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 ]  
(2016 TY55)
Classification: Apollo [NEO]          SPK-ID: 3760891
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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1531722260956968 3.3862e-05  
a 1.031094444685489 1.9316e-05 au
q .8731594132781061 1.8565e-05 au
i 4.208752803578716 0.00092875 deg
node 206.9395242500833 0.0002635 deg
peri 264.3222266466271 0.0032714 deg
M 95.13070129259302 0.030689 deg
tp 2458899.443490196887
(2020-Feb-19.94349020)
0.029761 TDB
period 382.4248432398893
1.05
0.010746
2.942e-05
d
yr
n .9413614370606604 2.6452e-05 deg/d
Q 1.189029476092871 2.2274e-05 au
  Orbit Determination Parameters
   # obs. used (total)      45  
   data-arc span      9 days  
   first obs. used      2016-10-10  
   last obs. used      2016-10-19  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .41221  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-17 06:11:30  

Additional Information
 Earth MOID = .00155845 au 
 Jupiter MOID = 3.86928 au 
 T_jup = 5.924 
[ 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 26.9   n/a E2016U23  

[ 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 2020-Nov-29 06:12 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin