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60375 (2000 AY146)
Classification: Mars-crossing Asteroid          SPK-ID: 2060375
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

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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 .1595287451966657 4.6297e-08  
a 1.920235535254273 7.7778e-09 au
q 1.613902769833111 9.0058e-08 au
i 20.32492966731167 6.1702e-06 deg
node 269.4266232879696 1.3332e-05 deg
peri 84.62011154332377 2.2536e-05 deg
M 349.0956912404434 2.02e-05 deg
tp 2459029.939187513956
(2020-Jun-29.43918751)
5.4605e-05 TDB
period 971.9192420826988
2.66
5.9051e-06
1.617e-08
d
yr
n .3704011448817147 2.2504e-09 deg/d
Q 2.226568300675435 9.0186e-09 au
  Orbit Determination Parameters
   # obs. used (total)      980  
   data-arc span      9806 days (26.85 yr)  
   first obs. used      1993-06-23  
   last obs. used      2020-04-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .45203  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-May-20 11:55:53  

Additional Information
 Earth MOID = .727344 au 
 Jupiter MOID = 3.22005 au 
 T_jup = 3.834 
[ 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 14.9   n/a MPO474485  

60375 (2000 AY146)          Discovered 2000-Jan-08 by LINEAR at Socorro
Reference: 20030614/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 2000 AY146 = 1993 MM1 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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