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JPL Small-Body Database Browser
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130190 (2000 AG90)
Classification: Jupiter Trojan          SPK-ID: 2130190
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 13 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .04451112606118138 7.6008e-08  
a 5.247368083544633 1.4402e-07 au
q 5.013801821288559 4.659e-07 au
i 14.72302044410583 7.8453e-06 deg
node 292.1060383876807 2.8548e-05 deg
peri 76.93531318958311 8.9273e-05 deg
M 328.4230792685591 8.4447e-05 deg
tp 2458985.603971227514
(2020-May-16.10397123)
0.0010282 TDB
period 4390.467038284221
12.02
0.00018075
4.949e-07
d
yr
n .08199583253008243 3.3757e-09 deg/d
Q 5.480934345800708 1.5043e-07 au
  Orbit Determination Parameters
   # obs. used (total)      431  
   data-arc span      14733 days (40.34 yr)  
   first obs. used      1979-06-15  
   last obs. used      2019-10-16  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .52846  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-07 15:20:55  

Additional Information
 Earth MOID = 4.04716 au 
 Jupiter MOID = .0279896 au 
 T_jup = 2.932 
[ 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 12.0   n/a MPO302662  
diameter diameter 17.168 km 0.654 urn:nasa:pds:neowise_diameters_albedos::2.0[jupiter_trojans] (http://adsabs.harvard.edu/abs/2011ApJ...742...40G)  
geometric albedo albedo 0.114   0.022 urn:nasa:pds:neowise_diameters_albedos::2.0[jupiter_trojans] (http://adsabs.harvard.edu/abs/2011ApJ...742...40G)  

130190 (2000 AG90)          Discovered 2000-Jan-05 by LINEAR at Socorro
Reference: 20060711/Numbers.arcLast Updated: 2006-07-17
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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