Skip Page Navigation
NASA JPL Caltech
NASA Logo - Jet Propulsion Laboratory + View the NASA Portal
+ Center for Near-Earth Object Studies
JPL Home Earth Solar System Stars & Galaxies Technology
JPL Solar System Dynamics
BODIES ORBITS EPHEMERIDES TOOLS PHYSICAL DATA DISCOVERY FAQ SITE MAP
JPL Small-Body Database Browser
Search: [ help ]  
(2020 GV1)
Classification: Apollo [NEO]          SPK-ID: 54016480
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 2458943.5 (2020-Apr-04.0) TDB
Reference: JPL 1 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .559033737088104 0.0026371  
a 2.221044026724281 0.013076 au
q .9794054842273957 9.0928e-05 au
i .8561503545732909 0.0029045 deg
node 12.61253919266728 0.00091315 deg
peri 209.0620601177793 0.01781 deg
M 353.4967497687754 0.059291 deg
tp 2458965.340478163179
(2020-Apr-25.84047816)
0.0063488 TDB
period 1209.021928910745
3.31
10.677
0.02923
d
yr
n .2977613485673813 0.0026296 deg/d
Q 3.462682569221167 0.020386 au
  Orbit Determination Parameters
   # obs. used (total)      13  
   data-arc span      2 days  
   first obs. used      2020-04-03  
   last obs. used      2020-04-05  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .33386  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Apr-05 08:12:19  

Additional Information
 Earth MOID = .00224316 au 
 Jupiter MOID = 1.52302 au 
 T_jup = 3.426 
[ 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 27.87   .22612 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-Apr-05 23:59 < 00:01 Earth 0.0165156502243113 0.0163131013615152 0.0167181802211939 9.25291579717488 9.23546369170296 2458945.499277631 0.348794954485996 10061.3210209924 18.6839251546494 -0.219443193395139 152.948638307702 T 1 CATAB v2.0f-lin.ifort 2020-Apr-05 08:12:20 2020-Apr-05 08:12
2079-Jun-22 01:10 6_13:16 Earth 0.139472678925008 0.0393283505379666 0.242428001296403 13.3849698291356 13.3835424840825 2480571.548582970 9435.49486496776 5159714.19115688 303.765980340548 7.58227259617201 7629.18945554856 T 1 CATAB v2.0f-lin.ifort 2020-Apr-05 08:12:20 2020-Apr-05 08:12
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
ABOUT SSD CREDITS/AWARDS PRIVACY/COPYRIGHT GLOSSARY LINKS
FirstGov 2021-Jan-17 01:14 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin