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JPL Small-Body Database Browser
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95976 (2004 LY17)
Classification: Main-belt Asteroid          SPK-ID: 2095976
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer was implemented using two-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances.


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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 17 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2174038599370153 3.4702e-08  
a 2.436341665296825 1.5157e-08 au
q 1.90667158313592 8.837e-08 au
i 2.801296083404309 5.8379e-06 deg
node 60.94680271177285 8.2813e-05 deg
peri 263.4722015645462 8.4342e-05 deg
M 57.73961042278914 1.9678e-05 deg
tp 2458777.719556590435
(2019-Oct-21.21955659)		 7.4438e-05 TDB
period 1389.011097237833
3.80		 1.2962e-05
3.549e-08		 d
yr
n .2591771949956993 2.4185e-09 deg/d
Q 2.966011747457731 1.8452e-08 au
   Orbit Determination Parameters
   # obs. used (total)      663  
   data-arc span      12308 days (33.70 yr)  
   first obs. used      1985-08-24  
   last obs. used      2019-05-06  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .56006  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-May-30 06:11:32  

Additional Information
 Earth MOID = .897105 au 
 Jupiter MOID = 2.37332 au 
 T_jup = 3.470 
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[ 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 15.6   n/a MPO436440  

95976 (2004 LY17)          Discovered 2004-Jun-14 by LINEAR at Socorro
Reference: 20041028/Numbers.arcLast Updated: 2004-10-29

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Alternate Designations
 2004 LY17 = 1985 QE6 = 1985 SS1 = 2003 EN48 
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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