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JPL Small-Body Database Browser
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74709 (1999 RU151)
Classification: Main-belt Asteroid          SPK-ID: 2074709
[ 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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 16 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1049709716361357 4.0889e-08  
a 2.230838760547607 9.0569e-09 au
q 1.996665448289373 9.3016e-08 au
i 2.056642127837287 5.3937e-06 deg
node 32.24191593656325 0.00010299 deg
peri 294.8292007207576 0.00010589 deg
M 332.5581736315283 2.3312e-05 deg
tp 2458693.270780572536
(2019-Jul-28.77078057)		 7.8633e-05 TDB
period 1217.028362386397
3.33		 7.4115e-06
2.029e-08		 d
yr
n .2958024735710332 1.8014e-09 deg/d
Q 2.465012072805842 1.0008e-08 au
   Orbit Determination Parameters
   # obs. used (total)      699  
   data-arc span      8441 days (23.11 yr)  
   first obs. used      1996-10-11  
   last obs. used      2019-11-21  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .53026  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Dec-14 07:27:04  

Additional Information
 Earth MOID = .985211 au 
 Jupiter MOID = 2.79488 au 
 T_jup = 3.634 
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[ 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 16.2   n/a MPO344829  

74709 (1999 RU151)          Discovered 1999-Sep-09 by LINEAR at Socorro
Reference: 20040415/Numbers.arcLast Updated: 2004-04-19

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Alternate Designations
 1999 RU151 = 1996 TF36 
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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