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226702 (2004 NY6)
Classification: Main-belt Asteroid          SPK-ID: 2226702
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 18 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2399869119981889 5.0516e-08  
a 2.796112873242333 1.4582e-08 au
q 2.125082379194522 1.4185e-07 au
i 6.084595356117926 5.0556e-06 deg
node 285.368478935787 5.0923e-05 deg
peri 57.46402284636559 5.1774e-05 deg
M 134.7934802315171 9.0506e-06 deg
tp 2458361.064327078491
(2018-Aug-30.56432708)
4.181e-05 TDB
period 1707.774306712494
4.68
1.3359e-05
3.657e-08
d
yr
n .2108006887004926 1.649e-09 deg/d
Q 3.467143367290144 1.8081e-08 au
  Orbit Determination Parameters
   # obs. used (total)      458  
   data-arc span      6973 days (19.09 yr)  
   first obs. used      2000-12-30  
   last obs. used      2020-02-02  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .50965  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-25 05:56:29  

Additional Information
 Earth MOID = 1.12434 au 
 Jupiter MOID = 1.98578 au 
 T_jup = 3.276 
[ 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 15.9   n/a MPO266653  
diameter diameter 3.909 km 0.163 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.055   0.005 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

226702 (2004 NY6)          Discovered 2004-Jul-11 by LINEAR at Socorro
Reference: 20091202/Numbers.arcLast Updated: 2009-12-04

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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