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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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Orbit Diagram
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Note: This Java-based orbit viewer will eventually be retired.

Note: Make sure you have Java enabled on your browser to see the applet. This applet is provided as a 3D orbit visualization tool. The applet 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. For accurate long-term ephemerides, please instead use our Horizons system.

Note: If the applet is not working, here are some notes that might help.
Orbit Viewer

Additional Notes: the orbits shown in the applet are color coded. The planets are white lines, and the asteroid/comet is a blue line. The bright white line indicates the portion of the orbit that is above the ecliptic plane, and the darker portion is below the ecliptic plane. Likewise for the asteroid/comet orbit, the light blue indicates the portion above the ecliptic plane, and the dark blue the portion below the ecliptic plane.

Orbit Viewer applet originally written and kindly provided by Osamu Ajiki (AstroArts), and further modified by Ron Baalke (JPL).


Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 21 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .094221647761318 1.0335e-05  
a .9912509412071083 5.6598e-06 au
q .8978536441816172 1.5366e-05 au
i 6.811124824076825 0.00080038 deg
node 6.680487743926498 0.00010443 deg
peri 101.6949893624364 0.0041128 deg
M 153.7899089395076 0.024514 deg
tp 2458446.507636402403
(2018-Nov-24.00763640)
0.023228 TDB
period 360.4739171602022
0.99
0.0030873
8.453e-06
d
yr
n .9986852941706971 8.5533e-06 deg/d
Q 1.084648238232599 6.193e-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 = .000134363 au 
 Jupiter MOID = 3.94282 au 
 T_jup = 6.112 
[ hide covariance matrix ]
Orbital Elements at Epoch 2455099.5 (2009-Sep-25.0) TDB
Reference: JPL 21 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .09363203927710632 8.9771e-06  
q .9155708981545505 6.1497e-06 au
tp 2455187.405719215446
(2009-Dec-21.90571922)
0.0016045 TDB
node 7.226871672711796 3.768e-05 deg
peri 91.23965566220225 0.00092719 deg
i 6.871089969648254 0.00079124 deg
  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
 Jupiter MOID = 3.94282 au 
 T_jup = 6.112 
Orbit Covariance (6×6)
  e q tp node peri i
e 8.058917332995007E-11 -5.515473475953928E-11 -1.434561494515785E-8 3.370190864161241E-10 -8.171833781516696E-9 7.102622605310631E-9
q -5.515473475953928E-11 3.781898412079306E-11 9.779577721083997E-9 -2.305699680373776E-10 5.545678999754861E-9 -4.860421006863799E-9
tp -1.434561494515785E-8 9.779577721083997E-9 2.574392788229055E-6 -6.003159814659429E-8 1.480031215281137E-6 -1.264623055422206E-6
node 3.370190864161241E-10 -2.305699680373776E-10 -6.003159814659429E-8 1.419772975156159E-9 -3.423298198603636E-8 2.970181265401026E-8
peri -8.171833781516696E-9 5.545678999754861E-9 1.480031215281137E-6 -3.423298198603636E-8 8.596763141936946E-7 -7.205687832551698E-7
i 7.102622605310631E-9 -4.860421006863799E-9 -1.264623055422206E-6 2.970181265401026E-8 -7.205687832551698E-7 6.260633629287703E-7

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-January); Warner et al., 2009 Incomplete or inconclusive result.
Published Reference List:
[Ryan, W. UNPUBLISHED]

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Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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