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(2014 OV299)
Classification: Apollo [NEO]          SPK-ID: 3678015
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 2456868.5 (2014-Jul-30.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5503619952285429 0.0021104  
a 1.915451177565277 0.0082805 au
q .8612596457175893 0.00031926 au
i 7.348441884171484 0.022135 deg
node 128.3239119108047 0.0013106 deg
peri 243.3071069119345 0.0084282 deg
M 341.619965921308 0.13676 deg
tp 2456917.936631204059
(2014-Sep-17.43663120)
0.047279 TDB
period 968.289131416438
2.65
6.2789
0.01719
d
yr
n .3717897767512715 0.0024109 deg/d
Q 2.969642709412965 0.012838 au
  Orbit Determination Parameters
   # obs. used (total)      17  
   data-arc span      6 days  
   first obs. used      2014-07-26  
   last obs. used      2014-08-01  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .7914  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-11 06:01:28  

Additional Information
 Earth MOID = .0179853 au 
 Jupiter MOID = 2.51705 au 
 T_jup = 3.721 
[ 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 26.3   n/a MPO302050  

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