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15570 (2000 GT60)
Classification: Main-belt Asteroid          SPK-ID: 2015570
[ 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 28 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1288290952702701 3.7142e-08  
a 2.454201571455696 7.7352e-09 au
q 2.138029003394183 9.1902e-08 au
i 1.469503883765751 4.0684e-06 deg
node 185.8003283768775 0.00012444 deg
peri 186.9056358906848 0.00012507 deg
M 287.2222734404716 1.3778e-05 deg
tp 2459284.396315273746
(2021-Mar-10.89631527)		 5.437e-05 TDB
period 1404.312532556948
3.84		 6.6392e-06
1.818e-08		 d
yr
n .2563531917959304 1.212e-09 deg/d
Q 2.770374139517207 8.7318e-09 au
   Orbit Determination Parameters
   # obs. used (total)      1859  
   data-arc span      15313 days (41.92 yr)  
   first obs. used      1978-09-03  
   last obs. used      2020-08-06  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .54081  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Aug-25 01:00:38  

Additional Information
 Earth MOID = 1.13824 au 
 Jupiter MOID = 2.69373 au 
 T_jup = 3.482 
[ 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 14.4   n/a MPO473976  
diameter diameter 8.194 km 0.045 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.050   0.007 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

15570 (2000 GT60)          Discovered 2000-Apr-05 by LINEAR at Socorro
Reference: 20000621/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 2000 GT60 = 1978 RP3 = 1982 SP8 = 1998 YG4 
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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