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JPL Small-Body Database Browser
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469001 (2015 AG193)
Classification: Main-belt Asteroid          SPK-ID: 2469001
[ 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.


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Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 22 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .05460247441318704 6.3243e-08  
a 3.034949969630783 9.1355e-08 au
q 2.869234191568716 1.7979e-07 au
i 10.8957443738884 6.8276e-06 deg
node 125.4664598480297 3.2468e-05 deg
peri 64.45830265551687 7.1095e-05 deg
M 231.2048776615943 6.4593e-05 deg
tp 2459291.411857923440
(2021-Mar-17.91185792)		 0.00035749 TDB
period 1931.193234157668
5.29		 8.7196e-05
2.387e-07		 d
yr
n .186413246293824 8.4168e-09 deg/d
Q 3.20066574769285 9.6343e-08 au
   Orbit Determination Parameters
   # obs. used (total)      167  
   data-arc span      3594 days (9.84 yr)  
   first obs. used      2008-12-03  
   last obs. used      2018-10-06  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .63605  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-14 16:21:10  

Additional Information
 Earth MOID = 1.89281 au 
 Jupiter MOID = 1.83876 au 
 T_jup = 3.212 
[ 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 16.0   n/a MPO419280  

469001 (2015 AG193)          Discovered 2011-Jun-10 by Mt. Lemmon Survey at Mount Lemmon
Reference: Last Updated: 2016-06-21

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