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185265 (2006 UE128)
Classification: Main-belt Asteroid          SPK-ID: 2185265
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 17 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .08702924080462417 4.2657e-08  
a 2.339782404267819 1.4463e-08 au
q 2.136152917976373 9.9678e-08 au
i 4.337540174964895 6.624e-06 deg
node 31.37145325846441 6.9923e-05 deg
peri 60.01183461696221 8.2791e-05 deg
M 226.808957066815 4.4406e-05 deg
tp 2459484.153295934011
(2021-Sep-26.65329593)
0.00016251 TDB
period 1307.258977043887
3.58
1.2121e-05
3.319e-08
d
yr
n .2753853722344062 2.5534e-09 deg/d
Q 2.543411890559266 1.5722e-08 au
  Orbit Determination Parameters
   # obs. used (total)      231  
   data-arc span      7607 days (20.83 yr)  
   first obs. used      1999-10-01  
   last obs. used      2020-07-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .55766  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Aug-25 13:43:40  

Additional Information
 Earth MOID = 1.15652 au 
 Jupiter MOID = 2.58639 au 
 T_jup = 3.556 
[ 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 17.2   n/a MPO433215  

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

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Close-Approach Data   ...sorted by Date/Time (TDB)
Date/Time (TDB) Time Uncertainty
(days_HH:MM)
Body Nominal Distance (au) Minimum Distance (au) Maximum Distance (au) V-relative (km/s) V-infinity (km/s) JD (TDB) Time Uncertainty (minutes) Semi-major axis (km) Semi-minor axis (km) range-LOV angle (deg) N-sigma BP Orbit Ref. Reference Modified
2073-May-05 19:37 00:04 Thisb 0.0245407837444963 0.0245161510795644 0.0245654179726475 4.39248893438352 4.39248887113132 2478333.317465876 3.57795200958262 1266.29540014384 117.245064332737 -14.2314149500732 8190.11677725423 T 17 CATAB v2.0f-lin.ifort 2020-Aug-25 13:43:41 2020-Aug-25 13:43

Alternate Designations
 2006 UE128 = 1999 TT62 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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