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(2016 UX5)
Classification: Apollo [NEO]          SPK-ID: 3761397
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 .2606805851175668 0.0002927  
a 1.247529965321455 0.00041914 au
q .9223231240097599 5.5282e-05 au
i 2.654107293332082 0.0029909 deg
node 205.9675471504613 0.0018243 deg
peri 246.5386496062983 0.0035834 deg
M 172.6147447543399 0.44463 deg
tp 2458756.466024150580
(2019-Sep-29.96602415)
0.50561 TDB
period 508.9497506763973
1.39
0.25649
0.0007022
d
yr
n .7073389848831988 0.00035648 deg/d
Q 1.572736806633149 0.0005284 au
  Orbit Determination Parameters
   # obs. used (total)      38  
   data-arc span      12 days  
   first obs. used      2016-10-21  
   last obs. used      2016-11-02  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .55631  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:22:52  

Additional Information
 Earth MOID = .0138934 au 
 Jupiter MOID = 3.60091 au 
 T_jup = 5.115 
[ 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 26.5   n/a E2016-UC0  

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