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(2014 OW3)
Classification: Apollo [NEO]          SPK-ID: 3674947
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2456864.5 (2014-Jul-26.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .7388734704576988 0.0013011  
a 1.761561971605099 0.0065523 au
q .4599905642189331 0.00058122 au
i 8.154059166753903 0.018706 deg
node 305.2178233179449 0.002962 deg
peri 106.2249494751962 0.0032295 deg
M 338.1679949779283 0.1457 deg
tp 2456916.288870347955
(2014-Sep-15.78887035)
0.056666 TDB
period 853.9753131430266
2.34
4.7647
0.01305
d
yr
n .4215578535578886 0.002352 deg/d
Q 3.063133378991264 0.011394 au
  Orbit Determination Parameters
   # obs. used (total)      20  
   data-arc span      2 days  
   first obs. used      2014-07-25  
   last obs. used      2014-07-27  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .40692  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:39:32  

Additional Information
 Earth MOID = .0012094 au 
 Jupiter MOID = 2.42056 au 
 T_jup = 3.730 
[ 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 22.4   n/a MPO302027  

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