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(2009 FU30)
Classification: Apollo [NEO]          SPK-ID: 3455349
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 2454920.5 (2009-Mar-30.0) TDB
Reference: JPL 11 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5967780962988251 0.0010013  
a 2.399278997078234 0.005849 au
q .9674418447121313 4.4072e-05 au
i .847442863205207 0.0012466 deg
node 115.0365506016755 0.013124 deg
peri 106.0598181307168 0.0081583 deg
M 353.3227465262913 0.025415 deg
tp 2454945.677634068615
(2009-Apr-24.17763407)
0.00377 TDB
period 1357.436601798964
3.72
4.9638
0.01359
d
yr
n .2652057558510683 0.00096978 deg/d
Q 3.831116149444337 0.0093396 au
  Orbit Determination Parameters
   # obs. used (total)      36  
   data-arc span      6 days  
   first obs. used      2009-03-28  
   last obs. used      2009-04-03  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      8  
   norm. resid. RMS      .51716  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 02:40:34  

Additional Information
 Earth MOID = .0106045 au 
 Jupiter MOID = 1.14512 au 
 T_jup = 3.258 
[ 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 MPO156203  

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