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(2014 OG1)
Classification: Apollo [NEO]          SPK-ID: 3674864
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 16 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6862242719818622 6.4567e-05  
a 1.342512490463086 0.000189 au
q .4212478340684981 2.7386e-05 au
i 17.92121129840221 0.0028219 deg
node 297.9711660441388 0.00056448 deg
peri 129.1662433206007 0.0013329 deg
M 235.9458553591639 0.27733 deg
tp 2459196.287385596917
(2020-Dec-12.78738560)
0.47904 TDB
period 568.166900178589
1.56
0.11998
0.0003285
d
yr
n .6336166360392396 0.0001338 deg/d
Q 2.263777146857674 0.00031869 au
  Orbit Determination Parameters
   # obs. used (total)      147  
   data-arc span      27 days  
   first obs. used      2014-07-07  
   last obs. used      2014-08-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .404  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:39:36  

Additional Information
 Earth MOID = .0685087 au 
 Jupiter MOID = 3.17246 au 
 T_jup = 4.579 
[ 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 21.6   n/a MPCxxxxx  

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