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17580 (1994 VV)
Classification: Main-belt Asteroid          SPK-ID: 2017580
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 35 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .06281931048221565 2.5244e-08  
a 2.646528095720063 1.1449e-08 au
q 2.480275025575118 6.7749e-08 au
i 21.14155026384552 7.0301e-07 deg
node 245.0228487725481 3.1039e-06 deg
peri 194.0820024197602 1.9286e-05 deg
M 5.8261857497238 1.7334e-05 deg
tp 2459175.049576351365
(2020-Nov-21.54957635)
7.5728e-05 TDB
period 1572.581600911522
4.31
1.0205e-05
2.794e-08
d
yr
n .2289229377930733 1.4856e-09 deg/d
Q 2.812781165865009 1.2169e-08 au
  Orbit Determination Parameters
   # obs. used (total)      2051  
   data-arc span      15347 days (42.02 yr)  
   first obs. used      1979-03-09  
   last obs. used      2021-03-15  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .4452  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 02:07:05  

Additional Information
 Earth MOID = 1.49682 au 
 Jupiter MOID = 2.50482 au 
 T_jup = 3.294 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 13.35   n/a E2021B10  
diameter diameter 5.353 km 0.265 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.355   0.093 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

17580 (1994 VV)          Discovered 1994-Nov-03 by Kobayashi, T. at Oizumi
Reference: 20001013/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1994 VV = 1999 AH37 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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