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JPL Small-Body Database Browser
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(2009 SH2)
Classification: Aten [NEO]          SPK-ID: 3467258
[ 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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 21 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .09423138874481182 1.0324e-05  
a .9912333761976367 5.5972e-06 au
q .8978280785883249 1.5298e-05 au
i 6.811121572713721 0.00080031 deg
node 6.674089746493703 0.00010347 deg
peri 101.7253950465811 0.0041077 deg
M 193.2620605369264 0.02791 deg
tp 2459167.453001661983
(2020-Nov-13.95300166)		 0.02936 TDB
period 360.4643357825869
0.99		 0.0030531
8.359e-06		 d
yr
n .9987118398784757 8.4591e-06 deg/d
Q 1.084638673806949 6.1246e-06 au
   Orbit Determination Parameters
   # obs. used (total)      109  
   data-arc span      14 days  
   first obs. used      2009-09-18  
   last obs. used      2009-10-02  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .37076  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:59:56  

Additional Information
 Earth MOID = .000599611 au 
 Jupiter MOID = 3.94128 au 
 T_jup = 6.112 
[ 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 24.9   n/a MPO164364  
rotation period rot_per 1.26 h n/a LCDB (Rev. 2019-August); Warner et al., 2009 Incomplete or inconclusive result.
Published Reference List:
[Ryan, W. UNPUBLISHED]

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