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(2020 AO)
Classification: Apollo [NEO]          SPK-ID: 3972415
[ 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.


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Orbital Elements at Epoch 2458851.5 (2020-Jan-03.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6068604080836143 0.0025321  
a 1.422749196299142 0.0063671 au
q .5593390384324105 0.0010994 au
i 5.672590874149955 0.021626 deg
node 307.5128896335316 0.010089 deg
peri 264.384520646609 0.0095297 deg
M 323.902493874513 0.30607 deg
tp 2458913.653508379660
(2020-Mar-05.15350838)		 0.10977 TDB
period 619.8562011152163
1.70		 4.161
0.01139		 d
yr
n .5807798637043637 0.0038987 deg/d
Q 2.286159354165874 0.010231 au
   Orbit Determination Parameters
   # obs. used (total)      42  
   data-arc span      7 days  
   first obs. used      2020-01-01  
   last obs. used      2020-01-08  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      9  
   norm. resid. RMS      .50031  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Jan-08 06:23:49  

Additional Information
 Earth MOID = .00902613 au 
 Jupiter MOID = 2.71023 au 
 T_jup = 4.484 
[ 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 24.3   .36265 E2020A86 autocmod 2.8

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