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362306 (2009 TD4)
Classification: Main-belt Asteroid          SPK-ID: 2362306
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | 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.


Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 20 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1953257986059543 4.4593e-08  
a 3.145457808704872 2.6648e-08 au
q 2.531068750238259 1.4113e-07 au
i 15.24856687824848 4.8891e-06 deg
node 248.3408730684976 2.1427e-05 deg
peri 30.62406739681646 2.876e-05 deg
M 44.77834896826203 1.6029e-05 deg
tp 2458747.051456981601
(2019-Sep-20.55145698)
9.0124e-05 TDB
period 2037.624825142475
5.58
2.5894e-05
7.089e-08
d
yr
n .1766762926903524 2.2452e-09 deg/d
Q 3.759846867171486 3.1853e-08 au
  Orbit Determination Parameters
   # obs. used (total)      463  
   data-arc span      6770 days (18.54 yr)  
   first obs. used      2002-05-04  
   last obs. used      2020-11-15  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .47263  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Dec-18 01:02:23  

Additional Information
 Earth MOID = 1.52726 au 
 Jupiter MOID = 1.39684 au 
 T_jup = 3.126 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457892.5 (2017-May-19.0) TDB
Reference: JPL 20 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1954398702295947 4.4256e-08  
q 2.530169766861959 1.3975e-07 au
tp 2458749.279114545150
(2019-Sep-22.77911455)
9.0506e-05 TDB
node 248.3598981648081 2.1419e-05 deg
peri 31.13823756394008 2.8837e-05 deg
i 15.25233679285808 4.8913e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      463  
   data-arc span      6770 days (18.54 yr)  
   first obs. used      2002-05-04  
   last obs. used      2020-11-15  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .47263  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Dec-18 01:02:23  

Additional Information
 Jupiter MOID = 1.39684 au 
 T_jup = 3.126 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.958558307314212E-15 -6.112413087991427E-15 -7.684725557103851E-13 2.113940453104713E-14 -2.723105986897239E-13 -3.745298936556197E-15
q -6.112413087991427E-15 1.952982746816577E-14 2.685703716573945E-12 -7.26183636808002E-14 8.660406495351535E-13 1.312553968175374E-14
tp -7.684725557103851E-13 2.685703716573945E-12 8.191421809601574E-9 -5.377849050622667E-11 1.768985560038004E-9 -1.652053332481737E-11
node 2.113940453104713E-14 -7.26183636808002E-14 -5.377849050622667E-11 4.587676564712974E-10 -4.533987080800751E-10 -1.320304748934283E-11
peri -2.723105986897239E-13 8.660406495351535E-13 1.768985560038004E-9 -4.533987080800751E-10 8.315734466737037E-10 9.236931078504469E-12
i -3.745298936556197E-15 1.312553968175374E-14 -1.652053332481737E-11 -1.320304748934283E-11 9.236931078504469E-12 2.392520164008027E-11

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 15.1   n/a MPO494884  

362306 (2009 TD4)          Discovered 2009-Oct-13 by Lowe, A. at Mayhill
Reference: Last Updated: 2013-04-29

[ hide close-approach data ]
Close-Approach Data   ...sorted by Date/Time (TDB)
Date/Time (TDB) Time Uncertainty
(days_HH:MM)
Body Nominal Distance (au) Minimum Distance (au) Maximum Distance (au) V-relative (km/s) V-infinity (km/s) JD (TDB) Time Uncertainty (minutes) Semi-major axis (km) Semi-minor axis (km) range-LOV angle (deg) N-sigma BP Orbit Ref. Reference Modified
1966-Mar-31 16:43 00:02 Jupiter 1.55119345280834 1.55119169125031 1.5511952143744 3.87774128536968 3.73427182659834 2439216.196360363 2.02362692519252 235.548913739136 52.1219529969068 71.4471365241136 2779348.25121821 T 20 CATAB v2.0f-lin.ifort 2020-Dec-18 01:02:24 2020-Dec-18 01:02
1977-Jan-19 12:13 00:01 Jupiter 1.47701255591914 1.47701151818645 1.47701359366948 4.05688914366509 3.91297960053861 2443163.008769728 1.45054282889302 312.183556000903 25.7127337158703 -81.7733458648242 2677604.21627692 T 20 CATAB v2.0f-lin.ifort 2020-Dec-18 01:02:24 2020-Dec-18 01:02
2061-Dec-30 10:38 00:02 Jupiter 1.93908964150362 1.93908767578778 1.93909160722311 3.06006778397183 2.91382665879976 2474188.942740613 2.21232725869071 241.93740106357 86.3762242713875 -69.8977865321201 2615049.75184638 T 20 CATAB v2.0f-lin.ifort 2020-Dec-18 01:02:24 2020-Dec-18 01:02
2072-Aug-25 08:01 00:02 Jupiter 1.44077298133188 1.44077215606569 1.44077380660872 3.97151764573146 3.8206234313706 2478079.833835354 2.03007296276715 336.824968097246 33.0361703046964 85.5919470634525 2777933.11413069 T 20 CATAB v2.0f-lin.ifort 2020-Dec-18 01:02:24 2020-Dec-18 01:02
2083-Jun-04 17:08 00:03 Jupiter 1.64368628803808 1.64368352402199 1.64368905209714 4.05979139286087 3.93081015415793 2482015.213759753 2.98438173613183 460.526545599795 31.2633194791693 -72.9717762381575 2568491.41647939 T 20 CATAB v2.0f-lin.ifort 2020-Dec-18 01:02:24 2020-Dec-18 01:02
2168-May-02 18:51 00:07 Jupiter 1.73215236900307 1.73214662857431 1.73215810946009 3.45308762859577 3.30844588322908 2513028.285459143 6.65254644250262 468.167626522679 86.5523580268812 48.7714819227924 2132151.58728305 T 20 CATAB v2.0f-lin.ifort 2020-Dec-18 01:02:24 2020-Dec-18 01:02
2179-Feb-02 20:42 00:06 Jupiter 1.43213608412204 1.43213502711556 1.43213714136379 4.03433805306543 3.88497150516396 2516956.362759139 5.93538404478045 1099.48015381472 26.8088899614182 -87.8685576115437 2786391.1211016 T 20 CATAB v2.0f-lin.ifort 2020-Dec-18 01:02:24 2020-Dec-18 01:02
2189-Oct-14 08:28 00:08 Jupiter 1.84643340027767 1.84642570298552 1.84644109767205 4.10259356208778 3.98921109219291 2520862.853065220 8.25517470145318 797.335274691999 38.4613104890765 -61.2989558348723 2508278.79574576 T 20 CATAB v2.0f-lin.ifort 2020-Dec-18 01:02:24 2020-Dec-18 01:02
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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