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(2013 BO76)
Classification: Apollo [NEO, PHA]          SPK-ID: 3626394
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

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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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 51 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5198870658697985 3.1451e-07  
a 1.702794883301041 8.9048e-07 au
q .8175338476435567 1.1444e-07 au
i 1.939650386320214 2.6373e-06 deg
node 242.6308131830211 0.00027481 deg
peri 4.471911679004408 0.00027352 deg
M 46.6388865535225 0.00089371 deg
tp 2458895.355247155827
(2020-Feb-15.85524716)
0.0019323 TDB
period 811.599800532618
2.22
0.00063664
1.743e-06
d
yr
n .4435683692427567 3.4795e-07 deg/d
Q 2.588055918958525 1.3534e-06 au
  Orbit Determination Parameters
   # obs. used (total)      281  
   data-arc span      717 days (1.96 yr)  
   first obs. used      2013-01-10  
   last obs. used      2014-12-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      2  
   norm. resid. RMS      .4256  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:46:58  

Additional Information
 Earth MOID = .0283976 au 
 Jupiter MOID = 2.45553 au 
 T_jup = 4.033 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 20.4   n/a E2013S24  
rotation period rot_per 5.03 h n/a LCDB (Rev. 2019-August); Warner et al., 2009 Result based on less than full coverage, so that the period may be wrong by 30 percent or so.
Published Reference List:
[Thirouin, A.; Moskovitz, N.; Binzel, R.P.; Christensen, E.; et al. (2016) Astron. J. 152, A163.]

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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