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35224 (1995 BN1)
Classification: Main-belt Asteroid          SPK-ID: 2035224
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 .1235305139741422 3.4397e-08  
a 2.303497220135308 6.785e-09 au
q 2.018945024593986 7.9084e-08 au
i 2.397647057370107 3.3296e-06 deg
node 77.76930925943029 9.3097e-05 deg
peri 60.32361440463822 9.4176e-05 deg
M 83.67355391489075 1.4374e-05 deg
tp 2458703.698781048819
(2019-Aug-08.19878105)
5.0589e-05 TDB
period 1276.967856906222
3.50
5.642e-06
1.545e-08
d
yr
n .2819178243626204 1.2456e-09 deg/d
Q 2.58804941567663 7.6232e-09 au
  Orbit Determination Parameters
   # obs. used (total)      1293  
   data-arc span      9253 days (25.33 yr)  
   first obs. used      1994-12-28  
   last obs. used      2020-04-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .55002  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-May-20 08:04:02  

Additional Information
 Earth MOID = 1.03372 au 
 Jupiter MOID = 2.42942 au 
 T_jup = 3.578 
[ 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 15.5   n/a MPO417054  
diameter diameter 2.176 km 0.234 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.215   0.044 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

35224 (1995 BN1)          Discovered 1995-Jan-25 by Kobayashi, T. at Oizumi
Reference: 20020227/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1995 BN1 = 1999 HU5 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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