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JPL Small-Body Database Browser
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(2006 SE6)
Classification: Aten [NEO]          SPK-ID: 3342322
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 33 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .345570683381128 1.2794e-07  
a .8050496968016047 1.1885e-09 au
q .5268481229221043 1.0344e-07 au
i 4.816568454381783 1.0646e-05 deg
node 347.2937578527681 1.8652e-05 deg
peri 183.1973177512749 4.7683e-05 deg
M 346.4107170975042 7.2683e-05 deg
tp 2458610.459246970203
(2019-May-06.95924697)
5.328e-05 TDB
period 263.8350334596817
0.72
5.8424e-07
1.6e-09
d
yr
n 1.364488996322067 3.0215e-09 deg/d
Q 1.083251270681105 1.5992e-09 au
  Orbit Determination Parameters
   # obs. used (total)      157  
   data-arc span      4785 days (13.10 yr)  
   first obs. used      2006-08-28  
   last obs. used      2019-10-04  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .57946  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Oct-04 06:12:21  

Additional Information
 Earth MOID = .0363938 au 
 Jupiter MOID = 3.88488 au 
 T_jup = 7.199 
[ 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 22.8   n/a MPO215111  

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