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(2014 ME6)
Classification: Apollo [NEO]          SPK-ID: 3673920
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 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5327962807639081 0.00051886  
a 1.382633531590651 0.0010039 au
q .6459715282996848 0.00024877 au
i 4.038033189469497 0.0043296 deg
node 268.8868628658323 0.0016744 deg
peri 98.28298422229589 0.0020675 deg
M 198.3741303746717 1.4014 deg
tp 2459267.104471087339
(2021-Feb-21.60447109)
2.602 TDB
period 593.8257892374027
1.63
0.64675
0.001771
d
yr
n .6062384061532858 0.00066027 deg/d
Q 2.119295534881617 0.0015388 au
  Orbit Determination Parameters
   # obs. used (total)      32  
   data-arc span      2 days  
   first obs. used      2014-06-23  
   last obs. used      2014-06-25  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .52056  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:39:59  

Additional Information
 Earth MOID = .00677713 au 
 Jupiter MOID = 3.35686 au 
 T_jup = 4.634 
[ 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 25.6   n/a MPO303422  

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