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35256 (1996 DT1)
Classification: Main-belt Asteroid          SPK-ID: 2035256
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 25 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1117347639718964 3.7184e-08  
a 3.169066653570336 2.0436e-08 au
q 2.814971739022447 1.1742e-07 au
i 12.50701905408419 3.7474e-06 deg
node 136.9269433366766 2.0847e-05 deg
peri 301.5675377665632 2.8291e-05 deg
M 159.0001402326016 2.0824e-05 deg
tp 2458090.397109134395
(2017-Dec-02.89710913)
0.0001156 TDB
period 2060.608501554255
5.64
1.9932e-05
5.457e-08
d
yr
n .1747056754004765 1.6899e-09 deg/d
Q 3.523161568118224 2.2719e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1228  
   data-arc span      8878 days (24.31 yr)  
   first obs. used      1996-02-23  
   last obs. used      2020-06-14  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .544  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Jun-23 20:28:56  

Additional Information
 Earth MOID = 1.85505 au 
 Jupiter MOID = 1.72306 au 
 T_jup = 3.156 
[ 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 13.7   n/a MPO474206  
diameter diameter 5.164 km 1.544 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.219   0.195 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

35256 (1996 DT1)          Discovered 1996-Feb-23 by Visnjan at Visnjan
Reference: 20020227/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 1996 DT1 = 1999 RU66 = 2000 YN122 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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