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(2016 JQ5)
Classification: Apollo [NEO]          SPK-ID: 3752771
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 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4274443763595397 0.00020467  
a 1.579756493980873 0.0010398 au
q .9044984646112858 0.00027201 au
i 3.435390351051915 0.0026888 deg
node 46.4730810666785 0.0046681 deg
peri 232.1535758230731 0.078498 deg
M 354.0361427845486 0.20255 deg
tp 2459012.514574293126
(2020-Jun-12.01457429)
0.4199 TDB
period 725.2431755608441
1.99
0.71603
0.00196
d
yr
n .4963852293013378 0.00049008 deg/d
Q 2.25501452335046 0.0014842 au
  Orbit Determination Parameters
   # obs. used (total)      63  
   data-arc span      5 days  
   first obs. used      2016-05-03  
   last obs. used      2016-05-08  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .25665  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:26:11  

Additional Information
 Earth MOID = .00293788 au 
 Jupiter MOID = 2.90161 au 
 T_jup = 4.288 
[ 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 28.1   n/a MPO382822  

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