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364136 (2006 CJ)
Classification: Aten [NEO, PHA]          SPK-ID: 2364136
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 65 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .7548825220790071 5.0684e-08  
a .6765338652903506 3.7641e-09 au
q .1658302747881115 3.4101e-08 au
i 10.23224314654655 1.1978e-05 deg
node 303.2456523433922 1.9505e-05 deg
peri 29.64148902124884 1.9218e-05 deg
M 74.92821140680547 2.6276e-05 deg
tp 2458958.196567899311
(2020-Apr-18.69656790)
1.4497e-05 TDB
period 203.2510221492486
0.56
1.6963e-06
4.644e-09
d
yr
n 1.771208804724483 1.4782e-08 deg/d
Q 1.18723745579259 6.6056e-09 au

Additional Model Parameters
 Parameter Value Uncertainty (1-sigma) 
A2 [EST] -2.86066987867071E-14 3.343E-15
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)      382  
   # delay obs. used      5  
   # Doppler obs. used      3  
   data-arc span      4104 days (11.24 yr)  
   first obs. used      2006-02-01  
   last obs. used      2017-04-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .41629  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Dec-21 06:16:48  

Additional Information
 Earth MOID = .0256747 au 
 Jupiter MOID = 4.19895 au 
 T_jup = 8.157 
 Nongravitational accels. using nonstandard g(r) = (1 au/ r)^2 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 20.2   n/a MPO261196  

364136 (2006 CJ)          Discovered 2006-Feb-01 by Siding Spring Survey at Siding Spring
Reference: Last Updated: 2013-06-26

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