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(2020 FP5)
Classification: Apollo [NEO]          SPK-ID: 54016378
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 1 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2929540842444238 0.00040476  
a 1.275400050732327 0.00059295 au
q .9017663968247465 9.7719e-05 au
i 5.346602746197174 0.0066246 deg
node 182.6582560362766 0.00015809 deg
peri 304.3095437927004 0.0033868 deg
M 78.36275333088021 0.063043 deg
tp 2458885.981603637770
(2020-Feb-06.48160364)
0.012368 TDB
period 526.0997213347878
1.44
0.36689
0.001004
d
yr
n .6842809174782115 0.0004772 deg/d
Q 1.649033704639908 0.00076666 au
  Orbit Determination Parameters
   # obs. used (total)      15  
   data-arc span      2 days  
   first obs. used      2020-03-24  
   last obs. used      2020-03-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .41985  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Mar-25 21:42:03  

Additional Information
 Earth MOID = .00164434 au 
 Jupiter MOID = 3.41498 au 
 T_jup = 5.022 
[ 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 29.729   .33343 1 autocmod 2.8

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