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14433 (1992 EE8)
Classification: Main-belt Asteroid          SPK-ID: 2014433
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | 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.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 25 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1233213280627085 2.5855e-08  
a 2.426068400163985 7.5973e-09 au
q 2.126882423084792 6.1841e-08 au
i 6.485039624583706 4.5205e-06 deg
node 161.5087365451024 3.4923e-05 deg
peri 135.1323741404806 4.1526e-05 deg
M 94.38720971896824 2.2512e-05 deg
tp 2458838.620788439405
(2019-Dec-21.12078844)
8.6312e-05 TDB
period 1380.234849082879
3.78
6.4834e-06
1.775e-08
d
yr
n .2608251778595566 1.2252e-09 deg/d
Q 2.725254377243178 8.5342e-09 au
  Orbit Determination Parameters
   # obs. used (total)      1738  
   data-arc span      13996 days (38.32 yr)  
   first obs. used      1982-09-24  
   last obs. used      2021-01-18  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .49745  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Feb-24 02:18:03  

Additional Information
 Earth MOID = 1.1151 au 
 Jupiter MOID = 2.47224 au 
 T_jup = 3.491 
[ 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 14.88   n/a E2021B10  

14433 (1992 EE8)          Discovered 1992-Mar-02 by UESAC at La Silla
Reference: 20000418/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 1992 EE8 = 1982 SS3 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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