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 UX2)
Classification: Apollo [NEO]          SPK-ID: 3653065
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1492876548705398 1.2289e-05  
a 1.118665712305694 3.1017e-05 au
q .9516627315314948 3.2558e-05 au
i 4.10534056484836 0.0021075 deg
node 211.4319628144509 0.00062959 deg
peri 228.0289018252415 0.018476 deg
M 171.238952455574 0.07116 deg
tp 2458794.935091674527
(2019-Nov-07.43509167)
0.076891 TDB
period 432.1643290615755
1.18
0.017974
4.921e-05
d
yr
n .8330164610802633 3.4645e-05 deg/d
Q 1.285668693079893 3.5647e-05 au
  Orbit Determination Parameters
   # obs. used (total)      15  
   data-arc span      1 day  
   first obs. used      2013-10-24  
   last obs. used      2013-10-25  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .71541  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:44:03  

Additional Information
 Earth MOID = .000368769 au 
 Jupiter MOID = 3.86153 au 
 T_jup = 5.566 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456590.5 (2013-Oct-25.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1246020900277683 2.8251e-05  
q .9140094063517702 1.8153e-05 au
tp 2456657.018375886974
(2013-Dec-30.51837589)
0.0029204 TDB
node 211.9959350789098 3.0981e-05 deg
peri 254.3539980229698 0.0032932 deg
i 5.17038365134843 0.00138 deg
  Orbit Determination Parameters
   # obs. used (total)      15  
   data-arc span      1 day  
   first obs. used      2013-10-24  
   last obs. used      2013-10-25  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .71541  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:44:03  

Additional Information
 Jupiter MOID = 3.86153 au 
 T_jup = 5.566 
Orbit Covariance (6×6)
  e q tp node peri i
e 7.981353220886473E-10 -4.839752886949557E-10 -3.742256102952098E-8 -3.400753289472354E-10 1.473305631161569E-8 3.866964731072195E-8
q -4.839752886949557E-10 3.295268786921789E-10 7.064971537221778E-9 4.749371494779771E-11 -2.845827624032544E-8 -2.446891093962788E-8
tp -3.742256102952098E-8 7.064971537221778E-9 8.528685663783067E-6 8.486588976777381E-8 7.772295543484904E-6 -1.370578317294804E-6
node -3.400753289472354E-10 4.749371494779771E-11 8.486588976777381E-8 9.59802895692651E-10 7.967447278310779E-8 -1.199716596696643E-8
peri 1.473305631161569E-8 -2.845827624032544E-8 7.772295543484904E-6 7.967447278310779E-8 1.084547718316606E-5 1.26663473403365E-6
i 3.866964731072195E-8 -2.446891093962788E-8 -1.370578317294804E-6 -1.199716596696643E-8 1.26663473403365E-6 1.90433605116241E-6

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 29.2   n/a E2013U44  

[ 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-30 06:20 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin