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15886 (1997 EB6)
Classification: Main-belt Asteroid          SPK-ID: 2015886
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 19 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1275730834977119 3.8178e-08  
a 2.301469970031771 9.0085e-09 au
q 2.007864349377432 8.5638e-08 au
i 3.701710724135899 4.3779e-06 deg
node 48.60044065068391 6.6177e-05 deg
peri 190.8407047387324 6.9661e-05 deg
M 176.2897842037138 2.2745e-05 deg
tp 2458376.002015563648
(2018-Sep-14.50201556)		 8.0701e-05 TDB
period 1275.282486801923
3.49		 7.4876e-06
2.05e-08		 d
yr
n .2822903974026856 1.6574e-09 deg/d
Q 2.595075590686111 1.0158e-08 au
   Orbit Determination Parameters
   # obs. used (total)      1105  
   data-arc span      8811 days (24.12 yr)  
   first obs. used      1995-10-15  
   last obs. used      2019-11-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .5499  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Dec-14 00:04:54  

Additional Information
 Earth MOID = .995735 au 
 Jupiter MOID = 2.40568 au 
 T_jup = 3.577 
[ show covariance matrix ]

[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 15.2   n/a MPO502291  

15886 (1997 EB6)          Discovered 1997-Mar-07 by Kobayashi, T. at Oizumi
Reference: 20000726/Numbers.arcLast Updated: 2004-04-19

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Alternate Designations
 1997 EB6 = 1998 QN107 = 1998 QO101 = 1998 SV165 = 2000 AT35 
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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