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JPL Small-Body Database Browser
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(2016 EV28)
Classification: Apollo [NEO]          SPK-ID: 3745642
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 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .7699747806275834 0.00011191  
a 1.946125597243309 0.0007459 au
q .4476579674321675 4.6241e-05 au
i 1.977461274411237 0.00059795 deg
node 166.1539673994386 0.00017145 deg
peri 106.814201185115 0.0002551 deg
M 39.1238380974625 0.22932 deg
tp 2458492.731043792034
(2019-Jan-09.23104379)
0.56971 TDB
period 991.6415699865622
2.71
0.57011
0.001561
d
yr
n .3630343976048507 0.00020871 deg/d
Q 3.444593227054451 0.0013202 au
  Orbit Determination Parameters
   # obs. used (total)      61  
   data-arc span      1 day  
   first obs. used      2016-03-07  
   last obs. used      2016-03-08  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .34809  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:27:44  

Additional Information
 Earth MOID = .00100939 au 
 Jupiter MOID = 1.7064 au 
 T_jup = 3.454 
[ 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 28.5   n/a MPO370795  

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