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JPL Small-Body Database Browser
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(2017 AE5)
Classification: Apollo [NEO]          SPK-ID: 3766360
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 11 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3384391039067978 8.3479e-08  
a 1.315171687926877 6.2834e-09 au
q .8700661603813141 1.1267e-07 au
i 2.258751334011315 7.4759e-06 deg
node 2.579160957701141 0.00021708 deg
peri 187.9327902384222 0.00022137 deg
M 147.4480536020591 1.3461e-05 deg
tp 2458374.863867684062
(2018-Sep-13.36386768)
1.9844e-05 TDB
period 550.8991515951971
1.51
3.948e-06
1.081e-08
d
yr
n .6534771363462354 4.6831e-09 deg/d
Q 1.76027721547244 8.4099e-09 au
  Orbit Determination Parameters
   # obs. used (total)      115  
   data-arc span      3298 days (9.03 yr)  
   first obs. used      2011-01-11  
   last obs. used      2020-01-22  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .5519  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Jan-23 10:50:57  

Additional Information
 Earth MOID = .0293907 au 
 Jupiter MOID = 3.19693 au 
 T_jup = 4.902 
[ 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 22.3   n/a E2020A55  

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