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 ]  
(2019 TZ6)
Classification: Apollo [NEO]          SPK-ID: 3879168
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 1 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .353098836331349 0.00022659  
a 1.008037145256997 0.00012555 au
q .6521004022879762 0.00015813 au
i 10.7858909762432 0.0082136 deg
node 17.33338186951813 0.00019784 deg
peri 110.0432142360748 0.008021 deg
M 157.8260748453851 0.012624 deg
tp 2458838.434906003708
(2019-Dec-20.93490600)
0.019183 TDB
period 369.6691683919872
1.01
0.06906
0.0001891
d
yr
n .9738437250960181 0.00018193 deg/d
Q 1.363973888226017 0.00016988 au
  Orbit Determination Parameters
   # obs. used (total)      24  
   first obs. used      2019-10-10  
   last obs. used      2019-10-10  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .28742  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Oct-11 07:12:07  

Additional Information
 Earth MOID = .00278427 au 
 Jupiter MOID = 3.7076 au 
 T_jup = 5.971 
[ hide covariance matrix ]
Orbital Elements at Epoch 2458766.5 (2019-Oct-10.0) TDB
Reference: JPL 1 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3520308661786198 0.00022897  
q .6574787341437736 0.00016586 au
tp 2458838.113376476722
(2019-Dec-20.61337648)
0.018373 TDB
node 17.36445144355494 0.00014895 deg
peri 108.9393334715465 0.0073423 deg
i 10.92438809294149 0.008001 deg
  Orbit Determination Parameters
   # obs. used (total)      24  
   first obs. used      2019-10-10  
   last obs. used      2019-10-10  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .28742  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Oct-11 07:12:07  

Additional Information
 Jupiter MOID = 3.7076 au 
 T_jup = 5.971 
Orbit Covariance (6×6)
  e q tp node peri i
e 5.242592728110929E-8 -3.724589517078833E-8 -4.160504343392071E-6 3.121336999736949E-8 -9.225057740689434E-8 1.811952794979432E-6
q -3.724589517078833E-8 2.750988051102286E-8 2.867690533635974E-6 -2.024649662857615E-8 -1.718628931365362E-7 -1.24926101408027E-6
tp -4.160504343392071E-6 2.867690533635974E-6 .0003375835810827176 -2.639119303032094E-6 2.727385228381337E-5 -.000146992216162129
node 3.121336999736949E-8 -2.024649662857615E-8 -2.639119303032094E-6 2.218679828435001E-8 -4.915983452214225E-7 1.14864928148258E-6
peri -9.225057740689434E-8 -1.718628931365362E-7 2.727385228381337E-5 -4.915983452214225E-7 5.390964841455775E-5 -1.179907690411514E-5
i 1.811952794979432E-6 -1.24926101408027E-6 -.000146992216162129 1.14864928148258E-6 -1.179907690411514E-5 6.40154026810284E-5

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 27.7   .27283 MPO502096 autocmod 2.8

[ 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-27 14:20 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin