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 ]  
(2013 YV102)
Classification: Apollo [NEO]          SPK-ID: 3655733
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 2456658.5 (2014-Jan-01.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .485902415649156 0.0010885  
a 1.332839498781567 0.0019288 au
q .685209566650993 0.00045932 au
i 1.892088744434415 0.0050379 deg
node 80.09575065412852 0.014028 deg
peri 112.8961800186948 0.011322 deg
M 322.0994937502687 0.11077 deg
tp 2456717.670837871565
(2014-Mar-01.17083787)
0.044494 TDB
period 562.0373905668986
1.54
1.22
0.00334
d
yr
n .6405267799654508 0.0013904 deg/d
Q 1.98046943091214 0.002866 au
  Orbit Determination Parameters
   # obs. used (total)      38  
   data-arc span      4 days  
   first obs. used      2013-12-31  
   last obs. used      2014-01-04  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      8  
   norm. resid. RMS      .46158  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 09:10:27  

Additional Information
 Earth MOID = .0131169 au 
 Jupiter MOID = 2.97256 au 
 T_jup = 4.788 
[ 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 25.5   n/a MPO279501  

[ 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 2021-Aug-03 18:50 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin