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5546 Salavat (1979 YS)
Classification: Main-belt Asteroid          SPK-ID: 2005546
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 28 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1125562396323325 4.3364e-08  
a 2.62255354126828 1.3619e-08 au
q 2.327368776428666 1.1232e-07 au
i 12.18930949583633 4.812e-06 deg
node 287.2011944058933 2.2569e-05 deg
peri 241.9171482846633 3.1234e-05 deg
M 39.31985743324266 2.1836e-05 deg
tp 2458431.068402490983
(2018-Nov-08.56840249)
9.406e-05 TDB
period 1551.261349479818
4.25
1.2083e-05
3.308e-08
d
yr
n .2320692126576339 1.8077e-09 deg/d
Q 2.917738306107895 1.5152e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1609  
   data-arc span      15863 days (43.43 yr)  
   first obs. used      1976-03-07  
   last obs. used      2019-08-12  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .45763  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Sep-24 00:50:53  

Additional Information
 Earth MOID = 1.36387 au 
 Jupiter MOID = 2.20099 au 
 T_jup = 3.363 
[ 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 12.5   n/a MPO384804  
diameter diameter 8.390 km 0.064 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2014ApJ...791..121M)  
geometric albedo albedo 0.302   0.053 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2014ApJ...791..121M)  

5546 Salavat (1979 YS)          Discovered 1979-Dec-18 by Debehogne, H. at La Silla
Reference: DISCOVERY.DBLast Updated: 2003-08-29

[ show close-approach data ]
Alternate Designations
 1979 YS = 1976 EE = 1990 OO4 = 1991 RK29 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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