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(2014 QD3)
Classification: Apollo [NEO]          SPK-ID: 3682231
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 2456889.5 (2014-Aug-20.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4097397021272258 0.0014603  
a 1.550272099662481 0.0035014 au
q .9150640713306269 0.00019797 au
i 4.31420763986132 0.014485 deg
node 308.2209659632843 0.0074646 deg
peri 81.26025136108538 0.014014 deg
M 333.0293623708288 0.10853 deg
tp 2456942.320077819686
(2014-Oct-11.82007782)
0.033617 TDB
period 705.0344258275979
1.93
2.3886
0.00654
d
yr
n .5106133641310031 0.0017299 deg/d
Q 2.185480127994334 0.0049361 au
  Orbit Determination Parameters
   # obs. used (total)      16  
   data-arc span      4 days  
   first obs. used      2014-08-19  
   last obs. used      2014-08-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .50067  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:39:17  

Additional Information
 Earth MOID = .0413326 au 
 Jupiter MOID = 3.28044 au 
 T_jup = 4.349 
[ 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 25.0   n/a MPO305346  

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