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(2016 VU5)
Classification: Apollo [NEO]          SPK-ID: 3763628
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 .3256749907435019 0.00025149  
a 1.42635566347807 0.0005001 au
q .9618272959779079 2.1489e-05 au
i 5.784489567340578 0.0036371 deg
node 230.4719298200992 0.00036698 deg
peri 144.0752153054703 0.002868 deg
M 47.55298247078357 0.40439 deg
tp 2458918.310671350019
(2020-Mar-09.81067135)
0.65571 TDB
period 622.2145652414575
1.70
0.32724
0.0008959
d
yr
n .5785785484791696 0.00030429 deg/d
Q 1.890884030978232 0.00066298 au
  Orbit Determination Parameters
   # obs. used (total)      27  
   data-arc span      11 days  
   first obs. used      2016-11-10  
   last obs. used      2016-11-21  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .69313  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:22:14  

Additional Information
 Earth MOID = .0108278 au 
 Jupiter MOID = 3.58091 au 
 T_jup = 4.633 
[ 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 27.4   n/a MPO394732  

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