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(2016 AQ164)
Classification: Apollo [NEO]          SPK-ID: 3739965
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 2457400.5 (2016-Jan-13.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5777302488746625 0.0011206  
a 1.916874278904693 0.0045381 au
q .8094380246916455 0.00023177 au
i 5.298539183255467 0.0084014 deg
node 289.9026877938601 0.00037172 deg
peri 120.7082951716054 0.0036229 deg
M 15.64809407654258 0.063229 deg
tp 2457358.364532246451
(2015-Dec-01.86453225)
0.020628 TDB
period 969.3684302433046
2.65
3.4424
0.009425
d
yr
n .3713758244733043 0.0013188 deg/d
Q 3.02431053311774 0.0071599 au
  Orbit Determination Parameters
   # obs. used (total)      11  
   data-arc span      2 days  
   first obs. used      2016-01-12  
   last obs. used      2016-01-14  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .3336  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:29:13  

Additional Information
 Earth MOID = .000666858 au 
 Jupiter MOID = 2.40569 au 
 T_jup = 3.701 
[ 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 29.8   n/a MPO365032  

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