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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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3063680317075554 1.3578e-06  
a 1.372818631343336 2.8721e-06 au
q .9522308893672182 3.4918e-07 au
i .9727099803180531 1.8482e-05 deg
node 18.23691566721642 0.00027721 deg
peri 58.03177374388728 0.00032123 deg
M 59.93665616144564 0.0023757 deg
tp 2458902.684386488322
(2020-Feb-23.18438649)
0.0035703 TDB
period 587.5139375368668
1.61
0.0018438
5.048e-06
d
yr
n .6127514208586921 1.923e-06 deg/d
Q 1.793406373319455 3.7521e-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 = .00695271 au 
 Jupiter MOID = 3.4666 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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