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(2020 OO1)
Classification: Apollo [NEO]          SPK-ID: 54048900
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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2521120512211046 3.7004e-05  
a 1.032569764126031 1.4799e-05 au
q .7722464828633251 2.7149e-05 au
i .5328154439908608 8.2895e-05 deg
node 124.7285687742866 0.00010623 deg
peri 280.8098184661663 0.00036272 deg
M 233.9381353536472 0.0059102 deg
tp 2459134.701929053271
(2020-Oct-12.20192905)
0.003407 TDB
period 383.2459133831746
1.05
0.0082389
2.256e-05
d
yr
n .9393446542509301 2.0194e-05 deg/d
Q 1.292893045388737 1.853e-05 au
  Orbit Determination Parameters
   # obs. used (total)      123  
   data-arc span      7 days  
   first obs. used      2020-07-20  
   last obs. used      2020-07-27  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .4438  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Jul-31 06:19:04  

Additional Information
 Earth MOID = 2.73005E-5 au 
 Jupiter MOID = 4.05274 au 
 T_jup = 5.901 
[ 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 26.423   .4533 9 autocmod 2.8

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