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(2014 UA176)
Classification: Apollo [NEO]          SPK-ID: 3695413
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 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5106672788364357 0.00047362  
a 1.911955841201472 0.0017811 au
q .9355825545196877 3.4004e-05 au
i 4.923230469118561 0.0033221 deg
node 46.4594163104119 0.00026095 deg
peri 32.71594200319747 0.001424 deg
M 27.103507789017 1.0538 deg
tp 2458927.799363333929
(2020-Mar-19.29936333)
2.7252 TDB
period 965.6399239360097
2.64
1.3493
0.003694
d
yr
n .3728097721277069 0.00052093 deg/d
Q 2.888329127883256 0.0026906 au
  Orbit Determination Parameters
   # obs. used (total)      22  
   data-arc span      10 days  
   first obs. used      2014-10-27  
   last obs. used      2014-11-06  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .56229  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:37:43  

Additional Information
 Earth MOID = .000587396 au 
 Jupiter MOID = 2.40792 au 
 T_jup = 3.760 
[ 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 26.7   n/a MPCxxxxx  

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