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JPL Small-Body Database Browser
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(2015 VO64)
Classification: Apollo [NEO]          SPK-ID: 3733857
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2444350467486802 9.6601e-05  
a 1.331962397925078 0.00017581 au
q 1.006384106920777 4.1713e-06 au
i 18.26411188171321 0.0044057 deg
node 44.0954894872531 9.016e-05 deg
peri 4.295325461791416 0.0016457 deg
M 89.89831858311132 0.16064 deg
tp 2458460.287916762637
(2018-Dec-07.78791676)
0.22278 TDB
period 561.4826924575352
1.54
0.11117
0.0003044
d
yr
n .6411595670461858 0.00012695 deg/d
Q 1.657540688929378 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 = .0158313 au 
 Jupiter MOID = 3.7315 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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