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59395 (1999 FM25)
Classification: Main-belt Asteroid          SPK-ID: 2059395
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 25 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1450710216025966 5.2198e-08  
a 2.443389349609005 1.2084e-08 au
q 2.088924360488323 1.2815e-07 au
i 7.130460675677631 4.9412e-06 deg
node 42.53852395453285 4.074e-05 deg
peri 139.1294031028138 4.3009e-05 deg
M 201.4080640018065 1.5356e-05 deg
tp 2459615.062478957784
(2022-Feb-04.56247896)
6.1256e-05 TDB
period 1395.042509773779
3.82
1.0349e-05
2.833e-08
d
yr
n .2580566523799893 1.9144e-09 deg/d
Q 2.797854338729687 1.3838e-08 au
  Orbit Determination Parameters
   # obs. used (total)      735  
   data-arc span      7523 days (20.60 yr)  
   first obs. used      1999-03-19  
   last obs. used      2019-10-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .53792  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-23 12:47:08  

Additional Information
 Earth MOID = 1.09662 au 
 Jupiter MOID = 2.16774 au 
 T_jup = 3.475 
[ 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 15.6   n/a MPO436197  
diameter diameter 1.758 km 0.238 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.433   0.096 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

59395 (1999 FM25)          Discovered 1999-Mar-19 by LINEAR at Socorro
Reference: 20030614/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1999 FM25 = 2001 VS110 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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