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67289 (2000 GQ47)
Classification: Main-belt Asteroid          SPK-ID: 2067289
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 28 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1397422429392202 3.0178e-08  
a 2.326367377192836 8.2793e-09 au
q 2.001275582003278 6.9626e-08 au
i 9.079331897656436 4.3634e-06 deg
node 208.0128427257361 2.2675e-05 deg
peri 253.7004824330733 2.9002e-05 deg
M 78.50109173783356 1.6638e-05 deg
tp 2459113.888993758669
(2020-Sep-21.38899376)
5.9904e-05 TDB
period 1296.03244992637
3.55
6.9187e-06
1.894e-08
d
yr
n .2777708228065219 1.4828e-09 deg/d
Q 2.651459172382394 9.4363e-09 au
  Orbit Determination Parameters
   # obs. used (total)      937  
   data-arc span      8291 days (22.70 yr)  
   first obs. used      1998-09-26  
   last obs. used      2021-06-08  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .52817  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Jul-08 22:35:17  

Additional Information
 Earth MOID = 1.03992 au 
 Jupiter MOID = 2.54757 au 
 T_jup = 3.544 
[ 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 15.95   n/a MPCxxxxx  
diameter diameter 1.666 km 0.280 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.334   0.110 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

67289 (2000 GQ47)          Discovered 2000-Apr-05 by LINEAR at Socorro
Reference: 20030910/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 2000 GQ47 = 1998 SF159 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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