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(2017 AZ3)
Classification: Apollo [NEO]          SPK-ID: 3766326
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 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2704544932019451 0.000115  
a 1.29676559529518 0.00018882 au
q .9460495134179032 1.1391e-05 au
i 4.034764638642355 0.0016589 deg
node 285.3834030793733 0.00014693 deg
peri 217.0561262381749 0.0011506 deg
M 87.21085470191245 0.17939 deg
tp 2458869.835175838121
(2020-Jan-21.33517584)
0.24024 TDB
period 539.3747929550425
1.48
0.11781
0.0003225
d
yr
n .667439421904921 0.00014578 deg/d
Q 1.647481677172456 0.00023989 au
  Orbit Determination Parameters
   # obs. used (total)      33  
   data-arc span      2 days  
   first obs. used      2017-01-05  
   last obs. used      2017-01-07  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .40965  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:21:11  

Additional Information
 Earth MOID = .00249584 au 
 Jupiter MOID = 3.37315 au 
 T_jup = 4.971 
[ 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 30.0   n/a MPO394978  

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