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 UK6)
Classification: Apollo [NEO]          SPK-ID: 3788050
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 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .08830561135422929 1.3493e-06  
a 1.07413982555512 1.4112e-06 au
q .9792872515795501 1.8456e-07 au
i 27.96308996053218 0.00024731 deg
node 34.98510828398394 1.2434e-05 deg
peri 58.65965480667715 0.00016085 deg
M 73.67219904601286 0.00070123 deg
tp 2458517.287075001684
(2019-Feb-02.78707500)
0.0006286 TDB
period 406.6208608851747
1.11
0.0008013
2.194e-06
d
yr
n .8853456244628335 1.7447e-06 deg/d
Q 1.16899239953069 1.5358e-06 au
  Orbit Determination Parameters
   # obs. used (total)      75  
   data-arc span      176 days  
   first obs. used      2017-10-25  
   last obs. used      2018-04-19  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      3  
   norm. resid. RMS      .43085  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Apr-19 06:22:18  

Additional Information
 Earth MOID = .025261 au 
 Jupiter MOID = 3.92105 au 
 T_jup = 5.644 
[ 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 24.0   n/a MPO446981  

[ 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