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(2016 OV)
Classification: Apollo [NEO]          SPK-ID: 3756107
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 2457600.5 (2016-Jul-31.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6538003399440255 0.0011175  
a 2.702747118773513 0.0084756 au
q .9356901337366548 8.5954e-05 au
i 10.47556528700547 0.01204 deg
node 133.2127202299409 0.0017821 deg
peri 213.9854885244756 0.00050906 deg
M 352.8669759033157 0.03587 deg
tp 2457632.657163725642
(2016-Sep-01.15716373)
0.010446 TDB
period 1622.955254926487
4.44
7.6342
0.0209
d
yr
n .2218175756276821 0.0010434 deg/d
Q 4.469804103810372 0.014017 au
  Orbit Determination Parameters
   # obs. used (total)      34  
   data-arc span      7 days  
   first obs. used      2016-07-28  
   last obs. used      2016-08-04  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .33484  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:24:49  

Additional Information
 Earth MOID = .00670624 au 
 Jupiter MOID = 1.02518 au 
 T_jup = 2.998 
[ 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 24.6   n/a MPO384702  

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