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
IMPORTANT: The SSD Announcement email list is now available. Major changes are coming in the near future, including possible hostname and/or URL changes. To be notified of such changes, subscribe to this email list.

Please visit this page for more details.


JPL Small-Body Database Browser
Search: [ help ]  
(2014 YT34)
Classification: Apollo [NEO]          SPK-ID: 3703077
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 15 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1594928761328733 1.1178e-06  
a 1.136678304162331 1.218e-06 au
q .9553862121936438 2.4834e-07 au
i 11.27818892233865 8.9832e-05 deg
node 285.4184684766348 1.0708e-05 deg
peri 240.0292552235555 6.2729e-05 deg
M 152.9464797370738 0.0020026 deg
tp 2458412.442019648430
(2018-Oct-20.94201965)
0.00216 TDB
period 442.6442049725372
1.21
0.00071147
1.948e-06
d
yr
n .8132942800467371 1.3072e-06 deg/d
Q 1.317970396131018 1.4123e-06 au
  Orbit Determination Parameters
   # obs. used (total)      72  
   data-arc span      171 days  
   first obs. used      2014-12-28  
   last obs. used      2015-06-17  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      3  
   norm. resid. RMS      .42191  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:36:38  

Additional Information
 Earth MOID = .0360208 au 
 Jupiter MOID = 3.68961 au 
 T_jup = 5.483 
[ 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 24.7   n/a E2015A31  

[ 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
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin