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JPL Small-Body Database Browser
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(2008 CD6)
Classification: Apollo [NEO]          SPK-ID: 3402132
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 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 22 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .594695750354548 1.6641e-07  
a 1.976681195105463 2.1362e-08 au
q .8011572885704951 3.3752e-07 au
i 1.065668418446478 8.6153e-06 deg
node 178.7264705778463 0.00010817 deg
peri 235.8166086694313 0.00012036 deg
M 318.3431246315109 6.6061e-06 deg
tp 2459513.959341848164
(2021-Oct-26.45934185)
1.6738e-05 TDB
period 1015.08725009474
2.78
1.6455e-05
4.505e-08
d
yr
n .3546493170576229 5.7492e-09 deg/d
Q 3.152205101640432 3.4067e-08 au
  Orbit Determination Parameters
   # obs. used (total)      148  
   # delay obs. used      0  
   # Doppler obs. used      1  
   data-arc span      4967 days (13.60 yr)  
   first obs. used      2008-02-07  
   last obs. used      2021-09-13  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .32366  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Sep-14 06:55:15  

Additional Information
 Earth MOID = .00234464 au 
 Jupiter MOID = 2.23654 au 
 T_jup = 3.623 
[ 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 23.7   n/a MPO133580  

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