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(2014 MC6)
Classification: Apollo [NEO]          SPK-ID: 3673912
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 20 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .629714718038155 9.6757e-06  
a 2.21472349903803 5.1705e-05 au
q .8200795153088209 2.2921e-06 au
i 10.39930348226502 0.00012706 deg
node 83.93491539780135 0.00038074 deg
peri 197.2628324677689 0.00036112 deg
M 281.8723570155847 0.022429 deg
tp 2459261.764208951671
(2021-Feb-16.26420895)
0.084153 TDB
period 1203.864747863484
3.30
0.042158
0.0001154
d
yr
n .299036914768787 1.0472e-05 deg/d
Q 3.60936748276724 8.4264e-05 au
  Orbit Determination Parameters
   # obs. used (total)      61  
   data-arc span      134 days  
   first obs. used      2014-06-15  
   last obs. used      2014-10-27  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .64595  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:40:00  

Additional Information
 Earth MOID = .111814 au 
 Jupiter MOID = 1.58406 au 
 T_jup = 3.346 
[ 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 19.4   n/a E2014T58  

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