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(2016 AW192)
Classification: Apollo [NEO]          SPK-ID: 3740344
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 2457403.5 (2016-Jan-16.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6849597739124197 0.0028628  
a 1.999340778226058 0.015384 au
q .6298727707984562 0.00088046 au
i 1.941875340854919 0.01006 deg
node 310.7595254659212 0.02926 deg
peri 72.72599329293178 0.030566 deg
M 18.406439716664 0.2419 deg
tp 2457350.704615792125
(2015-Nov-24.20461579)
0.084505 TDB
period 1032.591778062755
2.83
11.918
0.03263
d
yr
n .3486372907940403 0.0040238 deg/d
Q 3.36880878565366 0.025921 au
  Orbit Determination Parameters
   # obs. used (total)      16  
   data-arc span      3 days  
   first obs. used      2016-01-15  
   last obs. used      2016-01-18  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      9  
   norm. resid. RMS      .53095  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:29:04  

Additional Information
 Earth MOID = .00811303 au 
 Jupiter MOID = 2.09826 au 
 T_jup = 3.505 
[ 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 25.3   n/a MPO365057  

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