45:40  

Additional Information
 Earth MOID = .867854 au 
 Jupiter MOID = 2.68684 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 16.1   n/a MPO468581  
diameter diameter 1.454 km 0.235 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.277   0.049 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

65767 (1995 BZ11)          Discovered 1995-Jan-29 by Spacewatch at Kitt Peak
Reference: 20030910/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1995 BZ11 = 2000 RN67 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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