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JPL Small-Body Database Browser
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(2012 VU76)
Classification: Apollo [NEO]          SPK-ID: 3617715
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 11 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1283621457006199 1.4493e-06  
a 1.018556407271989 2.4294e-07 au
q .8878123213174423 1.2645e-06 au
i 6.757136569592309 6.0325e-05 deg
node 52.35766938276215 2.4015e-05 deg
peri 88.24472640024966 0.00012041 deg
M 25.62907496545337 0.00084282 deg
tp 2458573.769536763416
(2019-Mar-31.26953676)
0.00086948 TDB
period 375.4707018548889
1.03
0.00013433
3.678e-07
d
yr
n .9587965138732235 3.4303e-07 deg/d
Q 1.149300493226536 2.7412e-07 au
  Orbit Determination Parameters
   # obs. used (total)      47  
   data-arc span      596 days (1.63 yr)  
   first obs. used      2012-11-13  
   last obs. used      2014-07-02  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      2  
   norm. resid. RMS      .34575  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:48:00  

Additional Information
 Earth MOID = .00346739 au 
 Jupiter MOID = 3.84864 au 
 T_jup = 5.980 
[ 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 25.7   n/a MPO244152  

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