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(2014 UU116)
Classification: Apollo [NEO]          SPK-ID: 3694986
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 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .398611276185542 0.0004923  
a 1.654616661070889 0.0013503 au
q .9950678022035612 2.5502e-06 au
i 18.43991010233857 0.014199 deg
node 34.39699175089115 7.583e-06 deg
peri 19.36870982482476 0.0049743 deg
M 217.7667035514056 1.1507 deg
tp 2459307.644887863967
(2021-Apr-03.14488786)
2.8609 TDB
period 777.3999646488596
2.13
0.95163
0.002605
d
yr
n .4630820894912271 0.00056687 deg/d
Q 2.314165519938216 0.0018885 au
  Orbit Determination Parameters
   # obs. used (total)      31  
   data-arc span      4 days  
   first obs. used      2014-10-27  
   last obs. used      2014-10-31  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .40248  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-17 06:10:13  

Additional Information
 Earth MOID = .0177645 au 
 Jupiter MOID = 3.10902 au 
 T_jup = 4.126 
[ 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 26.2   n/a MPO313407  

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