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316695 (1996 TE9)
Classification: Amor [NEO]          SPK-ID: 2316695
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbit Diagram
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Note: This Java-based orbit viewer will eventually be retired.

Note: Make sure you have Java enabled on your browser to see the applet. This applet is provided as a 3D orbit visualization tool. The applet 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. For accurate long-term ephemerides, please instead use our Horizons system.

Note: If the applet is not working, here are some notes that might help.
Orbit Viewer

Additional Notes: the orbits shown in the applet are color coded. The planets are white lines, and the asteroid/comet is a blue line. The bright white line indicates the portion of the orbit that is above the ecliptic plane, and the darker portion is below the ecliptic plane. Likewise for the asteroid/comet orbit, the light blue indicates the portion above the ecliptic plane, and the dark blue the portion below the ecliptic plane.

Orbit Viewer applet originally written and kindly provided by Osamu Ajiki (AstroArts), and further modified by Ron Baalke (JPL).


Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 62 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3260003715739733 1.0045e-07  
a 1.793264567559931 1.8807e-09 au
q 1.208659652204953 1.8078e-07 au
i 21.63191768572667 1.4302e-05 deg
node 13.88365929766633 1.131e-05 deg
peri 3.89435396584412 2.8315e-05 deg
M 300.9642165123492 1.4583e-05 deg
tp 2459144.339382069330
(2020-Oct-21.83938207)
3.5641e-05 TDB
period 877.1320457835672
2.40
1.3798e-06
3.778e-09
d
yr
n .4104285115685195 6.4565e-10 deg/d
Q 2.377869482914909 2.4938e-09 au
  Orbit Determination Parameters
   # obs. used (total)      292  
   data-arc span      8776 days (24.03 yr)  
   first obs. used      1996-10-13  
   last obs. used      2020-10-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .45039  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Oct-24 07:52:08  

Additional Information
 Earth MOID = .210507 au 
 Jupiter MOID = 3.08806 au 
 T_jup = 3.933 
[ 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 18.8   n/a MPO285484  

316695 (1996 TE9)          Discovered 1996-Oct-13 by NEAT at Haleakala
Reference: 20120308/Numbers.arcLast Updated: 2012-03-13

[ 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
1900-Oct-05 13:27 < 00:01 Earth 0.257621608511674 0.257617681578164 0.257625535989065 11.826535043044 11.8256604850692 2415298.060522588 0.0805421512044137 627.062006923445 26.3307516126577 71.9567805895168 1205515.38635647 T 62 CATAB v2.0f-lin.ifort 2020-Oct-24 07:52:23 2020-Oct-24 07:52
1912-Oct-05 20:29 < 00:01 Earth 0.242139726129954 0.242137164697592 0.242142287956091 11.7195013618911 11.7185623857128 2419681.353313196 0.0641828359061187 512.354048238804 24.5321968135455 75.8210833566172 1243749.38940363 T 62 CATAB v2.0f-lin.ifort 2020-Oct-24 07:52:23 2020-Oct-24 07:52
1924-Oct-06 00:10 < 00:01 Earth 0.232862705498677 0.232861085391453 0.232864325852196 11.6605751111703 11.6595937910083 2424064.506747243 0.0541768959783809 403.055160369277 23.5974206808471 78.9281649085689 1262246.20498797 T 62 CATAB v2.0f-lin.ifort 2020-Oct-24 07:52:23 2020-Oct-24 07:52
1936-Oct-06 04:48 < 00:01 Earth 0.227176637825576 0.227175620190201 0.227177655591338 11.6211674661104 11.6201581718839 2428447.699909675 0.0479986190279843 309.193520077376 23.1529737989661 81.5780138325738 1267691.93747482 T 62 CATAB v2.0f-lin.ifort 2020-Oct-24 07:52:23 2020-Oct-24 07:52
1948-Oct-06 05:53 < 00:01 Earth 0.224496195156751 0.224495506096735 0.224496884267697 11.606250457463 11.6052277991157 2432830.745203200 0.044974872474528 231.392009513679 23.2271803939936 83.6853903377184 1256925.84525879 T 62 CATAB v2.0f-lin.ifort 2020-Oct-24 07:52:23 2020-Oct-24 07:52
1960-Oct-06 07:55 < 00:01 Earth 0.224369105178974 0.224368557544961 0.224369652825461 11.6026085522033 11.6015849933543 2437213.830057266 0.044038485748644 170.817165842466 23.7321002955571 85.419264119112 1236122.56155697 T 62 CATAB v2.0f-lin.ifort 2020-Oct-24 07:52:23 2020-Oct-24 07:52
1972-Oct-06 07:49 < 00:01 Earth 0.226217039455219 0.22621653433106 0.226217544580599 11.6157615827111 11.6147475351843 2441596.825749785 0.0440458767942539 121.906773394513 24.5715104860701 87.3414850847472 1210000.90258842 T 62 CATAB v2.0f-lin.ifort 2020-Oct-24 07:52:23 2020-Oct-24 07:52
1984-Oct-06 06:55 < 00:01 Earth 0.230951313672652 0.230950801037003 0.230951826308327 11.6438492042146 11.6428583407242 2445979.788530834 0.0463654346356573 83.6408712081253 25.5303540627975 -89.0782310476373 1195808.97665167 T 62 CATAB v2.0f-lin.ifort 2020-Oct-24 07:52:23 2020-Oct-24 07:52
1996-Oct-06 05:25 < 00:01 Earth 0.239261476904447 0.239260927899109 0.239262025910314 11.692758968961 11.6918065231666 2450362.725884127 0.0494778703954479 54.5054864480715 25.3812535064397 -77.7203082693344 1235835.51395067 T 62 CATAB v2.0f-lin.ifort 2020-Oct-24 07:52:23 2020-Oct-24 07:52
2008-Oct-06 00:47 < 00:01 Earth 0.252871408109353 0.252870800219392 0.252872016000061 11.7780890035585 11.7771943512382 2454745.532430383 0.0555439409037679 41.9426814558563 20.2719790306796 -52.1375000746097 1465032.1349411 T 62 CATAB v2.0f-lin.ifort 2020-Oct-24 07:52:23 2020-Oct-24 07:52
2020-Oct-05 20:01 < 00:01 Earth 0.273907573193482 0.273906875500779 0.273908270886636 11.9077618380145 11.9069448925338 2459128.333813944 0.0642323473497941 42.9902480254848 25.0989252611532 -46.3487270500796 1299503.68360127 T 62 CATAB v2.0f-lin.ifort 2020-Oct-24 07:52:23 2020-Oct-24 07:52
2032-Oct-05 09:01 < 00:01 Earth 0.304952982846791 0.304952161361451 0.304953804332251 12.1145126673794 12.1137914163418 2463510.876019506 0.077213780402717 50.1219365225659 38.7841566164344 -65.4640301633487 1070631.26237453 T 62 CATAB v2.0f-lin.ifort 2020-Oct-24 07:52:23 2020-Oct-24 07:52
2044-Oct-04 19:15 < 00:01 Earth 0.345552724911795 0.345551755324782 0.345553694498808 12.3969649633226 12.3963429587803 2467893.302049014 0.096514935945033 62.0606238342312 48.3491012456059 89.9868295930197 1005766.36687152 T 62 CATAB v2.0f-lin.ifort 2020-Oct-24 07:52:23 2020-Oct-24 07:52
2056-Oct-03 20:05 < 00:01 Earth 0.39588942245243 0.395888297640883 0.395890547264023 12.740603137913 12.7400748660566 2472275.337076867 0.120167601066336 73.5273973345462 55.4214372477502 79.7095266832345 1004299.59956756 T 62 CATAB v2.0f-lin.ifort 2020-Oct-24 07:52:23 2020-Oct-24 07:52
2068-Oct-02 07:17 < 00:01 Earth 0.454509907268038 0.454508633323324 0.454511181212855 13.1250974911082 13.1246508344068 2476656.803585999 0.158896572081125 82.7434219450377 62.3974109816498 77.325389720568 1036544.57068991 T 62 CATAB v2.0f-lin.ifort 2020-Oct-24 07:52:23 2020-Oct-24 07:52
2133-Oct-12 06:01 < 00:01 Earth 0.44569754850139 0.445695800775651 0.445699296230879 13.4074134656633 13.4069675688889 2500406.750648765 0.124045672317559 114.767431744736 44.0414532038717 -44.7983238753657 973547.395758188 T 62 CATAB v2.0f-lin.ifort 2020-Oct-24 07:52:23 2020-Oct-24 07:52
2145-Oct-11 05:29 < 00:01 Earth 0.386082898804323 0.386081237230755 0.38608456038351 12.9193552162317 12.9188210210938 2504788.728460439 0.10011550739976 118.661643991371 41.6115393009004 -49.8543928006291 935878.692236743 T 62 CATAB v2.0f-lin.ifort 2020-Oct-24 07:52:23 2020-Oct-24 07:52
2157-Oct-10 11:40 < 00:01 Earth 0.335293630705348 0.335292107036973 0.335295154381841 12.4939623445301 12.4933262847783 2509170.986244297 0.0811860602828802 121.884743265799 38.4288422940013 -55.4838126818062 927112.354737333 T 62 CATAB v2.0f-lin.ifort 2020-Oct-24 07:52:23 2020-Oct-24 07:52
2169-Oct-10 01:37 < 00:01 Earth 0.295178574691011 0.29517723301115 0.295179916381444 12.1773758954468 12.1766346073406 2513553.567585930 0.0695407922956678 123.521455313675 35.4228799552261 -61.3393329740714 935200.804681 T 62 CATAB v2.0f-lin.ifort 2020-Oct-24 07:52:23 2020-Oct-24 07:52
2181-Oct-09 19:12 < 00:01 Earth 0.265479876968589 0.265478741623615 0.265481012325847 11.9477767822629 11.9469367249498 2517936.300321011 0.0594761805502105 123.753404292973 32.5579034158304 -67.1750026814513 959686.579278507 T 62 CATAB v2.0f-lin.ifort 2020-Oct-24 07:52:23 2020-Oct-24 07:52
2193-Oct-09 14:10 < 00:01 Earth 0.245195054289576 0.245194112368318 0.24519599622349 11.7996371908916 11.7987162135498 2522319.090415221 0.0536506896382534 124.145728461329 30.2710930379325 -72.6456928228848 989412.754451012 T 62 CATAB v2.0f-lin.ifort 2020-Oct-24 07:52:23 2020-Oct-24 07:52
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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