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(2015 VU64)
Classification: Aten [NEO]          SPK-ID: 3733862
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 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1080104860282808 1.8718e-05  
a .9348575379049574 7.7562e-06 au
q .833883120868641 2.4411e-05 au
i 2.483961550600128 0.00036162 deg
node 224.5283879418883 0.00016087 deg
peri 49.78821051700524 0.00038833 deg
M 137.1739864961001 0.020436 deg
tp 2458874.698494784952
(2020-Jan-26.19849478)
0.017177 TDB
period 330.1540112250439
0.90
0.0041087
1.125e-05
d
yr
n 1.090400200391968 1.357e-05 deg/d
Q 1.035831954941274 8.5939e-06 au
  Orbit Determination Parameters
   # obs. used (total)      30  
   data-arc span      2 days  
   first obs. used      2015-11-08  
   last obs. used      2015-11-10  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .42701  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:30:50  

Additional Information
 Earth MOID = .00107975 au 
 Jupiter MOID = 3.99067 au 
 T_jup = 6.408 
[ 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 30.6   n/a MPO355052  

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