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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 ]

[ show orbit diagram ]
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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