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65444 (2002 UO29)
Classification: Main-belt Asteroid          SPK-ID: 2065444
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 17 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .156737201412821 4.1644e-08  
a 2.319477378679802 1.2706e-08 au
q 1.955928985605184 9.5929e-08 au
i 7.533039155672606 4.5544e-06 deg
node 110.8640216285144 4.4411e-05 deg
peri 220.938497983207 4.8343e-05 deg
M 54.03611207756538 2.1767e-05 deg
tp 2458806.828715998386
(2019-Nov-19.32871600)
7.7173e-05 TDB
period 1290.279029336899
3.53
1.0602e-05
2.903e-08
d
yr
n .2790094171994809 2.2926e-09 deg/d
Q 2.683025771754421 1.4697e-08 au
  Orbit Determination Parameters
   # obs. used (total)      511  
   data-arc span      8098 days (22.17 yr)  
   first obs. used      1995-12-26  
   last obs. used      2018-02-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .59821  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Mar-05 19:32:14  

Additional Information
 Earth MOID = .951614 au 
 Jupiter MOID = 2.65637 au 
 T_jup = 3.551 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456561.5 (2013-Sep-26.0) TDB
Reference: JPL 17 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .156117677414939 4.1509e-08  
q 1.958353209136958 9.549e-08 au
tp 2456225.861244775954
(2012-Oct-25.36124478)
6.9323e-05 TDB
node 110.9053165644237 4.4426e-05 deg
peri 221.0131962566069 4.8433e-05 deg
i 7.530279890762453 4.5545e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      511  
   data-arc span      8098 days (22.17 yr)  
   first obs. used      1995-12-26  
   last obs. used      2018-02-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .59821  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Mar-05 19:32:14  

Additional Information
 Jupiter MOID = 2.65637 au 
 T_jup = 3.551 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.723013380491483E-15 -3.938778092475117E-15 6.466479930490373E-13 2.688452203211707E-15 1.974612427954146E-13 1.344329721407282E-15
q -3.938778092475117E-15 9.118337646510437E-15 -1.295291994854949E-12 -5.885600929702938E-15 -3.965868838833716E-13 -2.877938835353837E-15
tp 6.466479930490373E-13 -1.295291994854949E-12 4.805744283160087E-9 -3.146754852301892E-11 1.375636758697562E-9 2.45193569935602E-12
node 2.688452203211707E-15 -5.885600929702938E-15 -3.146754852301892E-11 1.973704031930942E-9 -1.964901850411687E-9 -3.412031807149513E-11
peri 1.974612427954146E-13 -3.965868838833716E-13 1.375636758697562E-9 -1.964901850411687E-9 2.345741528158246E-9 3.455080391761258E-11
i 1.344329721407282E-15 -2.877938835353837E-15 2.45193569935602E-12 -3.412031807149513E-11 3.455080391761258E-11 2.074322868487584E-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 15.9   n/a MPO436238  

65444 (2002 UO29)          Discovered 2002-Oct-31 by NEAT at Palomar
Reference: 20030614/Numbers.arcLast Updated: 2004-04-19

[ hide close-approach data ]
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
2101-Jul-15 21:23 < 00:01 Juno 0.047780523496574 0.0477609253169169 0.047800121678637 6.46300264452367 6.46300260512689 2488630.390761905 0.522022629115075 976.987315022202 49.8591742961014 -0.844629437109477 7611.06952399142 T 17 CATAB v2.0e-lin.ifort 2018-Mar-05 19:32:21 2018-Dec-17 17:01
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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