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15528 (2000 AJ10)
Classification: Main-belt Asteroid          SPK-ID: 2015528
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 29 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1924911323143926 3.7206e-08  
a 2.198780556294001 5.38e-09 au
q 1.775534797302099 8.1687e-08 au
i 4.320071714275395 3.6619e-06 deg
node 286.3240921283798 4.5079e-05 deg
peri 20.87923588326735 4.5752e-05 deg
M 200.2815547727795 8.2978e-06 deg
tp 2459528.852579213719
(2021-Nov-10.35257921)
2.8273e-05 TDB
period 1190.888931120914
3.26
4.3708e-06
1.197e-08
d
yr
n .3022951936089901 1.1095e-09 deg/d
Q 2.622026315285904 6.4156e-09 au
  Orbit Determination Parameters
   # obs. used (total)      1491  
   data-arc span      10118 days (27.70 yr)  
   first obs. used      1992-08-06  
   last obs. used      2020-04-19  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .51743  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-May-20 04:12:14  

Additional Information
 Earth MOID = .761382 au 
 Jupiter MOID = 2.62293 au 
 T_jup = 3.639 
[ 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 15.1   n/a MPO347647  

15528 (2000 AJ10)          Discovered 2000-Jan-03 by LINEAR at Socorro
Reference: 20000621/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 2000 AJ10 = 1992 PK3 = 1997 AX23 = 1998 FJ117 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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