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(2016 JS5)
Classification: Apollo [NEO]          SPK-ID: 3752783
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 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6270621549882228 0.00014906  
a 2.104774891329445 0.00075885 au
q .7849502122073007 3.0799e-05 au
i 3.053441414146814 0.00061374 deg
node 45.4005450744751 7e-05 deg
peri 245.0880537177089 0.00068789 deg
M 105.9008839346171 0.25382 deg
tp 2458672.401690622452
(2019-Jul-07.90169062)
0.60895 TDB
period 1115.339050888766
3.05
0.60318
0.001651
d
yr
n .3227718062172497 0.00017456 deg/d
Q 3.424599570451589 0.0012347 au
  Orbit Determination Parameters
   # obs. used (total)      38  
   data-arc span      2 days  
   first obs. used      2016-05-03  
   last obs. used      2016-05-05  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .34593  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:26:10  

Additional Information
 Earth MOID = .000192781 au 
 Jupiter MOID = 1.80695 au 
 T_jup = 3.462 
[ 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 30.7   n/a MPO378516  

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