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160406 (2004 TR10)
Classification: Main-belt Asteroid          SPK-ID: 2160406
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 21 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2088387187107273 4.0481e-08  
a 2.17795448944547 1.5972e-08 au
q 1.723113264459402 9.2779e-08 au
i 5.640969939072066 3.9163e-06 deg
node 89.34159677461932 5.3688e-05 deg
peri 187.2566642534941 5.7612e-05 deg
M 26.31373710376229 2.7263e-05 deg
tp 2458914.687281924315
(2020-Mar-06.18728192)
8.826e-05 TDB
period 1174.009544346689
3.21
1.2915e-05
3.536e-08
d
yr
n .306641459376152 3.3732e-09 deg/d
Q 2.632795714431539 1.9308e-08 au
  Orbit Determination Parameters
   # obs. used (total)      459  
   data-arc span      6933 days (18.98 yr)  
   first obs. used      2000-03-12  
   last obs. used      2019-03-06  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .58661  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-24 13:19:19  

Additional Information
 Earth MOID = .706893 au 
 Jupiter MOID = 2.49118 au 
 T_jup = 3.648 
[ 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 16.6   n/a MPO433025  
diameter diameter 1.301 km 0.098 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.262   0.044 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

160406 (2004 TR10)          Discovered 2004-Oct-07 by LINEAR at Socorro
Reference: 20070730/Numbers.arcLast Updated: 2007-08-06

Alternate Designations
 2004 TR10 = 2005 YS116 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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