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JPL Small-Body Database Browser
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(2014 MB6)
Classification: Apollo [NEO]          SPK-ID: 3673917
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 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6502642474867234 0.00078578  
a 2.824055563080373 0.0062406 au
q .9876731974932195 3.6535e-05 au
i 1.279946724471008 0.0011272 deg
node 107.2015052161553 0.0027441 deg
peri 134.4007107983901 0.0018144 deg
M 12.29439258121785 1.2182 deg
tp 2458541.301206096048
(2019-Feb-26.80120610)
5.6697 TDB
period 1733.437879475256
4.75
5.7458
0.01573
d
yr
n .2076797814692838 0.0006884 deg/d
Q 4.660437928667528 0.010299 au
  Orbit Determination Parameters
   # obs. used (total)      33  
   data-arc span      12 days  
   first obs. used      2014-06-21  
   last obs. used      2014-07-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .40992  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:40:00  

Additional Information
 Earth MOID = .00904823 au 
 Jupiter MOID = .371973 au 
 T_jup = 2.962 
[ 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 26.2   n/a MPO298937  

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