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(2016 AV64)
Classification: Apollo [NEO]          SPK-ID: 3739378
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 2457393.5 (2016-Jan-06.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .489154308052099 0.0022386  
a 1.315095740977619 0.0037842 au
q .6718109937774494 0.0010109 au
i 6.060759839562622 0.029424 deg
node 104.550130398793 0.0017424 deg
peri 268.3942984277736 0.010048 deg
M 37.80458186688211 0.22357 deg
tp 2457335.653588593196
(2015-Nov-09.15358859)
0.092419 TDB
period 550.8514332939225
1.51
2.3776
0.00651
d
yr
n .6535337447473096 0.0028208 deg/d
Q 1.958380488177789 0.0056353 au
  Orbit Determination Parameters
   # obs. used (total)      9  
   data-arc span      4 days  
   first obs. used      2016-01-05  
   last obs. used      2016-01-09  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .36861  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:29:22  

Additional Information
 Earth MOID = .00641803 au 
 Jupiter MOID = 3.50928 au 
 T_jup = 4.829 
[ 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 27.0   n/a MPO364961  

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