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(2008 YC3)
Classification: Apollo [NEO]          SPK-ID: 3441850
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.


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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 13 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .04555856245388028 6.0303e-05  
a 1.015987664837534 1.1498e-05 au
q .9697007273566612 5.0293e-05 au
i 12.02240580744375 0.014518 deg
node 91.45814126719317 0.00083316 deg
peri 82.25519224478946 0.10196 deg
M 344.8114357122502 0.014934 deg
tp 2459016.281391820134
(2020-Jun-15.78139182)
0.015784 TDB
period 374.0512235136363
1.02
0.0063495
1.738e-05
d
yr
n .9624350285994344 1.6337e-05 deg/d
Q 1.062274602318407 1.2021e-05 au
  Orbit Determination Parameters
   # obs. used (total)      34  
   data-arc span      30 days  
   first obs. used      2008-12-22  
   last obs. used      2009-01-21  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .42887  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 09:01:52  

Additional Information
 Earth MOID = .0038436 au 
 Jupiter MOID = 3.91753 au 
 T_jup = 5.985 
[ 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 25.3   n/a MPO152529  

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