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 ]  
(2015 YV9)
Classification: Apollo [NEO]          SPK-ID: 3739060
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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5281353171308297 0.00067393  
a 2.135519780205246 0.0030171 au
q 1.007676363847388 1.5551e-05 au
i 6.158329701024689 0.0057914 deg
node 93.24073703962183 0.00019718 deg
peri 357.6435029243714 0.0036019 deg
M 152.1098171380583 1.0897 deg
tp 2458518.875503524907
(2019-Feb-04.37550352)
2.4298 TDB
period 1139.866065144668
3.12
2.4157
0.006614
d
yr
n .3158265791115642 0.00066931 deg/d
Q 3.263363196563103 0.0046106 au
  Orbit Determination Parameters
   # obs. used (total)      47  
   data-arc span      5 days  
   first obs. used      2015-12-29  
   last obs. used      2016-01-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .70308  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:29:35  

Additional Information
 Earth MOID = .0245162 au 
 Jupiter MOID = 1.97352 au 
 T_jup = 3.518 
[ 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 25.8   n/a E2016A20  

[ 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-Aug-04 20:59 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin