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(2020 AE1)
Classification: Apollo [NEO]          SPK-ID: 3973544
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | 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.


Orbital Elements at Epoch 2458852.5 (2020-Jan-04.0) TDB
Reference: JPL 1 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2353898608809961 0.0014257  
a 1.289617984403593 0.0021081 au
q .9860549864652004 0.0002416 au
i 4.434498837402137 0.0080502 deg
node 283.3844225974667 0.0012711 deg
peri 206.7804726533805 0.099356 deg
M 342.8212385353791 0.016973 deg
tp 2458878.025802043625
(2020-Jan-29.52580204)		 0.07156 TDB
period 534.921493300319
1.46		 1.3117
0.003591		 d
yr
n .6729959526937284 0.0016502 deg/d
Q 1.593180982341985 0.0026044 au
   Orbit Determination Parameters
   # obs. used (total)      19  
   first obs. used      2020-01-04  
   last obs. used      2020-01-04  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .42993  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Jan-04 15:12:10  

Additional Information
 Earth MOID = .0166207 au 
 Jupiter MOID = 3.45351 au 
 T_jup = 5.000 
[ show covariance matrix ]

[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 27.6   .59931 E2020A63 autocmod 2.8

[ show close-approach data ]
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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