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JPL Small-Body Database Browser
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(2006 AN)
Classification: Apollo [NEO]          SPK-ID: 3310464
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 14 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2204496380836382 1.541e-07  
a 1.094137497834916 1.5384e-09 au
q .8529352824234715 1.6806e-07 au
i 7.407304482908281 1.9609e-05 deg
node 277.6074247356605 3.8001e-05 deg
peri 273.4368442439398 9.2171e-05 deg
M 163.6243737164037 7.6563e-05 deg
tp 2458410.500798070622
(2018-Oct-19.00079807)
8.9047e-05 TDB
period 418.0288739447066
1.14
8.8163e-07
2.414e-09
d
yr
n .8611845315919919 1.8163e-09 deg/d
Q 1.335339713246361 1.8775e-09 au
  Orbit Determination Parameters
   # obs. used (total)      67  
   data-arc span      3193 days (8.74 yr)  
   first obs. used      2006-01-03  
   last obs. used      2014-10-01  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .57861  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 09:09:32  

Additional Information
 Earth MOID = .00541985 au 
 Jupiter MOID = 3.64159 au 
 T_jup = 5.643 
[ 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 24.3   n/a MPO279058  

[ show close-approach data ]
Alternate Designations
 2006 AN = 2014 AA16 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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