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JPL Small-Body Database Browser
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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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3988647171154164 0.0004882  
a 1.654447988589607 0.0013582 au
q .994547059638644 8.7702e-06 au
i 18.44370855883969 0.014104 deg
node 34.40236618997417 0.00016549 deg
peri 19.37631405322751 0.0046836 deg
M 32.47748775650015 0.92354 deg
tp 2458530.377396552300
(2019-Feb-15.87739655)
1.9077 TDB
period 777.2810948445259
2.13
0.95714
0.002621
d
yr
n .4631529087581994 0.00057033 deg/d
Q 2.314348917540571 0.0018999 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 = .0166862 au 
 Jupiter MOID = 3.10725 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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