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(2006 JY26)
Classification: Apollo [NEO]          SPK-ID: 3332535
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 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .08306377211064156 1.8526e-05  
a 1.01026291540192 9.7533e-06 au
q .9263466668251423 9.8279e-06 au
i 1.438796963561099 0.00016929 deg
node 43.45882801728808 0.0083472 deg
peri 273.6101178538601 0.018264 deg
M 61.8582617575269 0.12163 deg
tp 2459136.769803877499
(2020-Oct-14.26980388)
0.12438 TDB
period 370.8942015543914
1.02
0.005371
1.47e-05
d
yr
n .9706271990537072 1.4056e-05 deg/d
Q 1.094179163978697 1.0563e-05 au
  Orbit Determination Parameters
   # obs. used (total)      77  
   data-arc span      4 days  
   first obs. used      2006-05-06  
   last obs. used      2006-05-10  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      3  
   norm. resid. RMS      .51484  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-14 23:40:05  

Additional Information
 Earth MOID = .000187153 au 
 Jupiter MOID = 3.98204 au 
 T_jup = 6.028 
[ 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 28.4   n/a MPO102343  

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