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393808 (2005 QT104)
Classification: Main-belt Asteroid          SPK-ID: 2393808
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 14 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1250926367199001 1.2953e-07  
a 2.934490616083495 3.0483e-08 au
q 2.567407447487806 3.8255e-07 au
i 17.64704574132593 7.1643e-06 deg
node 173.8811672544223 1.7949e-05 deg
peri 214.9591681282465 3.406e-05 deg
M 303.8839082532884 3.4972e-05 deg
tp 2459286.708435898397
(2021-Mar-13.20843590)
0.00018118 TDB
period 1836.105005111315
5.03
2.861e-05
7.833e-08
d
yr
n .1960672178322257 3.0551e-09 deg/d
Q 3.301573784679183 3.4296e-08 au
  Orbit Determination Parameters
   # obs. used (total)      154  
   data-arc span      9020 days (24.70 yr)  
   first obs. used      1995-09-18  
   last obs. used      2020-05-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .53373  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Jun-24 06:57:04  

Additional Information
 Earth MOID = 1.58661 au 
 Jupiter MOID = 2.20133 au 
 T_jup = 3.193 
[ 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 16.5   n/a MPO476860  
diameter diameter 3.623 km 1.314 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.026   0.018 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

393808 (2005 QT104)          Discovered 2005-Aug-27 by NEAT at Palomar
Reference: Last Updated: 2014-05-15

Alternate Designations
 2005 QT104 = 1995 SV57 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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