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(2008 CP)
Classification: Amor [NEO]          SPK-ID: 3401386
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 19 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .07766371312162872 0.0001372  
a 1.120491566198018 0.00023273 au
q 1.033470030645611 6.0923e-05 au
i 13.5962209618506 0.016013 deg
node 140.0253589984122 0.00038337 deg
peri 17.06885334621658 0.001005 deg
M 120.1243526581289 1.1779 deg
tp 2458855.942751124696
(2020-Jan-07.44275112)
1.3725 TDB
period 433.222809892809
1.19
0.13497
0.0003695
d
yr
n .8309811759197852 0.0002589 deg/d
Q 1.207513101750425 0.00025081 au
  Orbit Determination Parameters
   # obs. used (total)      116  
   data-arc span      15 days  
   first obs. used      2008-02-02  
   last obs. used      2008-02-17  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .50221  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 09:04:34  

Additional Information
 Earth MOID = .0496927 au 
 Jupiter MOID = 3.77273 au 
 T_jup = 5.543 
[ 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 24.1   n/a MPO133579  
rotation period rot_per 0.83253 h n/a LCDB (Rev. 2019-August); Warner et al., 2009 Published Reference List:
[Statler, T.S.; Cotto-Figueroa, D.; Riethmiller, D.A.; Sweeney, K.M. (2013) Icarus 225, 141-155.]

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