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JPL Small-Body Database Browser
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(2014 UT56)
Classification: Apollo [NEO]          SPK-ID: 3694454
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 2456958.5 (2014-Oct-28.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4805435490785412 0.0019707  
a 1.810447694610328 0.0066517 au
q .940448734021218 0.00011454 au
i 8.399874587495168 0.027899 deg
node 32.81636900889247 0.0016231 deg
peri 51.44438409702114 0.0030552 deg
M 343.0791428464412 0.10349 deg
tp 2457000.321273996746
(2014-Dec-08.82127400)
0.02534 TDB
period 889.7692653626605
2.44
4.9036
0.01343
d
yr
n .4045992753562552 0.0022298 deg/d
Q 2.680446655199438 0.0098481 au
  Orbit Determination Parameters
   # obs. used (total)      15  
   data-arc span      5 days  
   first obs. used      2014-10-24  
   last obs. used      2014-10-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .57897  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:37:56  

Additional Information
 Earth MOID = .0389641 au 
 Jupiter MOID = 2.6324 au 
 T_jup = 3.898 
[ 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 26.3   n/a MPO313397  

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