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(2019 AS5)
Classification: Apollo [NEO]          SPK-ID: 3837685
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 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3922955234887866 3.0626e-05  
a 1.347930404267488 5.1157e-05 au
q .819143340698922 1.02e-05 au
i .701421166377695 5.5712e-05 deg
node 106.7480060704284 6.7024e-05 deg
peri 294.3618740817697 0.00026796 deg
M 350.708779241361 0.020483 deg
tp 2459015.252645591867
(2020-Jun-14.75264559)
0.033364 TDB
period 571.6097540933116
1.56
0.032541
8.909e-05
d
yr
n .6298003094279464 3.5854e-05 deg/d
Q 1.876717467836054 7.1226e-05 au
  Orbit Determination Parameters
   # obs. used (total)      20  
   data-arc span      3 days  
   first obs. used      2019-01-08  
   last obs. used      2019-01-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .41451  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Mar-12 06:04:19  

Additional Information
 Earth MOID = 9.99695E-5 au 
 Jupiter MOID = 3.53917 au 
 T_jup = 4.797 
[ 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 32.3   .38061 MPO467332 autocmod 2.6q

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