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 ]  
(2017 FA102)
Classification: Apollo [NEO]          SPK-ID: 3772997
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 2457836.5 (2017-Mar-24.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5751713977849745 0.0016961  
a 1.924267886785554 0.0069249 au
q .8174840366303679 0.00032184 au
i .3339860627577217 0.00058228 deg
node 228.2681768273893 0.033061 deg
peri 29.88252211975924 0.031192 deg
M 340.0077685767673 0.12177 deg
tp 2457890.644643025290
(2017-May-17.14464303)
0.037501 TDB
period 974.9822856918769
2.67
5.263
0.01441
d
yr
n .3692374777296935 0.0019932 deg/d
Q 3.031051736940741 0.010908 au
  Orbit Determination Parameters
   # obs. used (total)      27  
   data-arc span      13 days  
   first obs. used      2017-03-21  
   last obs. used      2017-04-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .38075  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:19:00  

Additional Information
 Earth MOID = .00296969 au 
 Jupiter MOID = 2.04844 au 
 T_jup = 3.699 
[ hide covariance matrix ]
Orbit Covariance (6×6)
  e q tp node peri i
e 2.876736485733509E-6 -5.458726455391635E-7 -6.360477666377605E-5 5.575154776389635E-5 -5.255129870934704E-5 9.867762960174027E-7
q -5.458726455391635E-7 1.035841966609342E-7 1.206908872243477E-5 -1.057815014592221E-5 9.970482810584582E-6 -1.872510949950844E-7
tp -6.360477666377605E-5 1.206908872243477E-5 .001406317362575539 -.001232732795417893 .001162003670237205 -2.18172404224142E-5
node 5.575154776389635E-5 -1.057815014592221E-5 -.001232732795417893 .001093052255442006 -.001031175205946442 1.904012368721301E-5
peri -5.255129870934704E-5 9.970482810584582E-6 .001162003670237205 -.001031175205946442 .0009729221926012282 -1.794141075819681E-5
i 9.867762960174027E-7 -1.872510949950844E-7 -2.18172404224142E-5 1.904012368721301E-5 -1.794141075819681E-5 3.390540341005944E-7

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 MPO405725  

[ 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