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JPL Small-Body Database Browser
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(2014 UD192)
Classification: Apollo [NEO]          SPK-ID: 3695649
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 2456962.5 (2014-Nov-01.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5776639018809754 0.0011524  
a 1.84922652303038 0.0043865 au
q .7809951142748612 0.00027853 au
i 1.02708383906748 0.0014631 deg
node 252.7941781239475 0.013283 deg
peri 218.5700555487025 0.011069 deg
M 340.0187883005536 0.081301 deg
tp 2457013.480362349229
(2014-Dec-21.98036235)
0.026037 TDB
period 918.5093838043319
2.51
3.2682
0.008948
d
yr
n .3919393817283962 0.0013946 deg/d
Q 2.917457931785899 0.0069205 au
  Orbit Determination Parameters
   # obs. used (total)      20  
   data-arc span      8 days  
   first obs. used      2014-10-30  
   last obs. used      2014-11-07  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .56486  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:37:39  

Additional Information
 Earth MOID = .00792894 au 
 Jupiter MOID = 2.24016 au 
 T_jup = 3.787 
[ 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 25.9   n/a MPCxxxxx  

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