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(2020 MF1)
Classification: Apollo [NEO]          SPK-ID: 54017566
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 2459020.5 (2020-Jun-20.0) TDB
Reference: JPL 2 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5222874430837 0.0012279  
a 1.93299669724752 0.0046476 au
q .9234167947528757 0.00015332 au
i 1.081427029927681 0.0017762 deg
node 105.0638737995909 0.0032211 deg
peri 213.8848974168498 0.0012298 deg
M 344.9287637811077 0.060302 deg
tp 2459061.595235247221
(2020-Jul-31.09523525)
0.016217 TDB
period 981.6238345766525
2.69
3.5403
0.009693
d
yr
n .3667392613335007 0.0013227 deg/d
Q 2.942576599742164 0.007075 au
  Orbit Determination Parameters
   # obs. used (total)      15  
   data-arc span      9 days  
   first obs. used      2020-06-17  
   last obs. used      2020-06-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .55723  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Jul-03 09:39:15  

Additional Information
 Earth MOID = .00295132 au 
 Jupiter MOID = 2.39644 au 
 T_jup = 3.731 
[ hide covariance matrix ]
Orbit Covariance (6×6)
  e q tp node peri i
e 1.507764725270334E-6 -1.882638744823643E-7 -1.991239134551984E-5 3.933602115366514E-6 -1.464202102573157E-6 2.180890399673708E-6
q -1.882638744823643E-7 2.350721947032546E-8 2.486310385643386E-6 -4.911994070816552E-7 1.82851136088862E-7 -2.72310207871302E-7
tp -1.991239134551984E-5 2.486310385643386E-6 .0002629760757193065 -5.193880031702218E-5 1.932889734997904E-5 -2.880263929495416E-5
node 3.933602115366514E-6 -4.911994070816552E-7 -5.193880031702218E-5 1.037537013463519E-5 -3.920063131253759E-6 5.683236035932878E-6
peri -1.464202102573157E-6 1.82851136088862E-7 1.932889734997904E-5 -3.920063131253759E-6 1.512318289344732E-6 -2.112096044318239E-6
i 2.180890399673708E-6 -2.72310207871302E-7 -2.880263929495416E-5 5.683236035932878E-6 -2.112096044318239E-6 3.154907003805863E-6

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 27.579   .22086 2 autocmod 2.8

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