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(2006 NL)
Classification: Aten [NEO]          SPK-ID: 3337325
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 48 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .575954307042822 2.3815e-07  
a .847714185991316 2.0177e-09 au
q .3594695494283177 2.0138e-07 au
i 20.07705229535916 1.6201e-05 deg
node 115.2195547805626 6.4016e-06 deg
peri 29.36343373065913 6.7748e-06 deg
M 33.46950167868282 2.7604e-05 deg
tp 2458973.995516300959
(2020-May-04.49551630)
2.1803e-05 TDB
period 285.0838420977151
0.78
1.0178e-06
2.787e-09
d
yr
n 1.262786404697768 4.5086e-09 deg/d
Q 1.335958822554314 3.1799e-09 au
  Orbit Determination Parameters
   # obs. used (total)      289  
   # delay obs. used      1  
   # Doppler obs. used      1  
   data-arc span      5134 days (14.06 yr)  
   first obs. used      2006-07-02  
   last obs. used      2020-07-22  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .34572  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Aug-31 09:27:52  

Additional Information
 Earth MOID = .0566991 au 
 Jupiter MOID = 3.7125 au 
 T_jup = 6.758 
[ 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 20.0   n/a MPO268432  

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