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233038 (2005 GE3)
Classification: Main-belt Asteroid          SPK-ID: 2233038
[ 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.


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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 16 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1429328271853139 5.9054e-08  
a 2.76283936373804 2.2977e-08 au
q 2.367938922420088 1.6515e-07 au
i 16.54529884452976 5.3264e-06 deg
node 98.43232373957788 2.2903e-05 deg
peri 139.8987073830775 3.0255e-05 deg
M 66.14987904302635 1.7788e-05 deg
tp 2458692.281691269967
(2019-Jul-27.78169127)		 8.3472e-05 TDB
period 1677.381618047107
4.59		 2.0925e-05
5.729e-08		 d
yr
n .2146202129120327 2.6773e-09 deg/d
Q 3.157739805055992 2.6261e-08 au
   Orbit Determination Parameters
   # obs. used (total)      448  
   data-arc span      5272 days (14.43 yr)  
   first obs. used      2005-03-12  
   last obs. used      2019-08-18  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .57241  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-25 07:15:22  

Additional Information
 Earth MOID = 1.37611 au 
 Jupiter MOID = 1.97799 au 
 T_jup = 3.266 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457460.5 (2016-Mar-13.0) TDB
Reference: JPL 16 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1416903843524357 5.9247e-08  
q 2.371915958827622 1.6519e-07 au
tp 2457015.143748200187
(2014-Dec-23.64374820)		 9.0621e-05 TDB
node 98.45424492581039 2.2913e-05 deg
peri 140.0541734952943 3.0382e-05 deg
i 16.53933101454849 5.3272e-06 deg
   Orbit Determination Parameters
   # obs. used (total)      448  
   data-arc span      5272 days (14.43 yr)  
   first obs. used      2005-03-12  
   last obs. used      2019-08-18  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .57241  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-25 07:15:22  

Additional Information
 Jupiter MOID = 1.97799 au 
 T_jup = 3.266 
Orbit Covariance (6×6)
  e q tp node peri i
e 3.51015653967911E-15 -9.718134502359366E-15 -1.66709830031717E-12 -3.579055874376533E-15 -3.531722760222312E-13 -7.840466777930924E-15
q -9.718134502359366E-15 2.728637296287077E-14 3.891259064113402E-12 1.04163687592593E-14 8.315897545865388E-13 2.225403870109858E-14
tp -1.66709830031717E-12 3.891259064113402E-12 8.212242046205697E-9 8.142931146183711E-12 1.866997787657554E-9 8.102997147370793E-12
node -3.579055874376533E-15 1.04163687592593E-14 8.142931146183711E-12 5.250110235863894E-10 -5.014021139229847E-10 -4.918528691495368E-11
peri -3.531722760222312E-13 8.315897545865388E-13 1.866997787657554E-9 -5.014021139229847E-10 9.23072014786715E-10 4.902450104940791E-11
i -7.840466777930924E-15 2.225403870109858E-14 8.102997147370793E-12 -4.918528691495368E-11 4.902450104940791E-11 2.837881007967787E-11

[ 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 15.5   n/a MPO433522  
diameter diameter 3.141 km 0.092 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.103   0.017 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

233038 (2005 GE3)          Discovered 2005-Apr-01 by CSS at Catalina
Reference: 20100228/Numbers.arcLast Updated: 2010-03-03

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Alternate Designations
 2005 GE3 = 2008 UU326 
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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