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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.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3063021970563786 1.3624e-06  
a 1.372822731983657 2.8641e-06 au
q .9523241130081225 3.4331e-07 au
i .9726952970903978 1.8481e-05 deg
node 18.236378670859 0.00027715 deg
peri 58.02465354501768 0.00032133 deg
M 182.5030898554787 0.0027592 deg
tp 2459490.173266162821
(2021-Oct-02.67326616)		 0.0054092 TDB
period 587.5165699149737
1.61		 0.0018386
5.034e-06		 d
yr
n .612748675415401 1.9176e-06 deg/d
Q 1.793321350959191 3.7414e-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 = .00687344 au 
 Jupiter MOID = 3.46698 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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