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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 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 17 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .01391935250374673 2.1025e-07  
a .9887202616094475 3.5485e-08 au
q .9749579157605088 1.7335e-07 au
i 4.320944515732164 2.6317e-05 deg
node 264.396295363925 6.7846e-05 deg
peri 87.67445508156993 0.00011213 deg
M 181.4964221765487 0.00055359 deg
tp 2459378.554519866309
(2021-Jun-13.05451987)		 0.0005617 TDB
period 359.0943550457509
0.98		 1.9332e-05
5.293e-08		 d
yr
n 1.002522025037497 5.3971e-08 deg/d
Q 1.002482607458386 3.5979e-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 = .00478619 au 
 Jupiter MOID = 3.98303 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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