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 ]  
185265 (2006 UE128)
Classification: Main-belt Asteroid          SPK-ID: 2185265
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 16 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .08702922799277336 5.008e-08  
a 2.339782400916258 1.5924e-08 au
q 2.136152944893439 1.1399e-07 au
i 4.337544274011742 7.3774e-06 deg
node 31.37145698668757 6.9972e-05 deg
peri 60.01183922501026 8.535e-05 deg
M 226.8089511106516 4.7099e-05 deg
tp 2459484.153316523283
(2021-Sep-26.65331652)
0.00017154 TDB
period 1307.258974235063
3.58
1.3345e-05
3.654e-08
d
yr
n .2753853728261092 2.8113e-09 deg/d
Q 2.543411856939078 1.731e-08 au
  Orbit Determination Parameters
   # obs. used (total)      223  
   data-arc span      7182 days (19.66 yr)  
   first obs. used      1999-10-01  
   last obs. used      2019-05-31  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .56148  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-24 20:02:47  

Additional Information
 Earth MOID = 1.15652 au 
 Jupiter MOID = 2.58639 au 
 T_jup = 3.556 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457007.5 (2014-Dec-16.0) TDB
Reference: JPL 16 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .08781059580431216 5.0395e-08  
q 2.134297016717953 1.1516e-07 au
tp 2456869.046919540832
(2014-Jul-30.54691954)
0.0001677 TDB
node 31.47041099867851 6.989e-05 deg
peri 59.65344786974451 8.4981e-05 deg
i 4.340728310676378 7.3801e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      223  
   data-arc span      7182 days (19.66 yr)  
   first obs. used      1999-10-01  
   last obs. used      2019-05-31  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .56148  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-24 20:02:47  

Additional Information
 Jupiter MOID = 2.58639 au 
 T_jup = 3.556 
Orbit Covariance (6×6)
  e q tp node peri i
e 2.539657336992766E-15 -5.7620095777598E-15 -2.314019326615843E-12 -3.306422858759186E-15 -7.424575407675003E-13 2.097071396413597E-16
q -5.7620095777598E-15 1.32624458570906E-14 5.384941598287474E-12 6.969692451641455E-15 1.726678689814427E-12 -4.576561849036882E-16
tp -2.314019326615843E-12 5.384941598287474E-12 2.812450225426776E-8 -1.142870508155373E-11 8.123135060555119E-9 -2.362758426179841E-11
node -3.306422858759186E-15 6.969692451641455E-15 -1.142870508155373E-11 4.884563930300579E-9 -4.872965944989137E-9 -1.229336555893883E-10
peri -7.424575407675003E-13 1.726678689814427E-12 8.123135060555119E-9 -4.872965944989137E-9 7.221755095732462E-9 1.15871223225627E-10
i 2.097071396413597E-16 -4.576561849036882E-16 -2.362758426179841E-11 -1.229336555893883E-10 1.15871223225627E-10 5.446530299065546E-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 17.2   n/a MPO433215  

185265 (2006 UE128)          Discovered 2006-Oct-19 by NEAT at Palomar
Reference: 20080420/Numbers.arcLast Updated: 2008-04-23

[ show close-approach data ]
Alternate Designations
 2006 UE128 = 1999 TT62 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
ABOUT SSD CREDITS/AWARDS PRIVACY/COPYRIGHT GLOSSARY LINKS
FirstGov 2020-Apr-10 18:43 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin