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(2014 OO6)
Classification: Apollo [NEO]          SPK-ID: 3674964
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 19 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6787239138272032 4.5638e-06  
a 2.203633683679195 2.4682e-05 au
q .7079748052509948 2.1336e-06 au
i 1.3818332820646 1.8228e-05 deg
node 111.1570309973244 0.00019647 deg
peri 287.3437334271505 0.00017716 deg
M 263.3360730858001 0.010581 deg
tp 2459321.325931189030
(2021-Apr-16.82593119)
0.040508 TDB
period 1194.833883901362
3.27
0.020075
5.496e-05
d
yr
n .3012971132225768 5.0621e-06 deg/d
Q 3.699292562107396 4.1435e-05 au
  Orbit Determination Parameters
   # obs. used (total)      99  
   data-arc span      154 days  
   first obs. used      2014-07-25  
   last obs. used      2014-12-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .42217  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:39:31  

Additional Information
 Earth MOID = .000194428 au 
 Jupiter MOID = 1.73459 au 
 T_jup = 3.317 
[ 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 23.1   n/a E2014P61  

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