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JPL Small-Body Database Browser
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(2016 UB107)
Classification: Apollo [NEO]          SPK-ID: 3763102
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 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3062507718025663 1.3535e-06  
a 1.372936667622115 2.8646e-06 au
q .9524737535267992 3.4858e-07 au
i .9728803976681568 1.8484e-05 deg
node 18.26019666484704 0.00027702 deg
peri 57.97867153450518 0.00032101 deg
M 174.8755029761139 0.0016083 deg
tp 2458315.069315622135
(2018-Jul-15.56931562)
0.0017335 TDB
period 587.5897116937336
1.61
0.001839
5.035e-06
d
yr
n .612672401908291 1.9175e-06 deg/d
Q 1.793399581717432 3.7419e-06 au
  Orbit Determination Parameters
   # obs. used (total)      26  
   # delay obs. used      1  
   # Doppler obs. used      1  
   data-arc span      35 days  
   first obs. used      2016-10-17  
   last obs. used      2016-11-21  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      3  
   norm. resid. RMS      .46245  
   source      ORB  
   producer      OSOD/JPL  
   solution date      2017-Jul-11 15:30:21  

Additional Information
 Earth MOID = .00691093 au 
 Jupiter MOID = 3.46712 au 
 T_jup = 4.768 
[ 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 25.2   n/a MPO389558  

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