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(2015 EO6)
Classification: Apollo [NEO]          SPK-ID: 3713070
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 2457092.5 (2015-Mar-11.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .7599788991761719 0.0013356  
a 2.299680332190768 0.01104 au
q .5519718048753348 0.00042179 au
i 6.533535260805334 0.011149 deg
node 170.5351315280516 4.6853e-05 deg
peri 92.03426441625706 0.0026684 deg
M 347.0032926779396 0.10567 deg
tp 2457138.486512131445
(2015-Apr-25.98651213)
0.042774 TDB
period 1273.795274224551
3.49
9.1723
0.02511
d
yr
n .2826199839838135 0.0020351 deg/d
Q 4.047388859506201 0.019429 au
  Orbit Determination Parameters
   # obs. used (total)      13  
   first obs. used      2015-03-11  
   last obs. used      2015-03-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .55607  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:35:10  

Additional Information
 Earth MOID = .000715716 au 
 Jupiter MOID = 1.15467 au 
 T_jup = 3.121 
[ 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 30.2   n/a MPO332789  

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