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212061 (2005 EJ32)
Classification: Main-belt Asteroid          SPK-ID: 2212061
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | 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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 19 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1717523439283306 4.2011e-08  
a 2.632417765090779 2.2413e-08 au
q 2.18029384373786 1.05e-07 au
i 3.729884555828908 6.5501e-06 deg
node 160.8716749652918 8.7014e-05 deg
peri 110.1142483547049 8.9978e-05 deg
M 117.6502560000308 2.2244e-05 deg
tp 2458490.675124174035
(2019-Jan-07.17512417)
9.6126e-05 TDB
period 1560.02172487665
4.27
1.9924e-05
5.455e-08
d
yr
n .2307660170748359 2.9472e-09 deg/d
Q 3.084541686443697 2.6263e-08 au
  Orbit Determination Parameters
   # obs. used (total)      589  
   data-arc span      9069 days (24.83 yr)  
   first obs. used      1996-01-13  
   last obs. used      2020-11-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .38227  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Dec-18 05:25:17  

Additional Information
 Earth MOID = 1.1676 au 
 Jupiter MOID = 2.02784 au 
 T_jup = 3.375 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 16.6   n/a MPO437019  

212061 (2005 EJ32)          Discovered 2005-Mar-03 by CSS at Catalina
Reference: 20090409/Numbers.arcLast Updated: 2009-04-10

[ show close-approach data ]
Alternate Designations
 2005 EJ32 = 1996 AE11 = 2005 GB213 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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