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349922 (2009 TW42)
Classification: Inner Main-belt Asteroid          SPK-ID: 2349922
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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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.


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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1054636585884915 1.8265e-07  
a 1.981876463433944 3.6077e-08 au
q 1.77286052072978 3.3589e-07 au
i 18.90362013152321 1.0631e-05 deg
node 233.6795276281318 2.4223e-05 deg
peri 229.8231191512454 9.0823e-05 deg
M 227.7642139123404 6.6463e-05 deg
tp 2459374.834450331773
(2021-Jun-09.33445033)		 0.00018686 TDB
period 1019.091776186101
2.79		 2.7827e-05
7.619e-08		 d
yr
n .3532557208412394 9.6458e-09 deg/d
Q 2.190892406138109 3.9882e-08 au
   Orbit Determination Parameters
   # obs. used (total)      67  
   data-arc span      4036 days (11.05 yr)  
   first obs. used      2008-05-14  
   last obs. used      2019-06-02  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .6112  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-25 23:44:45  

Additional Information
 Earth MOID = .823701 au 
 Jupiter MOID = 3.08117 au 
 T_jup = 3.787 
[ show covariance matrix ]

[ 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 17.9   n/a MPO368388  

349922 (2009 TW42)          Discovered 2009-Oct-01 by Charleston at Charleston
Reference: 20121228/Numbers.arcLast Updated: 2013-01-02

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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
2076-Nov-13 23:27 00:05 Iris 0.0377592998834313 0.0377054093175845 0.0378132444597621 6.46015910902379 6.4601590854567 2479621.477261804 5.31565327271612 3506.95623900993 69.6758770109105 39.9675385186134 52078.8592235027 T 7 CATAB v2.0f-lin.ifort 2020-Feb-25 23:44:46 2020-Feb-25 23:44
2180-Feb-03 14:28 00:16 Iris 0.0241028574993974 0.0240952435220383 0.0241117686884439 6.28374267823206 6.28374264027557 2517322.102454453 15.5850392640488 8959.34784601389 70.2051795196525 -87.4044888778971 51294.6825882017 T 7 CATAB v2.0f-lin.ifort 2020-Feb-25 23:44:46 2020-Feb-25 23:44
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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