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JPL Small-Body Database Browser
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(2014 UF56)
Classification: Apollo [NEO]          SPK-ID: 3694131
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 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5894311201927093 0.00020826  
a 2.125962153461501 0.00097699 au
q .872853899859384 4.1664e-05 au
i .9356647160525792 0.00014521 deg
node 214.80731997 0.0071103 deg
peri 227.4094597453768 0.0063498 deg
M 152.0166199990327 0.3809 deg
tp 2458122.398296081824
(2018-Jan-03.89829608)
0.86838 TDB
period 1132.222341291621
3.10
0.78048
0.002137
d
yr
n .3179587496827855 0.00021918 deg/d
Q 3.379070407063618 0.0015529 au
  Orbit Determination Parameters
   # obs. used (total)      62  
   data-arc span      2 days  
   first obs. used      2014-10-25  
   last obs. used      2014-10-27  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .41566  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:37:58  

Additional Information
 Earth MOID = .000127771 au 
 Jupiter MOID = 1.89852 au 
 T_jup = 3.480 
[ 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 27.4   n/a MPO313396  

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