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JPL Small-Body Database Browser
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(2014 UA58)
Classification: Apollo [NEO]          SPK-ID: 3694522
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 2456957.5 (2014-Oct-27.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5413704446201604 0.0017163  
a 2.011606291513179 0.007293 au
q .9225820990759774 0.00010818 au
i 7.833748013862667 0.019583 deg
node 211.013982352029 0.00061901 deg
peri 230.8348371364943 0.0038472 deg
M 346.8702201811325 0.079757 deg
tp 2456995.507372491341
(2014-Dec-04.00737249)
0.024206 TDB
period 1042.108419611183
2.85
5.6672
0.01552
d
yr
n .3454534991035944 0.0018786 deg/d
Q 3.100630483950381 0.011241 au
  Orbit Determination Parameters
   # obs. used (total)      19  
   data-arc span      4 days  
   first obs. used      2014-10-25  
   last obs. used      2014-10-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .64242  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-19 05:25:50  

Additional Information
 Earth MOID = .0288475 au 
 Jupiter MOID = 2.22667 au 
 T_jup = 3.622 
[ 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 26.6   n/a MPO313400  

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