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414800 (2010 SV3)
Classification: Apollo [NEO]          SPK-ID: 2414800
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | 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 39 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5153145931473193 9.9085e-08  
a 1.512581683246288 8.1708e-08 au
q .7331262685421399 1.877e-07 au
i 6.197003599740975 1.8801e-05 deg
node 24.184509094314 0.00013977 deg
peri 224.3451466250148 0.0001506 deg
M 123.2817353534076 0.00015954 deg
tp 2458767.812571256914
(2019-Oct-11.31257126)
0.00028228 TDB
period 679.4800065668888
1.86
5.5057e-05
1.507e-07
d
yr
n .5298169136998163 4.293e-08 deg/d
Q 2.292037097950437 1.2381e-07 au
  Orbit Determination Parameters
   # obs. used (total)      164  
   # delay obs. used      1  
   # Doppler obs. used      1  
   data-arc span      1495 days (4.09 yr)  
   first obs. used      2010-09-17  
   last obs. used      2014-10-21  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      1  
   norm. resid. RMS      .38918  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 09:21:31  

Additional Information
 Earth MOID = .0561751 au 
 Jupiter MOID = 2.76782 au 
 T_jup = 4.359 
[ show covariance matrix ]

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

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 20.8   n/a MPO265001  

414800 (2010 SV3)          Discovered 2010-Sep-17 by CSS at Catalina
Reference: Last Updated: 2014-11-10

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