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(2017 FO127)
Classification: Apollo [NEO]          SPK-ID: 3773596
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 2 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2190521318446452 0.00037241  
a 1.126775086491013 0.0003164 au
q .8799526016857222 0.00017275 au
i 4.744009452193732 0.0078567 deg
node 178.4873272728452 0.0020762 deg
peri 90.35561218804125 0.0023925 deg
M 177.8444241016585 0.36227 deg
tp 2458784.679828405391
(2019-Oct-28.17982841)
0.34873 TDB
period 436.8720704431391
1.20
0.18401
0.0005038
d
yr
n .8240398605359132 0.00034709 deg/d
Q 1.373597571296304 0.00038571 au
  Orbit Determination Parameters
   # obs. used (total)      12  
   data-arc span      2 days  
   first obs. used      2017-03-28  
   last obs. used      2017-03-30  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .51227  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:18:56  

Additional Information
 Earth MOID = .0225531 au 
 Jupiter MOID = 3.69718 au 
 T_jup = 5.523 
[ 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 26.8   n/a MPO405767  

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