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(2013 UE1)
Classification: Apollo [NEO]          SPK-ID: 3652984
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 14 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5283394365315623 0.00050711  
a 1.983334835457804 0.0019737 au
q .9354608260386089 7.4859e-05 au
i 2.69324161648666 0.0020572 deg
node 201.51274338165 0.00095269 deg
peri 236.8205503730589 0.00056683 deg
M 116.178280038627 1.2108 deg
tp 2458671.258229324736
(2019-Jul-06.75822932)
2.9398 TDB
period 1020.216837464689
2.79
1.5229
0.004169
d
yr
n .3528661621529648 0.00052673 deg/d
Q 3.031208844876999 0.0030165 au
  Orbit Determination Parameters
   # obs. used (total)      63  
   data-arc span      15 days  
   first obs. used      2013-10-22  
   last obs. used      2013-11-06  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .34318  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:44:05  

Additional Information
 Earth MOID = .0184221 au 
 Jupiter MOID = 2.26377 au 
 T_jup = 3.671 
[ 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 24.4   n/a E2013V29  

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