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(2014 KC46)
Classification: Apollo [NEO]          SPK-ID: 3672672
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 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .7043669766310003 4.4019e-05  
a 2.415508585316926 0.00031208 au
q .7141041060510183 1.4074e-05 au
i 4.015558579766642 0.00020435 deg
node 53.68874332898931 0.00074501 deg
peri 279.6021910267409 0.0011894 deg
M 201.3565269109731 0.10734 deg
tp 2459604.769971865093
(2022-Jan-25.26997187)
0.52596 TDB
period 1371.233153407811
3.75
0.26574
0.0007276
d
yr
n .2625374095611109 5.0879e-05 deg/d
Q 4.116913064582834 0.0005319 au
  Orbit Determination Parameters
   # obs. used (total)      46  
   data-arc span      158 days  
   first obs. used      2014-05-25  
   last obs. used      2014-10-30  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .37787  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:40:20  

Additional Information
 Earth MOID = .0111543 au 
 Jupiter MOID = 1.30326 au 
 T_jup = 3.119 
[ 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 22.8   n/a MPO296108  

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