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JPL Small-Body Database Browser
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(2019 VV)
Classification: Aten [NEO]          SPK-ID: 3892280
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 14 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2954185259970022 1.4003e-05  
a .9408351408315994 5.5721e-07 au
q .6628950103209463 1.2782e-05 au
i .3055396457982688 1.3221e-05 deg
node 255.604815622756 0.00032716 deg
peri 26.43657383495082 0.0004435 deg
M 240.7710212049386 0.0012763 deg
tp 2458710.894654764266
(2019-Aug-15.39465476)
0.0012798 TDB
period 333.3256404338347
0.91
0.00029612
8.107e-07
d
yr
n 1.080024925569625 9.5947e-07 deg/d
Q 1.218775271342252 7.2182e-07 au
  Orbit Determination Parameters
   # obs. used (total)      98  
   data-arc span      3215 days (8.80 yr)  
   first obs. used      2011-01-30  
   last obs. used      2019-11-19  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      3  
   norm. resid. RMS      .53285  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-19 08:12:17  

Additional Information
 Earth MOID = .00317641 au 
 Jupiter MOID = 3.90079 au 
 T_jup = 6.343 
[ 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 25.314   .48288 14 autocmod 2.8

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