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(2020 VZ6)
Classification: Apollo [NEO]          SPK-ID: 54096685
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

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.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .532927014500039 3.5336e-05  
a 2.009489335146291 0.00014769 au
q .9385781830971102 2.0239e-06 au
i .4842895332093373 7.2597e-05 deg
node 238.1819756972924 0.0013863 deg
peri 223.9916169237563 0.0013979 deg
M 356.5136650200629 0.00049755 deg
tp 2459210.576126192812
(2020-Dec-27.07612619)
0.00032738 TDB
period 1040.463825274152
2.85
0.11471
0.0003141
d
yr
n .3459995352602898 3.8146e-05 deg/d
Q 3.080400487195472 0.0002264 au
  Orbit Determination Parameters
   # obs. used (total)      76  
   data-arc span      21 days  
   first obs. used      2020-11-14  
   last obs. used      2020-12-05  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .44729  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Dec-06 05:25:14  

Additional Information
 Earth MOID = .00190404 au 
 Jupiter MOID = 2.10604 au 
 T_jup = 3.641 
[ hide covariance matrix ]
Orbital Elements at Epoch 2459174.5 (2020-Nov-21.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5388735216897836 3.4746e-05  
q .9408002131436692 2.2868e-06 au
tp 2459209.963947313075
(2020-Dec-26.46394731)
0.00021745 TDB
node 243.4898458299314 6.5047e-05 deg
peri 217.8785997594395 0.00016362 deg
i .7983418720496455 3.6593e-05 deg
  Orbit Determination Parameters
   # obs. used (total)      76  
   data-arc span      21 days  
   first obs. used      2020-11-14  
   last obs. used      2020-12-05  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .44729  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Dec-06 05:25:14  

Additional Information
 Jupiter MOID = 2.10604 au 
 T_jup = 3.641 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.20729128415251E-9 -7.942441678944587E-11 -7.537649500735736E-9 -1.003537234359742E-9 5.245481097574398E-9 1.253498933993058E-9
q -7.942441678944587E-11 5.229360582184127E-12 4.949988339698725E-10 6.574103588305339E-11 -3.460764287463621E-10 -8.248851382962657E-11
tp -7.537649500735736E-9 4.949988339698725E-10 4.728616030210394E-8 6.168168145915864E-9 -3.234463103039422E-8 -7.82836689850545E-9
node -1.003537234359742E-9 6.574103588305339E-11 6.168168145915864E-9 4.231138159161738E-9 -7.836160090797076E-9 -7.331764674092502E-10
peri 5.245481097574398E-9 -3.460764287463621E-10 -3.234463103039422E-8 -7.836160090797076E-9 2.677161430099805E-8 5.137180973469892E-9
i 1.253498933993058E-9 -8.248851382962657E-11 -7.82836689850545E-9 -7.331764674092502E-10 5.137180973469892E-9 1.33902647405562E-9

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 25.0   .27787 E2021-CC3 autocmod 2.8

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