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97016 (1999 TS262)
Classification: Main-belt Asteroid          SPK-ID: 2097016
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 26 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .146787361789185 6.1457e-08  
a 2.632287807278092 1.2281e-08 au
q 2.245901224577902 1.6109e-07 au
i 14.71882168084012 5.5958e-06 deg
node 327.1825296890679 1.876e-05 deg
peri 33.32627576630532 2.3081e-05 deg
M 321.7162755912913 1.4182e-05 deg
tp 2459166.386164389464
(2020-Nov-12.88616439)
6.1898e-05 TDB
period 1559.906203029253
4.27
1.0917e-05
2.989e-08
d
yr
n .230783106895081 1.6151e-09 deg/d
Q 3.018674389978282 1.4084e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1179  
   data-arc span      7589 days (20.78 yr)  
   first obs. used      1999-09-07  
   last obs. used      2020-06-17  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .49526  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Jun-24 01:02:26  

Additional Information
 Earth MOID = 1.25363 au 
 Jupiter MOID = 2.44063 au 
 T_jup = 3.338 
[ 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 14.1   n/a MPO395861  
diameter diameter 6.171 km 0.360 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.140   0.016 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

97016 (1999 TS262)          Discovered 1999-Oct-14 by LINEAR at Socorro
Reference: 20050224/Numbers.arcLast Updated: 2005-02-28

Alternate Designations
 1999 TS262 = 2001 BU9 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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