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 ]  
193114 (2000 GE166)
Classification: Main-belt Asteroid          SPK-ID: 2193114
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 17 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .03396470238842382 4.8568e-08  
a 3.110628313698172 3.5577e-08 au
q 3.004976748782409 1.5117e-07 au
i 14.68002759713549 6.5493e-06 deg
node 204.7803026856159 2.1652e-05 deg
peri 119.760294743955 0.00010125 deg
M 53.82359050177151 9.9045e-05 deg
tp 2458300.900714832041
(2018-Jul-01.40071483)
0.00055059 TDB
period 2003.874911632202
5.49
3.4378e-05
9.412e-08
d
yr
n .1796519323188551 3.0821e-09 deg/d
Q 3.216279878613935 3.6785e-08 au
  Orbit Determination Parameters
   # obs. used (total)      293  
   data-arc span      8442 days (23.11 yr)  
   first obs. used      1996-09-14  
   last obs. used      2019-10-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .54628  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-07 21:43:49  

Additional Information
 Earth MOID = 2.02341 au 
 Jupiter MOID = 1.901 au 
 T_jup = 3.168 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457333.5 (2015-Nov-07.0) TDB
Reference: JPL 17 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .03398091188830588 4.8621e-08  
q 3.008577300418605 1.5155e-07 au
tp 2458277.089909264169
(2018-Jun-07.58990926)
0.00054942 TDB
node 204.8369502458064 2.1703e-05 deg
peri 115.2990032246918 0.00010071 deg
i 14.65236723705051 6.5407e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      293  
   data-arc span      8442 days (23.11 yr)  
   first obs. used      1996-09-14  
   last obs. used      2019-10-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .54628  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-07 21:43:49  

Additional Information
 Jupiter MOID = 1.901 au 
 T_jup = 3.168 
Orbit Covariance (6×6)
  e q tp node peri i
e 2.364019517916105E-15 -7.172032966569097E-15 7.26143753366349E-13 5.251713027959878E-15 1.252908378559014E-13 -2.407318552915766E-15
q -7.172032966569097E-15 2.296615252415291E-14 1.305760093517088E-12 -2.066386862809916E-14 1.440022434192754E-13 7.233764648300865E-15
tp 7.26143753366349E-13 1.305760093517088E-12 3.018654572849367E-7 -8.663126014016287E-11 5.403872000146146E-8 3.996587409800223E-11
node 5.251713027959878E-15 -2.066386862809916E-14 -8.663126014016287E-11 4.710201443899309E-10 -4.708685556637028E-10 1.393506693057148E-11
peri 1.252908378559014E-13 1.440022434192754E-13 5.403872000146146E-8 -4.708685556637028E-10 1.014179028889377E-8 -6.380007072011577E-12
i -2.407318552915766E-15 7.233764648300865E-15 3.996587409800223E-11 1.393506693057148E-11 -6.380007072011577E-12 4.278098287127042E-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 15.2   n/a MPO454339  

193114 (2000 GE166)          Discovered 2000-Apr-05 by LINEAR at Socorro
Reference: 20081113/Numbers.arcLast Updated: 2008-11-17

[ show close-approach data ]
Alternate Designations
 2000 GE166 = 2002 TR80 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
ABOUT SSD CREDITS/AWARDS PRIVACY/COPYRIGHT GLOSSARY LINKS
FirstGov
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin