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 TN127)
Classification: Aten [NEO]          SPK-ID: 3650847
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 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .09687400452108495 5.1749e-05  
a .9348301385459982 1.7306e-05 au
q .8442693994780467 6.2946e-05 au
i 13.45964955645298 0.016031 deg
node 198.7800156260856 0.00054008 deg
peri 2.333416848401165 0.015709 deg
M 156.2005868898335 0.060329 deg
tp 2459057.255602342246
(2020-Jul-26.75560234)
0.051357 TDB
period 330.1394968071511
0.90
0.0091675
2.51e-05
d
yr
n 1.09044813929153 3.028e-05 deg/d
Q 1.02539087761395 1.8982e-05 au
  Orbit Determination Parameters
   # obs. used (total)      31  
   data-arc span      3 days  
   first obs. used      2013-10-11  
   last obs. used      2013-10-14  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      5  
   norm. resid. RMS      .50546  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 08:47:14  

Additional Information
 Earth MOID = .0264813 au 
 Jupiter MOID = 3.92961 au 
 T_jup = 6.387 
[ 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 26.2   n/a E2013U15  

[ 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-May-08 23:49 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin