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JPL Small-Body Database Browser
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(2014 AZ32)
Classification: Apollo [NEO]          SPK-ID: 3655872
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 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4839157542471662 0.00030205  
a 1.902129566135926 0.0011503 au
q .9816591024634246 1.9104e-05 au
i 1.586198713705733 0.00078214 deg
node 291.6699483915869 0.00076448 deg
peri 198.1587641931503 0.00073414 deg
M 150.6849397905958 0.78263 deg
tp 2458599.424697926554
(2019-Apr-25.92469793)
1.7193 TDB
period 958.2053053682246
2.62
0.86919
0.00238
d
yr
n .3757023656445496 0.0003408 deg/d
Q 2.822600029808428 0.0017069 au
  Orbit Determination Parameters
   # obs. used (total)      80  
   data-arc span      5 days  
   first obs. used      2014-01-09  
   last obs. used      2014-01-14  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .35253  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:42:56  

Additional Information
 Earth MOID = .00457157 au 
 Jupiter MOID = 2.25125 au 
 T_jup = 3.793 
[ 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 26.0   n/a E2014B07  

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