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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 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2521122095742922 3.6892e-05  
a 1.032569811503956 1.4755e-05 au
q .772246354785983 2.7066e-05 au
i .5328157984371845 8.2655e-05 deg
node 124.7285684544341 0.00010609 deg
peri 280.8098203291688 0.00036155 deg
M 233.9381558901765 0.0058926 deg
tp 2459134.701916427139
(2020-Oct-12.20191643)
0.0033968 TDB
period 383.2459397601763
1.05
0.0082144
2.249e-05
d
yr
n .9393445896002892 2.0134e-05 deg/d
Q 1.292893268221929 1.8474e-05 au
  Orbit Determination Parameters
   # obs. used (total)      125  
   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      .44243  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Sep-13 07:22:40  

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 26.424   .45149 10 autocmod 2.8

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