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(2015 VO64)
Classification: Apollo [NEO]          SPK-ID: 3733857
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

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 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2442697913938872 9.6382e-05  
a 1.331983561669086 0.00017584 au
q 1.006620214920091 4.5067e-06 au
i 18.26157921032087 0.0044035 deg
node 44.08869868511201 8.1407e-05 deg
peri 4.323130489326686 0.0016995 deg
M 346.3191052621131 0.21134 deg
tp 2459021.838246372579
(2020-Jun-21.33824637)		 0.33385 TDB
period 561.4960747307766
1.54		 0.11119
0.0003044		 d
yr
n .6411442861334534 0.00012696 deg/d
Q 1.65734690841808 0.00021879 au
   Orbit Determination Parameters
   # obs. used (total)      89  
   data-arc span      4 days  
   first obs. used      2015-11-06  
   last obs. used      2015-11-10  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .4544  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-17 06:10:56  

Additional Information
 Earth MOID = .0165817 au 
 Jupiter MOID = 3.73268 au 
 T_jup = 4.838 
[ 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 26.3   n/a MPO361299  

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