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80517 (2000 AM59)
Classification: Main-belt Asteroid          SPK-ID: 2080517
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer was implemented using two-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances.


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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 19 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1611162232854962 7.1496e-08  
a 2.362485512991115 1.4316e-08 au
q 1.981850769571288 1.651e-07 au
i 9.526467640353921 5.5408e-06 deg
node 304.1643512945463 3.2657e-05 deg
peri 75.46275566909129 3.6954e-05 deg
M 307.0993417905925 2.0407e-05 deg
tp 2459195.399503558221
(2020-Dec-11.89950356)
7.6221e-05 TDB
period 1326.331725462012
3.63
1.2055e-05
3.3e-08
d
yr
n .2714253101912331 2.4671e-09 deg/d
Q 2.743120256410941 1.6622e-08 au
  Orbit Determination Parameters
   # obs. used (total)      662  
   data-arc span      7592 days (20.79 yr)  
   first obs. used      1998-08-17  
   last obs. used      2019-05-31  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .54177  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-23 19:00:13  

Additional Information
 Earth MOID = 1.0083 au 
 Jupiter MOID = 2.80863 au 
 T_jup = 3.514 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456903.5 (2014-Sep-03.0) TDB
Reference: JPL 19 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1614983156877075 7.1335e-08  
q 1.981245049023998 1.6505e-07 au
tp 2456544.846704636038
(2013-Sep-09.34670464)
6.5339e-05 TDB
node 304.2264969059517 3.2675e-05 deg
peri 75.79438207295236 3.695e-05 deg
i 9.523791589313694 5.5388e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      662  
   data-arc span      7592 days (20.79 yr)  
   first obs. used      1998-08-17  
   last obs. used      2019-05-31  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .54177  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-23 19:00:13  

Additional Information
 Jupiter MOID = 2.80863 au 
 T_jup = 3.514 
Orbit Covariance (6×6)
  e q tp node peri i
e 5.088711606367345E-15 -1.174740894073148E-14 8.634520163478269E-13 -2.005069723619511E-14 -2.32242041076856E-14 -5.328587036486606E-15
q -1.174740894073148E-14 2.724046938260518E-14 -1.808747823188602E-12 4.349648876570428E-14 1.097200648723686E-13 1.21528297629895E-14
tp 8.634520163478269E-13 -1.808747823188602E-12 4.269185418697923E-9 -3.176995564081768E-11 1.129958926815805E-9 -7.395356002407995E-12
node -2.005069723619511E-14 4.349648876570428E-14 -3.176995564081768E-11 1.067668734789601E-9 -1.060154030523205E-9 2.020369094374118E-11
peri -2.32242041076856E-14 1.097200648723686E-13 1.129958926815805E-9 -1.060154030523205E-9 1.365316632626007E-9 -2.165481619556214E-11
i -5.328587036486606E-15 1.21528297629895E-14 -7.395356002407995E-12 2.020369094374118E-11 -2.165481619556214E-11 3.06777751834991E-11

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 15.3   n/a MPO320003  
diameter diameter 4.567 km 1.487 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2015ApJ...814..117N)  
geometric albedo albedo 0.064   0.050 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2015ApJ...814..117N)  

80517 (2000 AM59)          Discovered 2000-Jan-04 by LINEAR at Socorro
Reference: 20040504/Numbers.arcLast Updated: 2004-07-16

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Alternate Designations
 2000 AM59 = 2002 PE41 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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