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JPL Small-Body Database Browser
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(2015 BF92)
Classification: Apollo [NEO]          SPK-ID: 3704768
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 13 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5309838078222733 0.00062481  
a 1.751191041337488 0.0020678 au
q .8213369539838569 0.00012431 au
i 5.96978714308758 0.0054217 deg
node 139.1677823197954 0.0011797 deg
peri 60.40810170139389 0.00020223 deg
M 276.8707726384724 1.1216 deg
tp 2458795.956429187205
(2019-Nov-08.45642919)
2.9834 TDB
period 846.444947712319
2.32
1.4992
0.004105
d
yr
n .4253082270417816 0.00075332 deg/d
Q 2.68104512869112 0.0031658 au
  Orbit Determination Parameters
   # obs. used (total)      40  
   data-arc span      18 days  
   first obs. used      2015-01-19  
   last obs. used      2015-02-06  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .32993  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:36:12  

Additional Information
 Earth MOID = .00278604 au 
 Jupiter MOID = 2.28939 au 
 T_jup = 3.949 
[ 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 24.0   n/a MPCxxxxx  

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