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(2016 OA)
Classification: Apollo [NEO]          SPK-ID: 3755754
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2457586.5 (2016-Jul-17.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6922508372590036 0.0015943  
a 2.44543556958841 0.011571 au
q .7525807490778846 0.00033774 au
i 1.085490750679075 0.0017227 deg
node 133.4662259410802 0.0094559 deg
peri 231.7526191165101 0.011545 deg
M 348.4531750540285 0.09158 deg
tp 2457631.301529950195
(2016-Aug-30.80152995)
0.037337 TDB
period 1396.795297195288
3.82
9.9142
0.02714
d
yr
n .2577328265085559 0.0018293 deg/d
Q 4.138290390098934 0.019582 au
  Orbit Determination Parameters
   # obs. used (total)      45  
   data-arc span      2 days  
   first obs. used      2016-07-16  
   last obs. used      2016-07-18  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .26302  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:24:50  

Additional Information
 Earth MOID = .00552688 au 
 Jupiter MOID = 1.31513 au 
 T_jup = 3.117 
[ 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 25.4   n/a MPO384700  

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