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 SR260)
Classification: Amor [NEO]          SPK-ID: 3691094
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 11 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5991714375887817 6.2587e-05  
a 2.823647535797922 0.00038918 au
q 1.13179858252986 2.074e-05 au
i 8.51576069398012 0.00054216 deg
node 186.3765246806239 0.00075721 deg
peri 215.7100771904514 0.00079653 deg
M 336.9855209365628 0.073349 deg
tp 2458711.293122413577
(2019-Aug-15.79312241)
0.37601 TDB
period 1733.062215266612
4.74
0.3583
0.000981
d
yr
n .207724798814922 4.2946e-05 deg/d
Q 4.515496489065985 0.00062237 au
  Orbit Determination Parameters
   # obs. used (total)      33  
   data-arc span      53 days  
   first obs. used      2014-09-24  
   last obs. used      2014-11-16  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .47137  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:38:25  

Additional Information
 Earth MOID = .159253 au 
 Jupiter MOID = .968064 au 
 T_jup = 3.009 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456936.5 (2014-Oct-06.0) TDB
Reference: JPL 11 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5928651718504174 5.4661e-05  
q 1.155063114023051 1.33e-05 au
tp 2456969.540683489884
(2014-Nov-08.04068349)
0.00020759 TDB
node 186.5763503380917 0.00012839 deg
peri 215.4105354486032 0.00024981 deg
i 8.508019695073342 0.00058579 deg
  Orbit Determination Parameters
   # obs. used (total)      33  
   data-arc span      53 days  
   first obs. used      2014-09-24  
   last obs. used      2014-11-16  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .47137  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:38:25  

Additional Information
 Jupiter MOID = .968064 au 
 T_jup = 3.009 
Orbit Covariance (6×6)
  e q tp node peri i
e 2.987790850573134E-9 7.250017267016685E-10 -3.588125013365282E-9 -6.462667847038087E-9 -8.306763451884459E-9 3.19171984471056E-8
q 7.250017267016685E-10 1.768833202550936E-10 -1.043212290221731E-9 -1.583250649853105E-9 -2.188970499891932E-9 7.783545216952183E-9
tp -3.588125013365282E-9 -1.043212290221731E-9 4.309373526949437E-8 1.049648602328543E-8 4.782112072639804E-8 -4.50615742318243E-8
node -6.462667847038087E-9 -1.583250649853105E-9 1.049648602328543E-8 1.648488727717475E-8 1.847127660904531E-8 -6.940810626110894E-8
peri -8.306763451884459E-9 -2.188970499891932E-9 4.782112072639804E-8 1.847127660904531E-8 6.240593341827125E-8 -9.577510316188615E-8
i 3.19171984471056E-8 7.783545216952183E-9 -4.50615742318243E-8 -6.940810626110894E-8 -9.577510316188615E-8 3.431461642181084E-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 23.2   n/a MPO315319  

[ 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-10 13:51 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin