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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 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 27 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2086962573935194 2.8925e-08  
a 2.177466500576253 9.7774e-09 au
q 1.723037391306225 5.892e-08 au
i 5.640897402824228 2.6439e-06 deg
node 89.33964879085713 5.1058e-05 deg
peri 187.2178740716653 5.2846e-05 deg
M 87.70222431018946 1.4681e-05 deg
tp 2458914.587095341287
(2020-Mar-06.08709534)
4.7699e-05 TDB
period 1173.614996503323
3.21
7.9047e-06
2.164e-08
d
yr
n .3067445466124638 2.066e-09 deg/d
Q 2.63189560984628 1.1818e-08 au
  Orbit Determination Parameters
   # obs. used (total)      699  
   data-arc span      7605 days (20.82 yr)  
   first obs. used      2000-03-12  
   last obs. used      2021-01-06  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .54492  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 20:01:13  

Additional Information
 Earth MOID = .704961 au 
 Jupiter MOID = 2.49102 au 
 T_jup = 3.649 
[ 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 16.76   n/a E2021B55  
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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