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(2020 VW3)
Classification: Apollo [NEO]          SPK-ID: 54087763
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459165.5 (2020-Nov-12.0) TDB
Reference: JPL 1 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5070645236197564 0.027124  
a 1.234182264625485 0.043777 au
q .6083722225532112 0.011919 au
i 2.712164774046633 0.17812 deg
node 40.90396348035528 0.3893 deg
peri 264.5868304320753 0.1211 deg
M 45.20173811487774 3.5953 deg
tp 2459102.618917025014
(2020-Sep-10.11891703)
1.656 TDB
period 500.8035269233183
1.37
26.646
0.07295
d
yr
n .7188447777348066 0.038247 deg/d
Q 1.859992306697758 0.065975 au
  Orbit Determination Parameters
   # obs. used (total)      11  
   data-arc span      1 day  
   first obs. used      2020-11-12  
   last obs. used      2020-11-13  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      9  
   norm. resid. RMS      .34852  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-12 18:12:14  

Additional Information
 Earth MOID = .00255836 au 
 Jupiter MOID = 3.41082 au 
 T_jup = 5.055 
[ 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 26.933   .2517 1 autocmod 2.8

[ hide close-approach data ]
Close-Approach Data   ...sorted by Date/Time (TDB)
Date/Time (TDB) Time Uncertainty
(days_HH:MM)
Body Nominal Distance (au) Minimum Distance (au) Maximum Distance (au) V-relative (km/s) V-infinity (km/s) JD (TDB) Time Uncertainty (minutes) Semi-major axis (km) Semi-minor axis (km) range-LOV angle (deg) N-sigma BP Orbit Ref. Reference Modified
2020-Nov-05 10:14 12:50 Earth 0.0166778544845772 0.0160783440778373 0.0172772780600544 15.6414655817457 15.6312482710227 2459158.926555757 770.05074507481 29832.9152368089 4128.10942385479 0.704110523380526 57.4519923551855 T 1 CATAB v2.0f-lin.ifort 2020-Nov-12 18:12:15 2020-Nov-12 18:12
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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