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(2020 PG6)
Classification: Apollo [NEO]          SPK-ID: 54051164
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 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2530446645242467 8.124e-05  
a 1.177706439767116 8.7456e-05 au
q .8796941088082012 3.0354e-05 au
i 4.868995759056975 0.0014808 deg
node 158.2561725295035 0.00032308 deg
peri 248.6627297102737 0.00083321 deg
M 244.3194092671086 0.016043 deg
tp 2459150.507163332724
(2020-Oct-28.00716333)
0.0040951 TDB
period 466.8248878886995
1.28
0.051999
0.0001424
d
yr
n .7711671107086117 8.59e-05 deg/d
Q 1.475718770726031 0.00010959 au
  Orbit Determination Parameters
   # obs. used (total)      30  
   data-arc span      22 days  
   first obs. used      2020-08-11  
   last obs. used      2020-09-02  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .81526  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Sep-03 08:17:52  

Additional Information
 Earth MOID = .000257012 au 
 Jupiter MOID = 3.88691 au 
 T_jup = 5.335 
[ hide covariance matrix ]
Orbital Elements at Epoch 2459080.5 (2020-Aug-19.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2532144321815153 8.1119e-05  
q .8795705664053215 3.0252e-05 au
tp 2459150.492764558803
(2020-Oct-27.99276456)
0.0040803 TDB
node 158.2371165257146 0.00030715 deg
peri 248.6813892677077 0.00084657 deg
i 4.872282073901268 0.0014789 deg
  Orbit Determination Parameters
   # obs. used (total)      30  
   data-arc span      22 days  
   first obs. used      2020-08-11  
   last obs. used      2020-09-02  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .81526  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Sep-03 08:17:52  

Additional Information
 Jupiter MOID = 3.88691 au 
 T_jup = 5.335 
Orbit Covariance (6×6)
  e q tp node peri i
e 6.580236949248474E-9 -2.453826369853805E-9 -3.309408986410854E-7 -2.489910328034796E-8 -6.815399622563654E-8 1.199668709716867E-7
q -2.453826369853805E-9 9.151698931277808E-10 1.233876849305702E-7 9.286858923334552E-9 2.537975760209289E-8 -4.473814988309353E-8
tp -3.309408986410854E-7 1.233876849305702E-7 1.664863253468415E-5 1.25194974828825E-6 3.43464223654094E-6 -6.033218420054366E-6
node -2.489910328034796E-8 9.286858923334552E-9 1.25194974828825E-6 9.434236544126281E-8 2.572911628262255E-7 -4.539881403247517E-7
peri -6.815399622563654E-8 2.537975760209289E-8 3.43464223654094E-6 2.572911628262255E-7 7.166888763415929E-7 -1.242070577948423E-6
i 1.199668709716867E-7 -4.473814988309353E-8 -6.033218420054366E-6 -4.539881403247517E-7 -1.242070577948423E-6 2.187197627483397E-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 26.956   .2988 8 autocmod 2.8

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Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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