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5504 Lanzerotti (1985 FC2)
Classification: Main-belt Asteroid          SPK-ID: 2005504
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 37 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .07275727358310818 2.1366e-08  
a 2.614162376930036 1.0895e-08 au
q 2.42396304968107 5.4155e-08 au
i 13.66495449679074 8.7212e-07 deg
node 60.1625545224376 1.425e-06 deg
peri 133.5757164770874 1.0524e-05 deg
M 155.470375400368 9.9516e-06 deg
tp 2458533.781642346249
(2019-Feb-19.28164235)
4.0955e-05 TDB
period 1543.822147063408
4.23
9.6509e-06
2.642e-08
d
yr
n .233187482563828 1.4577e-09 deg/d
Q 2.804361704179003 1.1687e-08 au
  Orbit Determination Parameters
   # obs. used (total)      2253  
   data-arc span      26009 days (71.21 yr)  
   first obs. used      1949-11-19  
   last obs. used      2021-02-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .39239  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Mar-16 17:48:51  

Additional Information
 Earth MOID = 1.43629 au 
 Jupiter MOID = 2.19898 au 
 T_jup = 3.364 
[ 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 12.69   n/a E2021B10  
diameter diameter 7.167 km 0.036 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2014ApJ...791..121M)  
geometric albedo albedo 0.261   0.035 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2014ApJ...791..121M)  

5504 Lanzerotti (1985 FC2)          Discovered 1985-Mar-22 by Bowell, E. at Flagstaff
Reference: DISCOVERY.DBLast Updated: 2003-08-29

[ show close-approach data ]
Alternate Designations
 1985 FC2 = 1991 RJ25 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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