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(2013 BV15)
Classification: Apollo [NEO]          SPK-ID: 3624597
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 41 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3833584986964566 1.0719e-06  
a 1.494950081420097 2.2738e-06 au
q .9218482625807433 2.2275e-07 au
i .5629844890543262 4.77e-06 deg
node 177.9246760161642 0.00038636 deg
peri 8.558672374989113 0.00037843 deg
M 338.382896074382 0.0032224 deg
tp 2459040.589761568800
(2020-Jul-10.08976157)
0.0060675 TDB
period 667.6340278710782
1.83
0.0015232
4.17e-06
d
yr
n .5392175727590639 1.2302e-06 deg/d
Q 2.068051900259451 3.1455e-06 au
  Orbit Determination Parameters
   # obs. used (total)      149  
   # delay obs. used      3  
   # Doppler obs. used      4  
   data-arc span      26 days  
   first obs. used      2013-01-17  
   last obs. used      2013-02-12  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      3  
   norm. resid. RMS      .29707  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:47:09  

Additional Information
 Earth MOID = .00512528 au 
 Jupiter MOID = 2.88858 au 
 T_jup = 4.471 
[ 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 24.3   n/a MPO254838  

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