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(2016 CL136)
Classification: Aten [NEO, PHA]          SPK-ID: 3742342
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 32 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6222402980967345 1.8313e-07  
a .729740430857481 1.3455e-09 au
q .2756665276274825 1.3358e-07 au
i 21.51906213750334 2.431e-05 deg
node 316.4401227283495 3.6117e-06 deg
peri 23.52457000030419 6.0127e-06 deg
M 70.05050515769022 3.2303e-05 deg
tp 2458956.194278758478
(2020-Apr-16.69427876)
2.0383e-05 TDB
period 227.6937134292293
0.62
6.2975e-07
1.724e-09
d
yr
n 1.58107131979247 4.3729e-09 deg/d
Q 1.183814334087479 2.1828e-09 au
  Orbit Determination Parameters
   # obs. used (total)      201  
   data-arc span      1842 days (5.04 yr)  
   first obs. used      2016-02-06  
   last obs. used      2021-02-21  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .42134  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Feb-22 05:18:30  

Additional Information
 Earth MOID = .0281825 au 
 Jupiter MOID = 4.22404 au 
 T_jup = 7.676 
[ 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 21.37   n/a E2021D77  
diameter diameter 0.123 km 0.056 urn:nasa:pds:neowise_diameters_albedos::2.0[neos] (http://adsabs.harvard.edu/abs/2017AJ....154..168M)  
geometric albedo albedo 0.320   0.185 urn:nasa:pds:neowise_diameters_albedos::2.0[neos] (http://adsabs.harvard.edu/abs/2017AJ....154..168M)  

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