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 ]  
(2015 GB14)
Classification: Apollo [NEO]          SPK-ID: 3715908
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 2457132.5 (2015-Apr-20.0) TDB
Reference: JPL 13 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5321848569625284 0.00091809  
a 1.921395888080897 0.0035009 au
q .8988580922141747 0.00012624 au
i 2.446718725240242 0.0030602 deg
node 39.09875528148609 0.0016429 deg
peri 227.9448672138525 0.0015176 deg
M 343.2981208054285 0.050701 deg
tp 2457177.632204738086
(2015-Jun-04.13220474)
0.013654 TDB
period 972.8003368023267
2.66
2.6588
0.007279
d
yr
n .3700656613497371 0.0010114 deg/d
Q 2.94393368394762 0.0053641 au
  Orbit Determination Parameters
   # obs. used (total)      75  
   data-arc span      14 days  
   first obs. used      2015-04-15  
   last obs. used      2015-04-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .34504  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:34:25  

Additional Information
 Earth MOID = .00116799 au 
 Jupiter MOID = 2.16705 au 
 T_jup = 3.736 
[ hide covariance matrix ]
Orbit Covariance (6×6)
  e q tp node peri i
e 8.428924662543573E-7 -1.158946605265473E-7 -1.253509768879418E-5 1.507524356206248E-6 1.387914810455581E-6 2.8095071662177E-6
q -1.158946605265473E-7 1.593543033654064E-8 1.723488410088232E-6 -2.072778960375765E-7 -1.909032950551909E-7 -3.862988910541631E-7
tp -1.253509768879418E-5 1.723488410088232E-6 .0001864214356341286 -2.241930265930097E-5 -2.063152692538924E-5 -4.178141644118617E-5
node 1.507524356206248E-6 -2.072778960375765E-7 -2.241930265930097E-5 2.699181297228023E-6 2.479146620354544E-6 5.024007620880269E-6
peri 1.387914810455581E-6 -1.909032950551909E-7 -2.063152692538924E-5 2.479146620354544E-6 2.302992776046683E-6 4.62738585517505E-6
i 2.8095071662177E-6 -3.862988910541631E-7 -4.178141644118617E-5 5.024007620880269E-6 4.62738585517505E-6 9.364964989098129E-6

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 25.4   n/a MPO337014  

[ 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 2019-Dec-14 10:40 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin