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(2015 VP64)
Classification: Apollo [NEO]          SPK-ID: 3733856
[ 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 2457334.5 (2015-Nov-08.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6987215188783361 0.00065838  
a 2.090654779162269 0.0038853 au
q .629869296415756 0.00020596 au
i .7151404754393659 0.0006253 deg
node 44.12536232042804 0.00013633 deg
peri 274.8979560313128 0.0013855 deg
M 15.68177119839518 0.050045 deg
tp 2457286.403383299097
(2015-Sep-20.90338330)		 0.019426 TDB
period 1104.134334908356
3.02		 3.0779
0.008427		 d
yr
n .326047283032712 0.0009089 deg/d
Q 3.551440261908782 0.0066001 au
   Orbit Determination Parameters
   # obs. used (total)      30  
   data-arc span      2 days  
   first obs. used      2015-11-07  
   last obs. used      2015-11-09  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .42744  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:30:52  

Additional Information
 Earth MOID = .000319343 au 
 Jupiter MOID = 1.78201 au 
 T_jup = 3.396 
[ 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 28.3   n/a MPO361299  

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