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(2003 YN107)
Classification: Aten [NEO]          SPK-ID: 3170221
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

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.


Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 17 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .01394089337692221 2.1107e-07  
a .9887073048543162 3.5761e-08 au
q .9749238417363582 1.7389e-07 au
i 4.32116932297961 2.6316e-05 deg
node 264.3992225246647 6.779e-05 deg
peri 87.6138467362434 0.00011144 deg
M 341.043178903016 0.00054203 deg
tp 2459019.408760100284
(2020-Jun-18.90876010)		 0.00054167 TDB
period 359.0872964025253
0.98		 1.9482e-05
5.334e-08		 d
yr
n 1.002541731792293 5.4393e-08 deg/d
Q 1.002490767972275 3.626e-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 = .00511928 au 
 Jupiter MOID = 3.98416 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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