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17515 (1992 UT1)
Classification: Main-belt Asteroid          SPK-ID: 2017515
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 25 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1483228855727247 3.6986e-08  
a 2.519230277099746 9.371e-09 au
q 2.145570772978137 9.5179e-08 au
i 4.58966005323409 5.1959e-06 deg
node 82.98460222986239 5.0851e-05 deg
peri 212.95162689 5.4558e-05 deg
M 44.32996954789297 2.052e-05 deg
tp 2458820.656328599860
(2019-Dec-03.15632860)
8.3097e-05 TDB
period 1460.495514983448
4.00
8.1491e-06
2.231e-08
d
yr
n .2464916847102266 1.3753e-09 deg/d
Q 2.892889781221355 1.0761e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1913  
   data-arc span      11249 days (30.80 yr)  
   first obs. used      1988-11-03  
   last obs. used      2019-08-22  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .51158  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Sep-24 01:24:21  

Additional Information
 Earth MOID = 1.1313 au 
 Jupiter MOID = 2.29296 au 
 T_jup = 3.437 
[ 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 13.7   n/a MPO347661  
diameter diameter 3.793 km 0.397 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.407   0.206 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

17515 (1992 UT1)          Discovered 1992-Oct-21 by Sugie, A. at Dynic
Reference: 20001013/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 1992 UT1 = 1988 VJ12 = 1996 VX7 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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