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79350 (1996 YW)
Classification: Main-belt Asteroid          SPK-ID: 2079350
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 .09030831997443671 3.9793e-08  
a 2.158289866948568 5.5023e-09 au
q 1.963378335046593 8.4947e-08 au
i 4.164616913380146 4.3641e-06 deg
node 72.12765316832656 4.17e-05 deg
peri 2.470278591452729 4.5208e-05 deg
M 288.8188740528173 1.742e-05 deg
tp 2459625.494703308478
(2022-Feb-14.99470331)
5.6231e-05 TDB
period 1158.145394499969
3.17
4.4289e-06
1.213e-08
d
yr
n .3108418007873964 1.1887e-09 deg/d
Q 2.353201398850544 5.9993e-09 au
  Orbit Determination Parameters
   # obs. used (total)      1440  
   data-arc span      8993 days (24.62 yr)  
   first obs. used      1996-12-20  
   last obs. used      2021-08-04  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .47573  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Aug-25 01:49:17  

Additional Information
 Earth MOID = .978133 au 
 Jupiter MOID = 2.82367 au 
 T_jup = 3.690 
[ 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 15.30   n/a MPO637106  
diameter diameter 2.278 km 0.331 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.283   0.093 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

79350 (1996 YW)          Discovered 1996-Dec-20 by Kobayashi, T. at Oizumi
Reference: 20040504/Numbers.arcLast Updated: 2004-07-16

Alternate Designations
 1996 YW = 1999 XO66 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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