Skip Page Navigation
NASA JPL Caltech
NASA Logo - Jet Propulsion Laboratory + View the NASA Portal
+ Center for Near-Earth Object Studies
JPL Home Earth Solar System Stars & Galaxies Technology
JPL Solar System Dynamics
BODIES ORBITS EPHEMERIDES TOOLS PHYSICAL DATA DISCOVERY FAQ SITE MAP
IMPORTANT: The SSD Announcement email list is now available. Major changes are coming in the near future, including possible hostname and/or URL changes. To be notified of such changes, subscribe to this email list.

Please visit this page for more details.


JPL Small-Body Database Browser
Search: [ help ]  
413158 (2002 GE64)
Classification: Main-belt Asteroid          SPK-ID: 2413158
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2134366552517036 5.1914e-08  
a 2.974957966809757 3.0835e-08 au
q 2.339992888859474 1.5406e-07 au
i 2.847685958993671 5.9096e-06 deg
node 99.23298082206412 0.00018701 deg
peri 130.8239529711653 0.00018865 deg
M 100.9328487019027 2.5007e-05 deg
tp 2458075.027844562257
(2017-Nov-17.52784456)
0.00012552 TDB
period 1874.21615847073
5.13
2.9139e-05
7.978e-08
d
yr
n .1920802989414747 2.9863e-09 deg/d
Q 3.609923044760041 3.7416e-08 au
  Orbit Determination Parameters
   # obs. used (total)      166  
   data-arc span      6409 days (17.55 yr)  
   first obs. used      2002-04-08  
   last obs. used      2019-10-25  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .59255  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-08 14:34:49  

Additional Information
 Earth MOID = 1.33089 au 
 Jupiter MOID = 1.3867 au 
 T_jup = 3.225 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457365.5 (2015-Dec-09.0) TDB
Reference: JPL 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2136922427798923 5.1676e-08  
q 2.338826642105812 1.5314e-07 au
tp 2458076.229510693149
(2017-Nov-18.72951069)
0.00012582 TDB
node 99.26429295096952 0.0001871 deg
peri 131.0961123001054 0.00018876 deg
i 2.84747306700997 5.91e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      166  
   data-arc span      6409 days (17.55 yr)  
   first obs. used      2002-04-08  
   last obs. used      2019-10-25  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .59255  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-08 14:34:49  

Additional Information
 Jupiter MOID = 1.3867 au 
 T_jup = 3.225 
Orbit Covariance (6×6)
  e q tp node peri i
e 2.670357660335147E-15 -7.816173222240899E-15 -2.241881425056805E-12 3.376965317330374E-14 -4.711164595899886E-13 -1.893253300743097E-15
q -7.816173222240899E-15 2.345080102914607E-14 8.284324802601216E-12 -1.112871453327242E-13 1.689907725058392E-12 6.595492856125875E-15
tp -2.241881425056805E-12 8.284324802601216E-12 1.582990303679311E-8 -1.087141312088447E-10 3.292115442597055E-9 1.0011871307231E-11
node 3.376965317330374E-14 -1.112871453327242E-13 -1.087141312088447E-10 3.500697771609526E-8 -3.498449278404326E-8 5.064388303958459E-10
peri -4.711164595899886E-13 1.689907725058392E-12 3.292115442597055E-9 -3.498449278404326E-8 3.562940123477802E-8 -5.038018758623232E-10
i -1.893253300743097E-15 6.595492856125875E-15 1.0011871307231E-11 5.064388303958459E-10 -5.038018758623232E-10 3.492775637725757E-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 16.6   n/a MPO455941  

413158 (2002 GE64)          Discovered 2002-Apr-08 by NEAT at Palomar
Reference: Last Updated: 2014-11-10

[ show close-approach data ]
Alternate Designations
 2002 GE64 = 2007 ES24 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
ABOUT SSD CREDITS/AWARDS PRIVACY/COPYRIGHT GLOSSARY LINKS
FirstGov 2019-Dec-11 14:37 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin