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JPL Small-Body Database Browser
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(2014 MJ26)
Classification: Apollo [NEO]          SPK-ID: 3674026
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 2456836.5 (2014-Jun-28.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5033083483756098 0.0012678  
a 2.013071132655067 0.0050842 au
q .999875625715827 2.7394e-05 au
i 6.47329943544336 0.010878 deg
node 111.1290486246506 0.0083751 deg
peri 188.7337833750632 0.0086603 deg
M 353.0312879317318 0.028784 deg
tp 2456856.694687103341
(2014-Jul-18.19468710)
0.007078 TDB
period 1043.246913630841
2.86
3.9522
0.01082
d
yr
n .3450765061428095 0.0013073 deg/d
Q 3.026266639594306 0.0076431 au
  Orbit Determination Parameters
   # obs. used (total)      39  
   data-arc span      1 day  
   first obs. used      2014-06-27  
   last obs. used      2014-06-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .44198  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:39:55  

Additional Information
 Earth MOID = .0113955 au 
 Jupiter MOID = 2.21742 au 
 T_jup = 3.653 
[ 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 24.8   n/a MPO298946  

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