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(2014 MA6)
Classification: Apollo [NEO]          SPK-ID: 3673918
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.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 26 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2125003337637733 9.9723e-06  
a 1.265538539529423 1.5437e-05 au
q .996611177488502 4.6455e-07 au
i 3.178327737821963 0.00013476 deg
node 242.5619951548476 0.00011457 deg
peri 86.28113590186486 0.00021075 deg
M 160.2912037770094 0.02902 deg
tp 2458968.963918268037
(2020-Apr-29.46391827)
0.037682 TDB
period 520.0097538693632
1.42
0.0095144
2.605e-05
d
yr
n .6922947066305205 1.2667e-05 deg/d
Q 1.534465901570343 1.8717e-05 au
  Orbit Determination Parameters
   # obs. used (total)      95  
   data-arc span      161 days  
   first obs. used      2014-06-21  
   last obs. used      2014-11-29  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      5  
   norm. resid. RMS      .39238  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 10:11:24  

Additional Information
 Earth MOID = .0455726 au 
 Jupiter MOID = 3.7631 au 
 T_jup = 5.074 
[ 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 24.5   n/a MPO317923  

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