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100215 (1994 PV5)
Classification: Main-belt Asteroid          SPK-ID: 2100215
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 16 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .112054862313387 3.8792e-08  
a 3.055741229352016 2.1774e-08 au
q 2.713330566631636 1.2352e-07 au
i 1.284334272600897 4.0745e-06 deg
node 236.1200175087934 0.00019319 deg
peri 120.4141145176976 0.00019409 deg
M 279.8830804961899 2.0892e-05 deg
tp 2459434.705209070018
(2021-Aug-08.20520907)
0.00011582 TDB
period 1951.071961245
5.34
2.0853e-05
5.709e-08
d
yr
n .1845139529196454 1.9721e-09 deg/d
Q 3.398151892072396 2.4213e-08 au
  Orbit Determination Parameters
   # obs. used (total)      757  
   data-arc span      9040 days (24.75 yr)  
   first obs. used      1994-08-10  
   last obs. used      2019-05-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .5084  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-May-30 06:34:15  

Additional Information
 Earth MOID = 1.70927 au 
 Jupiter MOID = 2.04054 au 
 T_jup = 3.225 
[ 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 14.8   n/a MPO436466  
diameter diameter 3.441 km 0.716 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.197   0.123 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

100215 (1994 PV5)          Discovered 1994-Aug-10 by Elst, E. W. at La Silla
Reference: 20051019/Numbers.arcLast Updated: 2005-10-26

Alternate Designations
 1994 PV5 = 1997 EO45 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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