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(2011 CL50)
Classification: Aten [NEO]          SPK-ID: 3557536
[ 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 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 25 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1463964484614483 4.5424e-08  
a .8830594778163257 1.0523e-08 au
q .7537827064837945 4.1968e-08 au
i .190980427858396 1.1062e-06 deg
node 354.6432506819495 0.00089025 deg
peri 308.7678269415601 0.00088683 deg
M 4.981597099908099 3.4262e-05 deg
tp 2459392.305796868132
(2021-Jun-26.80579687)		 2.8854e-05 TDB
period 303.0982026829276
0.83		 5.4178e-06
1.483e-08		 d
yr
n 1.187733865834228 2.123e-08 deg/d
Q 1.012336249148857 1.2063e-08 au

Additional Model Parameters
 Parameter Value Uncertainty (1-sigma) 
A2 [EST] 4.363195656880273E-12 3.548E-13
ALN [SET] 1. n/a
NK [SET] 0. n/a
NM [SET] 2. n/a
R0 [SET] 1. n/a
   Orbit Determination Parameters
   # obs. used (total)      131  
   data-arc span      3628 days (9.93 yr)  
   first obs. used      2011-02-12  
   last obs. used      2021-01-18  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      1  
   norm. resid. RMS      .44163  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 04:47:51  

Additional Information
 Earth MOID = .00117228 au 
 Jupiter MOID = 4.09007 au 
 T_jup = 6.707 
 Nongravitational accels. using nonstandard g(r) = (1 au/ r)^2 
[ 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 27.3   n/a MPCxxxxx  

[ show close-approach data ]
Alternate Designations
 2011 CL50 = 2020 YN4 
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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