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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.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 42 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3833975854314671 1.0638e-06  
a 1.49501585646708 2.2713e-06 au
q .921830386915845 2.1304e-07 au
i .5630689101745775 4.7089e-06 deg
node 177.9121306057908 0.00038152 deg
peri 8.579794244436162 0.00037389 deg
M 86.21331634023575 0.0034652 deg
tp 2459040.603493285509
(2020-Jul-10.10349329)
0.0060623 TDB
period 667.6780903549594
1.83
0.0015216
4.166e-06
d
yr
n .5391819878477849 1.2288e-06 deg/d
Q 2.068201326018316 3.1422e-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.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      3  
   norm. resid. RMS      .29566  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 07:34:38  

Additional Information
 Earth MOID = .00515375 au 
 Jupiter MOID = 2.88737 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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