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105701 (2000 SS67)
Classification: Main-belt Asteroid          SPK-ID: 2105701
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 22 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .08001759370340078 4.7904e-08  
a 3.046903011568196 2.2655e-08 au
q 2.803097164334864 1.5677e-07 au
i 9.992328385163338 4.998e-06 deg
node 178.1476344188978 2.756e-05 deg
peri 156.3619535710395 4.4135e-05 deg
M 280.3516282340958 3.4607e-05 deg
tp 2459430.294420467542
(2021-Aug-03.79442047)
0.00018771 TDB
period 1942.613363435383
5.32
2.1667e-05
5.932e-08
d
yr
n .185317370288941 2.0669e-09 deg/d
Q 3.290708858801528 2.4468e-08 au
  Orbit Determination Parameters
   # obs. used (total)      606  
   data-arc span      8160 days (22.34 yr)  
   first obs. used      1998-04-17  
   last obs. used      2020-08-19  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .59282  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-12 19:35:06  

Additional Information
 Earth MOID = 1.79726 au 
 Jupiter MOID = 2.08106 au 
 T_jup = 3.210 
[ 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 14.9   n/a MPO385451  
diameter diameter 3.401 km 0.952 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.184   0.098 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

105701 (2000 SS67)          Discovered 2000-Sep-24 by LINEAR at Socorro
Reference: 20051019/Numbers.arcLast Updated: 2005-10-26

Alternate Designations
 2000 SS67 = 2003 EF20 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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