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(2019 SU10)
Classification: Apollo [NEO]          SPK-ID: 3874051
[ 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 2458752.5 (2019-Sep-26.0) TDB
Reference: JPL 1 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6164908545783865 0.0019069  
a 2.593969897586899 0.012884 au
q .9948111786729419 6.3856e-06 au
i 16.40703962710981 0.030903 deg
node 182.2745942156871 1.8588e-05 deg
peri 194.9862701957338 0.0048988 deg
M 357.1935043541871 0.023405 deg
tp 2458764.396184653049
(2019-Oct-07.89618465)		 0.010688 TDB
period 1525.969399413459
4.18		 11.369
0.03113		 d
yr
n .2359156088833591 0.0017577 deg/d
Q 4.193128616500856 0.020827 au
   Orbit Determination Parameters
   # obs. used (total)      24  
   data-arc span      1 day  
   first obs. used      2019-09-25  
   last obs. used      2019-09-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .31557  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Oct-05 06:19:53  

Additional Information
 Earth MOID = .00479298 au 
 Jupiter MOID = 1.28658 au 
 T_jup = 3.073 
[ 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 27.2   .21608 MPO492735 autocmod 2.8

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