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(2013 TV135)
Classification: Apollo [NEO, PHA]          SPK-ID: 3651198
Ephemeris | Orbit Diagram | Orbital Elements | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2457000.5 (2014-Dec-09.0) TDB
Reference: JPL 59 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5913595627908189 1.2701e-05  
a 2.43089106225854 7.5096e-05 AU
q .9933603864892206 2.597e-07 AU
i 6.75152269021055 0.00011092 deg
node 333.437600873487 0.00059393 deg
peri 23.6871120187438 0.00047848 deg
M 115.5811004080614 0.0053269 deg
tp 2456556.041725094083
(2013-Sep-20.54172509)
0.00013045 JED
period 1384.352445176846
3.79
0.064149
0.0001756
d
yr
n .2600493835614321 1.205e-05 deg/d
Q 3.868421738027861 0.00011951 AU
  Orbit Determination Parameters
   # obs. used (total)      949  
   data-arc span      108 days  
   first obs. used      2013-10-12  
   last obs. used      2014-01-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-BIG16  
   condition code      4  
   fit RMS      .28198  
   data source      ORB  
   producer      Otto Matic  
   solution date      2015-Apr-15 06:15:03  

Additional Information
 Earth MOID = .0107804 AU 
 T_jup = 3.235 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Physical Parameters | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 19.5 mag n/a MPO281957  

[ 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
1945-Aug-22 03:44 1_21:17 Earth 0.0201249982069021 0.0039992278580471 0.0446577009218539 10.2996047148325 10.2867421606917 2431689.655820868 2717.02731741915 881629.641676619 50.3306937533675 11.229959166101 7784.04181606365 T 59 CATAB v2.0c-linF95 2015-Apr-15 06:15:09 2015-Apr-15 06:15
1960-Oct-16 13:38 1_21:06 Earth 0.113782507374979 0.0899684471715072 0.141659472212758 11.100857138536 11.0987474341109 2437224.068172428 2705.95187619739 1378765.72505706 43.9355902957473 -37.0950336488207 164782.620766853 T 59 CATAB v2.0c-linF95 2015-Apr-15 06:15:09 2015-Apr-15 06:15
1992-Oct-26 11:05 3_00:32 Jupiter 1.62422302521387 1.62282412205887 1.62563344498085 3.10494090049586 2.93217838011816 2448921.961598700 4351.555518713 17372.0293124043 10.3331740945685 28.9531516503984 586844.153036603 T 59 CATAB v2.0c-linF95 2015-Apr-15 06:15:09 2015-Apr-15 06:15
1994-Oct-31 02:39 08:44 Earth 0.24792346864141 0.232518051035003 0.26336358477744 15.0356674153277 15.0349526189714 2449656.610193946 524.192647878441 750988.824047648 55.3358341463833 -18.4421368487726 170236.883124165 T 59 CATAB v2.0c-linF95 2015-Apr-15 06:15:09 2015-Apr-15 06:15
2004-Feb-05 22:34 14:32 Jupiter 1.78208146832632 1.78119372149626 1.78297752299179 3.22135625490447 3.07026660498227 2453041.440517018 872.248482870456 14927.5613845586 12.6246800412816 -15.4363475703006 298468.506025677 T 59 CATAB v2.0c-linF95 2015-Apr-15 06:15:09 2015-Apr-15 06:15
2013-Sep-16 17:13 < 00:01 Earth 0.0447618567115854 0.0447579873481671 0.0447657259935624 8.81037469720731 8.80361578971648 2456552.217692951 0.437938995963036 166.095778841332 16.6979328646328 -3.51803495379586 29060.8588564875 T 59 CATAB v2.0c-linF95 2015-Apr-15 06:15:09 2015-Apr-15 06:15
2047-Aug-19 06:13 1_06:20 Earth 0.0377305279180121 0.0158137221461314 0.0587360791775842 10.8335020813134 10.8269815749833 2468941.758701434 1819.76997814939 778447.650056375 53.8556466158182 2.85418841358956 3519.68960945296 T 59 CATAB v2.0c-linF95 2015-Apr-15 06:15:09 2015-Apr-15 06:15
2115-Jul-19 21:37 07:36 Earth 0.410311759565217 0.383997106200877 0.436558257604101 21.8582339974329 21.8579369086372 2493747.400628726 456.204770764539 1275356.91679855 81.2749348789472 4.69693108930645 55017.6248782436 T 59 CATAB v2.0c-linF95 2015-Apr-15 06:15:09 2015-Apr-15 06:15
Ephemeris | Orbit Diagram | Orbital Elements | Physical Parameters | Close-Approach Data ]
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