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(2015 CS)
Classification: Apollo [NEO]          SPK-ID: 3709926
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 11 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4955493309393675 0.00018173  
a 1.902378261164755 0.00066858 au
q .9596559866509634 8.46e-06 au
i 2.989711615690979 0.00086172 deg
node 321.7383587593256 8.934e-05 deg
peri 211.3017072125237 0.0012083 deg
M 357.6204122892754 0.37729 deg
tp 2459006.834946554701
(2020-Jun-06.33494655)
1.0078 TDB
period 958.3932331697627
2.62
0.50524
0.001383
d
yr
n .3756286955505165 0.00019802 deg/d
Q 2.845100535678547 0.0009999 au
  Orbit Determination Parameters
   # obs. used (total)      62  
   data-arc span      6 days  
   first obs. used      2015-02-10  
   last obs. used      2015-02-16  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .32797  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:35:48  

Additional Information
 Earth MOID = .00605642 au 
 Jupiter MOID = 2.13017 au 
 T_jup = 3.784 
[ 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 26.4   n/a MPO335352  
rotation period rot_per 0.2433 h n/a LCDB (Rev. 2019-August); Warner et al., 2009 Published Reference List:
[Thirouin, A.; Moskovitz, N.; Binzel, R.P.; Christensen, E.; et al. (2016) Astron. J. 152, A163.]

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