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(2016 CY135)
Classification: Apollo [NEO]          SPK-ID: 3742333
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 33 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3534619958837394 8.0174e-06  
a 1.475081133061978 1.6806e-05 au
q .9536960116794433 9.6048e-07 au
i 1.10374712867583 2.1032e-05 deg
node 173.4902546844873 6.1526e-05 deg
peri 26.54235538971641 0.00015012 deg
M 113.2784770475396 0.01425 deg
tp 2458794.594859047999
(2019-Nov-07.09485905)
0.022383 TDB
period 654.368355531581
1.79
0.011183
3.062e-05
d
yr
n .5501488526405763 9.4023e-06 deg/d
Q 1.996466254444513 2.2747e-05 au
  Orbit Determination Parameters
   # obs. used (total)      87  
   data-arc span      164 days  
   first obs. used      2016-01-31  
   last obs. used      2016-07-13  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .37376  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:28:31  

Additional Information
 Earth MOID = .00178157 au 
 Jupiter MOID = 2.96002 au 
 T_jup = 4.523 
[ 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 24.5   n/a MPO373615  

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