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(2010 FV9)
Classification: Apollo [NEO]          SPK-ID: 3512702
[ 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.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 20 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .287336318164286 7.2249e-07  
a 1.147446673140897 4.6665e-08 au
q .8177435707907327 8.621e-07 au
i .6392525788934017 2.1831e-05 deg
node 30.46569837772213 0.0011138 deg
peri 64.84962953965277 0.0011905 deg
M 322.8090530794074 0.00030053 deg
tp 2459246.880126504943
(2021-Feb-01.38012650)		 0.00037759 TDB
period 448.9491912488652
1.23		 2.7387e-05
7.498e-08		 d
yr
n .8018724769245476 4.8917e-08 deg/d
Q 1.477149775491061 6.0074e-08 au
   Orbit Determination Parameters
   # obs. used (total)      71  
   data-arc span      1644 days (4.50 yr)  
   first obs. used      2010-03-21  
   last obs. used      2014-09-20  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      2  
   norm. resid. RMS      .46468  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 03:37:27  

Additional Information
 Earth MOID = .00274114 au 
 Jupiter MOID = 3.68431 au 
 T_jup = 5.434 
[ 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 25.4   n/a MPO190720  

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