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JPL Small-Body Database Browser
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(2012 AK10)
Classification: Main-belt Asteroid          SPK-ID: 3595862
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters ]

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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 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1357747013820422 0.0025643  
a 2.328257836142065 0.0010034 au
q 2.012139323699476 0.0066478 au
i 9.816552871045984 0.060654 deg
node 306.5777788245425 0.098689 deg
peri 109.5946160980472 0.34766 deg
M 57.5456780638573 0.42056 deg
tp 2458393.077794468058
(2018-Oct-01.57779447)
1.3841 TDB
period 1297.612548915264
3.55
0.83887
0.002297
d
yr
n .2774325820915812 0.00017935 deg/d
Q 2.644376348584654 0.0011397 au
  Orbit Determination Parameters
   # obs. used (total)      14  
   data-arc span      16 days  
   first obs. used      2011-12-20  
   last obs. used      2012-01-05  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .26256  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-07 19:22:39  

Additional Information
 Earth MOID = 1.04871 au 
 Jupiter MOID = 2.67816 au 
 T_jup = 3.541 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 18.192   .26546 3 autocmod 2.6i
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters ]
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