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17528 (1993 FX14)
Classification: Main-belt Asteroid          SPK-ID: 2017528
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 20 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .09919806058136045 4.7626e-08  
a 3.001926772678559 2.1276e-08 au
q 2.704141458821583 1.4434e-07 au
i 11.12369504738612 5.3746e-06 deg
node 155.6002509347776 2.479e-05 deg
peri 186.4479390267925 3.5799e-05 deg
M 331.0242793417932 2.9345e-05 deg
tp 2459353.408037154916
(2021-May-18.90803715)
0.00015579 TDB
period 1899.759251032771
5.20
2.0197e-05
5.53e-08
d
yr
n .1894976954602497 2.0146e-09 deg/d
Q 3.299712086535535 2.3387e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1001  
   data-arc span      14977 days (41.00 yr)  
   first obs. used      1979-08-22  
   last obs. used      2020-08-23  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .53689  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 02:05:38  

Additional Information
 Earth MOID = 1.69409 au 
 Jupiter MOID = 2.09777 au 
 T_jup = 3.217 
[ 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 14.23   n/a E2021B10  
diameter diameter 5.228 km 0.322 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.135   0.023 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

17528 (1993 FX14)          Discovered 1993-Mar-17 by UESAC at La Silla
Reference: 20001013/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1993 FX14 = 1979 QB3 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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