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 ]  
(2006 FH36)
Classification: Aten [NEO]          SPK-ID: 3329255
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 20 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1985703085525618 1.0785e-07  
a .9548840625075463 3.2009e-09 au
q .7652724395834992 1.0339e-07 au
i 1.587921449642542 4.9596e-06 deg
node 278.314219144346 0.00040723 deg
peri 157.0179488625688 0.00040512 deg
M 158.2014765113695 2.0338e-05 deg
tp 2458850.727380426313
(2020-Jan-02.22738043)
1.926e-05 TDB
period 340.8194679058662
0.93
1.7137e-06
4.692e-09
d
yr
n 1.056277689217658 5.3112e-09 deg/d
Q 1.144495685431594 3.8365e-09 au
  Orbit Determination Parameters
   # obs. used (total)      85  
   data-arc span      5117 days (14.01 yr)  
   first obs. used      2006-03-31  
   last obs. used      2020-04-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .50563  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Apr-04 06:25:23  

Additional Information
 Earth MOID = .0173502 au 
 Jupiter MOID = 4.03111 au 
 T_jup = 6.289 
[ hide covariance matrix ]
Orbital Elements at Epoch 2454588.5 (2008-May-02.0) TDB
Reference: JPL 20 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1984501577353485 1.0786e-07  
q .7654302338162819 1.0303e-07 au
tp 2454419.743541289597
(2007-Nov-15.24354129)
1.9698e-05 TDB
node 280.7808363927344 0.00041557 deg
peri 154.6774067631811 0.0004129 deg
i 1.58722957480042 4.6934e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      85  
   data-arc span      5117 days (14.01 yr)  
   first obs. used      2006-03-31  
   last obs. used      2020-04-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .50563  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Apr-04 06:25:23  

Additional Information
 Jupiter MOID = 4.03111 au 
 T_jup = 6.289 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.163400847942717E-14 -1.1112705804268E-14 1.936017338062787E-12 3.732236983671057E-12 -3.301192020090999E-12 2.017560897375982E-14
q -1.1112705804268E-14 1.061497958244062E-14 -1.847761758616878E-12 -3.479423458790305E-12 3.069960911959944E-12 -2.093367059173955E-14
tp 1.936017338062787E-12 -1.847761758616878E-12 3.879939879952237E-10 1.083723717409884E-9 -9.429261928774784E-10 -1.533288305734913E-11
node 3.732236983671057E-12 -3.479423458790305E-12 1.083723717409884E-9 1.72701361789872E-7 -1.715490050151682E-7 -1.082282825352552E-9
peri -3.301192020090999E-12 3.069960911959944E-12 -9.429261928774784E-10 -1.715490050151682E-7 1.704904988719111E-7 1.055998598128652E-9
i 2.017560897375982E-14 -2.093367059173955E-14 -1.533288305734913E-11 -1.082282825352552E-9 1.055998598128652E-9 2.202809338132264E-11

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 22.9   n/a MPO121856  

[ 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-Apr-05 14:48 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin