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66723 (1999 TE107)
Classification: Main-belt Asteroid          SPK-ID: 2066723
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 26 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1131580236543092 4.0561e-08  
a 2.633855676363807 1.2236e-08 au
q 2.335813773435795 1.0745e-07 au
i 13.3870144327702 5.0493e-06 deg
node 281.6108686350843 1.7426e-05 deg
peri 162.5643134761867 3.0258e-05 deg
M 268.5807257920177 2.4697e-05 deg
tp 2459596.980338910573
(2022-Jan-17.48033891)
0.00010813 TDB
period 1561.300100491758
4.27
1.088e-05
2.979e-08
d
yr
n .230577068358999 1.6068e-09 deg/d
Q 2.931897579291819 1.3621e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1550  
   data-arc span      10596 days (29.01 yr)  
   first obs. used      1992-01-07  
   last obs. used      2021-01-10  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .45511  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 12:24:32  

Additional Information
 Earth MOID = 1.35504 au 
 Jupiter MOID = 2.27083 au 
 T_jup = 3.351 
[ 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 14.16   n/a E2021B10  
diameter diameter 4.054 km 0.327 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.270   0.078 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

66723 (1999 TE107)          Discovered 1999-Oct-04 by LINEAR at Socorro
Reference: 20030910/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 1999 TE107 = 1992 AM6 = 2000 VT36 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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