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JPL Small-Body Database Browser
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(2003 YN107)
Classification: Aten [NEO]          SPK-ID: 3170221
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | 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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 17 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .0139483706887979 2.113e-07  
a .9886958239928577 3.5989e-08 au
q .9749051281413388 1.7388e-07 au
i 4.321254694442802 2.6316e-05 deg
node 264.4003970666828 6.7774e-05 deg
peri 87.68763945091693 0.00011024 deg
M 299.9440040361035 0.00051919 deg
tp 2458660.402693332217
(2019-Jun-25.90269333)		 0.00052111 TDB
period 359.0810418423841
0.98		 1.9606e-05
5.368e-08		 d
yr
n 1.002559194305834 5.474e-08 deg/d
Q 1.002486519844377 3.6491e-08 au
   Orbit Determination Parameters
   # obs. used (total)      45  
   data-arc span      467 days (1.28 yr)  
   first obs. used      2003-12-20  
   last obs. used      2005-03-31  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      1  
   norm. resid. RMS      .4166  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 09:13:21  

Additional Information
 Earth MOID = .00504976 au 
 Jupiter MOID = 3.98535 au 
 T_jup = 6.132 
[ show covariance matrix ]

[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 26.5   n/a MPO77762  

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