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79280 (1995 SE32)
Classification: Main-belt Asteroid          SPK-ID: 2079280
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 21 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2269060957799279 3.1176e-08  
a 2.985182451761677 1.5333e-08 au
q 2.307826356441682 9.7373e-08 au
i 2.664639967669723 4.5955e-06 deg
node 175.0761185826793 9.9525e-05 deg
peri 147.382309210779 0.00010036 deg
M 290.9197799240475 1.3273e-05 deg
tp 2459361.998049656810
(2021-May-27.49804966)
7.0549e-05 TDB
period 1883.886555852975
5.16
1.4515e-05
3.974e-08
d
yr
n .191094309198996 1.4723e-09 deg/d
Q 3.662538547081672 1.8813e-08 au
  Orbit Determination Parameters
   # obs. used (total)      981  
   data-arc span      9029 days (24.72 yr)  
   first obs. used      1995-09-21  
   last obs. used      2020-06-10  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .551  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Jun-24 00:02:18  

Additional Information
 Earth MOID = 1.29601 au 
 Jupiter MOID = 1.68631 au 
 T_jup = 3.217 
[ 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 14.7   n/a MPO432342  
diameter diameter 6.465 km 0.410 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.067   0.008 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

79280 (1995 SE32)          Discovered 1995-Sep-21 by Spacewatch at Kitt Peak
Reference: 20040504/Numbers.arcLast Updated: 2004-07-16

[ show close-approach data ]
Alternate Designations
 1995 SE32 = 2000 NN24 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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