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17596 (1995 EP1)
Classification: Main-belt Asteroid          SPK-ID: 2017596
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 25 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .103479347545776 5.249e-08  
a 2.864069998933482 1.5321e-08 au
q 2.567697904118414 1.547e-07 au
i 11.87779180670158 5.3176e-06 deg
node 349.7098253412639 2.1979e-05 deg
peri 209.3820465654535 3.1913e-05 deg
M 54.41975180914265 2.4632e-05 deg
tp 2458732.874232979689
(2019-Sep-06.37423298)
0.00012072 TDB
period 1770.410061133827
4.85
1.4206e-05
3.889e-08
d
yr
n .2033427214989077 1.6316e-09 deg/d
Q 3.16044209374855 1.6906e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1562  
   data-arc span      32187 days (88.12 yr)  
   first obs. used      1932-03-14  
   last obs. used      2020-04-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .50433  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-May-20 04:38:18  

Additional Information
 Earth MOID = 1.57408 au 
 Jupiter MOID = 1.83272 au 
 T_jup = 3.261 
[ 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 13.2   n/a MPO395172  
diameter diameter 6.340 km 0.208 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.253   0.031 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

17596 (1995 EP1)          Discovered 1995-Mar-11 by Kobayashi, T. at Oizumi
Reference: 20001013/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 1995 EP1 = 1932 EQ = 1990 EP6 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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