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JPL Small-Body Database Browser
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(2014 TK64)
Classification: Apollo [NEO]          SPK-ID: 3693554
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 2456948.5 (2014-Oct-18.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6067332700689591 0.0053151  
a 1.962679241502816 0.022052 au
q .7718564472093483 0.0017602 au
i 6.717559705305187 0.070943 deg
node 16.22302584294398 0.033397 deg
peri 88.43650619113596 0.078873 deg
M 337.0829475246991 0.41171 deg
tp 2457012.433529254931
(2014-Dec-20.93352925)
0.071255 TDB
period 1004.320715178403
2.75
16.926
0.04634
d
yr
n .3584512343111945 0.0060411 deg/d
Q 3.153502035796284 0.035431 au
  Orbit Determination Parameters
   # obs. used (total)      17  
   data-arc span      7 days  
   first obs. used      2014-10-15  
   last obs. used      2014-10-22  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      9  
   norm. resid. RMS      .38836  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:38:07  

Additional Information
 Earth MOID = .0437413 au 
 Jupiter MOID = 2.08483 au 
 T_jup = 3.621 
[ 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 23.3   n/a MPO322361  

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