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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 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 18 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .0139120918919508 2.1059e-07  
a .9887145486066238 3.5387e-08 au
q .9749594609514998 1.7377e-07 au
i 4.320840629081052 2.6316e-05 deg
node 264.393817312871 6.7855e-05 deg
peri 87.49641279364907 0.00011532 deg
M 18.17007476228493 0.00056782 deg
tp 2459378.375792427691
(2021-Jun-12.87579243)		 0.00056542 TDB
period 359.0912426829616
0.98		 1.9278e-05
5.278e-08		 d
yr
n 1.002530714228085 5.3823e-08 deg/d
Q 1.002469636261748 3.588e-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.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      1  
   norm. resid. RMS      .41945  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-14 22:05:46  

Additional Information
 Earth MOID = .0051284 au 
 Jupiter MOID = 3.98204 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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