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(2014 QD364)
Classification: Aten [NEO]          SPK-ID: 3684638
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 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .0414575545570381 1.6818e-05  
a .9857680451522379 7.773e-07 au
q .9449005126397542 1.7287e-05 au
i 4.009363011425154 0.0019291 deg
node 156.5696670630728 0.0029353 deg
peri 26.68301146785279 0.015367 deg
M 102.4954174227789 0.01489 deg
tp 2458898.719992532420
(2020-Feb-19.21999253)
0.014897 TDB
period 357.4872283039812
0.98
0.00042283
1.158e-06
d
yr
n 1.007028983127426 1.1911e-06 deg/d
Q 1.026635577664722 8.0952e-07 au
  Orbit Determination Parameters
   # obs. used (total)      30  
   data-arc span      17 days  
   first obs. used      2014-08-30  
   last obs. used      2014-09-16  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .64055  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:39:01  

Additional Information
 Earth MOID = .0114807 au 
 Jupiter MOID = 3.92877 au 
 T_jup = 6.146 
[ 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 27.2   n/a E2014T62  

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