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(2014 JY79)
Classification: Apollo [NEO]          SPK-ID: 3698572
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters ]

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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 2456783.5 (2014-May-06.0) TDB
Reference: JPL 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6768930302462429 1.571  
a 1.800288235262527 5.3923 au
q .581685676379014 2.7246 au
i 20.0478815896878 92.349 deg
node 275.0325737813246 216.28 deg
peri 158.2510592374149 119.2 deg
M 106.1427123541086 912.44 deg
tp 2456523.364769961569
(2013-Aug-18.86476996)
1074.2 TDB
period 882.2902744505772
2.42
3964
10.85
d
yr
n .4080289791522189 1.8332 deg/d
Q 3.01889079414604 9.0424 au
  Orbit Determination Parameters
   # obs. used (total)      16  
   data-arc span      1 day  
   first obs. used      2014-05-05  
   last obs. used      2014-05-06  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      9  
   norm. resid. RMS      .1923  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Dec-18 11:21:06  

Additional Information
 Earth MOID = .296593 au 
 Jupiter MOID = 2.34835 au 
 T_jup = 3.704 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 18.6   n/a MPO317897  
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters ]
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