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(2016 JG29)
Classification: Apollo [NEO]          SPK-ID: 3753306
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 2457521.5 (2016-May-13.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6198795676646943 0.0011304  
a 2.161871214399914 0.0059072 au
q .8217714206709477 0.00019855 au
i 4.678141007684899 0.0063489 deg
node 223.6910639416055 0.0021289 deg
peri 304.9590902261791 0.003685 deg
M 13.8778444150505 0.06414 deg
tp 2457476.742824799133
(2016-Mar-29.24282480)
0.023414 TDB
period 1161.029234110598
3.18
4.7587
0.01303
d
yr
n .3100697117896232 0.0012709 deg/d
Q 3.50197100812888 0.009569 au
  Orbit Determination Parameters
   # obs. used (total)      56  
   data-arc span      4 days  
   first obs. used      2016-05-12  
   last obs. used      2016-05-16  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .47509  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:25:53  

Additional Information
 Earth MOID = .00559623 au 
 Jupiter MOID = 1.52043 au 
 T_jup = 3.415 
[ 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 25.4   n/a MPO386980  

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