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JPL Small-Body Database Browser
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(2014 BP8)
Classification: Apollo [NEO]          SPK-ID: 3656923
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2363180160537878 0.00015847  
a 1.193025025442269 0.00020801 au
q .9110917183272321 3.0214e-05 au
i 13.44327349811487 0.0073484 deg
node 304.3330584305637 5.2658e-05 deg
peri 236.6262682343959 0.0036703 deg
M 334.5919260047174 0.36635 deg
tp 2458634.092474968919
(2019-May-30.59247497)
0.49315 TDB
period 475.962522427165
1.30
0.12448
0.0003408
d
yr
n .756362072719895 0.00019781 deg/d
Q 1.474958332557305 0.00025716 au
  Orbit Determination Parameters
   # obs. used (total)      51  
   data-arc span      4 days  
   first obs. used      2014-01-23  
   last obs. used      2014-01-27  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .62286  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:42:47  

Additional Information
 Earth MOID = .0100651 au 
 Jupiter MOID = 3.53525 au 
 T_jup = 5.267 
[ 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 27.3   n/a E2014B58  

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