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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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4836542630782931 0.00031064  
a 1.901384443309015 0.0011409 au
q .9817717515518626 1.6036e-06 au
i 1.58574809882426 0.00079132 deg
node 291.6791336666058 0.00064808 deg
peri 198.0892232133972 0.00074521 deg
M .4865898445894614 0.64827 deg
tp 2458599.205613808474
(2019-Apr-25.70561381)
1.7233 TDB
period 957.6423226471884
2.62
0.86192
0.00236
d
yr
n .3759232351018701 0.00033835 deg/d
Q 2.820997135066167 0.0016927 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 = .00469379 au 
 Jupiter MOID = 2.25438 au 
 T_jup = 3.794 
[ 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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