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17786 (1998 FL36)
Classification: Main-belt Asteroid          SPK-ID: 2017786
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 34 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1135066223467019 3.3476e-08  
a 2.757762130860632 1.2661e-08 au
q 2.444737866150998 9.1002e-08 au
i 6.762951525268379 4.3034e-06 deg
node 164.7477669449431 3.2727e-05 deg
peri 120.6788687096461 3.8152e-05 deg
M 211.4088614483209 2.0817e-05 deg
tp 2459690.936976367045
(2022-Apr-21.43697637)
9.8069e-05 TDB
period 1672.759990365708
4.58
1.152e-05
3.154e-08
d
yr
n .2152131818512079 1.4821e-09 deg/d
Q 3.070786395570265 1.4098e-08 au
  Orbit Determination Parameters
   # obs. used (total)      2000  
   data-arc span      16395 days (44.89 yr)  
   first obs. used      1975-03-15  
   last obs. used      2020-02-02  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .51389  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-22 22:12:06  

Additional Information
 Earth MOID = 1.43705 au 
 Jupiter MOID = 2.10054 au 
 T_jup = 3.323 
[ 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 13.3   n/a MPO416899  
diameter diameter 15.609 km 0.152 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.033   0.004 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

17786 (1998 FL36)          Discovered 1998-Mar-20 by LINEAR at Socorro
Reference: 20001013/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 1998 FL36 = 1975 EU4 = 1986 VB5 = 1989 FV = 1993 BQ15 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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