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17667 (1996 XT5)
Classification: Main-belt Asteroid          SPK-ID: 2017667
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 24 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .05777062288086528 4.3288e-08  
a 2.980447702692921 1.981e-08 au
q 2.808265382444507 1.2083e-07 au
i 8.775649844164521 4.3808e-06 deg
node 289.6008098276071 2.9011e-05 deg
peri 180.29387488429 4.9394e-05 deg
M 193.4763118566146 4.0475e-05 deg
tp 2459869.849093792723
(2022-Oct-17.34909379)
0.00021309 TDB
period 1879.406331043431
5.15
1.8738e-05
5.13e-08
d
yr
n .1915498495741105 1.9098e-09 deg/d
Q 3.152630022941335 2.0955e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1629  
   data-arc span      10507 days (28.77 yr)  
   first obs. used      1990-10-24  
   last obs. used      2019-07-31  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .48581  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Jan-29 00:32:38  

Additional Information
 Earth MOID = 1.82496 au 
 Jupiter MOID = 1.95362 au 
 T_jup = 3.239 
[ 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 13.4   n/a MPO347662  
diameter diameter 6.968 km 0.361 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.191   0.027 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

17667 (1996 XT5)          Discovered 1996-Dec-07 by Kobayashi, T. at Oizumi
Reference: 20001013/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 1996 XT5 = 1994 NY3 = 1996 BO17 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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