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226032 (2002 FN16)
Classification: Main-belt Asteroid          SPK-ID: 2226032
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 18 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1882079833950228 3.5791e-08  
a 2.640977524669558 1.7062e-08 au
q 2.143924470559921 9.5583e-08 au
i 12.91715800474214 6.7496e-06 deg
node 58.64006979033133 2.0406e-05 deg
peri 84.46878879947091 2.8076e-05 deg
M 121.7995764346501 1.9039e-05 deg
tp 2458470.118017848753
(2018-Dec-17.61801785)
8.1538e-05 TDB
period 1567.636925871363
4.29
1.5192e-05
4.159e-08
d
yr
n .229645011583212 2.2254e-09 deg/d
Q 3.138030578779194 2.0273e-08 au
  Orbit Determination Parameters
   # obs. used (total)      633  
   data-arc span      7646 days (20.93 yr)  
   first obs. used      1998-06-01  
   last obs. used      2019-05-08  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .58694  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-May-30 08:28:41  

Additional Information
 Earth MOID = 1.20171 au 
 Jupiter MOID = 2.04179 au 
 T_jup = 3.334 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 15.7   n/a MPO385977  
diameter diameter 1.903 km 0.255 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.308   0.062 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

226032 (2002 FN16)          Discovered 2002-Mar-16 by NEAT at Haleakala
Reference: 20091202/Numbers.arcLast Updated: 2009-12-04

Alternate Designations
 2002 FN16 = 1998 LX3 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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