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43562 (2001 FE97)
Classification: Main-belt Asteroid          SPK-ID: 2043562
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 34 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .09795581178479096 5.2864e-08  
a 3.082649588084025 1.92e-08 au
q 2.780686145235203 1.6736e-07 au
i 13.17140106572584 4.957e-06 deg
node 55.00604700549459 1.9133e-05 deg
peri 120.996053071456 2.8246e-05 deg
M 243.1345300463492 2.1628e-05 deg
tp 2459842.253692764178
(2022-Sep-19.75369276)
0.00012118 TDB
period 1976.899844639583
5.41
1.847e-05
5.057e-08
d
yr
n .1821033073456653 1.7013e-09 deg/d
Q 3.384613030932847 2.1081e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1273  
   data-arc span      9075 days (24.85 yr)  
   first obs. used      1996-05-14  
   last obs. used      2021-03-19  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .56575  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-May-04 05:26:10  

Additional Information
 Earth MOID = 1.80832 au 
 Jupiter MOID = 1.66203 au 
 T_jup = 3.180 
[ 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 13.92   n/a MPCxxxxx  
diameter diameter 6.665 km 0.353 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.132   0.016 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

43562 (2001 FE97)          Discovered 2001-Mar-16 by LINEAR at Socorro
Reference: 20020624/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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