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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.


Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 13 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5310226481321192 0.00062224  
a 1.751039039353864 0.0020716 au
q .8211976516934532 0.00011803 au
i 5.970519537533053 0.005417 deg
node 139.1640798449275 0.001077 deg
peri 60.40284214066558 0.00049155 deg
M 87.0010562377698 1.4236 deg
tp 2458795.966620395879
(2019-Nov-08.46662040)		 2.9837 TDB
period 846.3347439857591
2.32		 1.5019
0.004112		 d
yr
n .4253636076720697 0.00075485 deg/d
Q 2.680880427014275 0.0031717 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 = .00258164 au 
 Jupiter MOID = 2.28846 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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