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JPL Small-Body Database Browser
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(2014 KQ75)
Classification: Apollo [NEO]          SPK-ID: 3672732
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6626811527650904 0.00057011  
a 2.189770035933203 0.0034601 au
q .7386507042305347 8.126e-05 au
i 14.44853672246717 0.0098291 deg
node 68.68047929064872 0.00041767 deg
peri 254.2515348057796 0.0047904 deg
M 170.8783492675415 1.2508 deg
tp 2458038.701300960039
(2017-Oct-12.20130096)
2.7807 TDB
period 1183.576108508224
3.24
2.8053
0.00768
d
yr
n .3041629493972661 0.00072092 deg/d
Q 3.640889367635872 0.0057531 au
  Orbit Determination Parameters
   # obs. used (total)      57  
   data-arc span      5 days  
   first obs. used      2014-05-27  
   last obs. used      2014-06-01  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .32217  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:40:19  

Additional Information
 Earth MOID = .011248 au 
 Jupiter MOID = 1.97913 au 
 T_jup = 3.317 
[ 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 25.3   n/a MPO296110  

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