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 ]  
(2017 LV)
Classification: Apollo [NEO]          SPK-ID: 3775204
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.


[ revert to old Java-based viewer ]

Orbital Elements at Epoch 2457919.5 (2017-Jun-15.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4847371077084951 0.00079288  
a 1.778190604951907 0.002528 au
q .9162356341531003 0.00010733 au
i 4.430093401771816 0.0057118 deg
node 256.3299497899617 0.00068983 deg
peri 58.33598282667563 0.00088544 deg
M 343.1096846899924 0.041604 deg
tp 2457960.135082908524
(2017-Jul-25.63508291)
0.013439 TDB
period 866.095722819404
2.37
1.8469
0.005057
d
yr
n .4156584434201925 0.00088638 deg/d
Q 2.640145575750713 0.0037534 au
  Orbit Determination Parameters
   # obs. used (total)      65  
   data-arc span      6 days  
   first obs. used      2017-06-13  
   last obs. used      2017-06-19  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .42717  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Jun-19 06:18:18  

Additional Information
 Earth MOID = .0165404 au 
 Jupiter MOID = 2.68129 au 
 T_jup = 3.946 
[ 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 26.1   n/a MPO412131  

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
ABOUT SSD CREDITS/AWARDS PRIVACY/COPYRIGHT GLOSSARY LINKS
FirstGov 2020-Nov-27 07:03 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin