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79352 (1997 AO6)
Classification: Main-belt Asteroid          SPK-ID: 2079352
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 25 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1277580852330771 3.2926e-08  
a 2.207681021884612 7.1668e-09 au
q 1.925631921723231 7.232e-08 au
i 3.959186444007214 3.344e-06 deg
node 90.00265085411742 6.0416e-05 deg
peri 38.31853453250046 6.2656e-05 deg
M 148.532781811753 1.5464e-05 deg
tp 2458902.163444185589
(2020-Feb-22.66344419)
5.1269e-05 TDB
period 1198.127160364718
3.28
5.8342e-06
1.597e-08
d
yr
n .3004689417861237 1.4631e-09 deg/d
Q 2.489730122045994 8.0824e-09 au
  Orbit Determination Parameters
   # obs. used (total)      836  
   data-arc span      8566 days (23.45 yr)  
   first obs. used      1996-12-28  
   last obs. used      2020-06-11  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .56445  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Jul-08 23:08:24  

Additional Information
 Earth MOID = .943146 au 
 Jupiter MOID = 2.55309 au 
 T_jup = 3.646 
[ 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 16.46   n/a E2021B10  
diameter diameter 1.319 km 0.246 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.306   0.141 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

79352 (1997 AO6)          Discovered 1997-Jan-03 by Kawasato, N. at Uenohara
Reference: 20040504/Numbers.arcLast Updated: 2004-07-16

Alternate Designations
 1997 AO6 = 1999 VM7 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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