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15598 (2000 GP96)
Classification: Main-belt Asteroid          SPK-ID: 2015598
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 31 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .165060752038473 3.3229e-08  
a 2.620553370606224 7.4873e-09 au
q 2.188002860497005 8.7138e-08 au
i 2.547953360824356 3.7706e-06 deg
node 27.99140408581526 6.5314e-05 deg
peri 147.2160348455783 6.5966e-05 deg
M 345.1360521084843 9.4845e-06 deg
tp 2459264.476372813670
(2021-Feb-18.97637281)
4.09e-05 TDB
period 1549.487012536393
4.24
6.6407e-06
1.818e-08
d
yr
n .2323349580134314 9.9572e-10 deg/d
Q 3.053103880715442 8.7232e-09 au
  Orbit Determination Parameters
   # obs. used (total)      1989  
   data-arc span      12421 days (34.01 yr)  
   first obs. used      1987-03-21  
   last obs. used      2021-03-23  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .50445  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-May-04 02:04:53  

Additional Information
 Earth MOID = 1.19266 au 
 Jupiter MOID = 1.90829 au 
 T_jup = 3.384 
[ 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 14.30   n/a MPCxxxxx  
diameter diameter 7.548 km 1.830 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2017AJ....154..168M)  
geometric albedo albedo 0.068   0.036 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2017AJ....154..168M)  

15598 (2000 GP96)          Discovered 2000-Apr-06 by LINEAR at Socorro
Reference: 20000621/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 2000 GP96 = 1987 FY = 1991 CR6 = 1991 CT3 = 1997 PA1 = 1998 XM67 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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