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(2014 BM62)
Classification: Apollo [NEO]          SPK-ID: 3660382
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 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4365418953840745 0.00026487  
a 1.625226193192058 0.00066231 au
q .9157468703881527 5.7325e-05 au
i 1.71348051699771 0.00095007 deg
node 306.2659471649307 0.0074038 deg
peri 225.7497155371235 0.007193 deg
M 4.511841539202829 0.69253 deg
tp 2458991.015368022403
(2020-May-21.51536802)
1.45 TDB
period 756.779129379228
2.07
0.46261
0.001267
d
yr
n .475700222197329 0.00029079 deg/d
Q 2.334705515995962 0.00095144 au
  Orbit Determination Parameters
   # obs. used (total)      23  
   data-arc span      2 days  
   first obs. used      2014-01-31  
   last obs. used      2014-02-02  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .81124  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Aug-10 06:17:41  

Additional Information
 Earth MOID = .00296202 au 
 Jupiter MOID = 2.63709 au 
 T_jup = 4.207 
[ 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 25.3   n/a MPO284140  

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