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

[ hide orbit diagram ]
Orbit Diagram
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 2-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 has stopped working because of a recent Java upgrade, here is a possible workaround.
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 2457000.5 (2014-Dec-09.0) TDB
Reference: JPL 60 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5913595627896366 1.2701e-05  
a 2.430891062277483 7.5096e-05 AU
q .993360386499835 2.597e-07 AU
i 6.751522690166895 0.00011092 deg
node 333.4376008736552 0.00059393 deg
peri 23.68711201926817 0.00047848 deg
M 115.5811004066475 0.0053269 deg
tp 2456556.041725094325
(2013-Sep-20.54172509)
0.00013045 JED
period 1384.352445193027
3.79
0.064149
0.0001756
d
yr
n .2600493835583925 1.205e-05 deg/d
Q 3.86842173805513 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-Jun-04 14:53:42  

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 0.020124991555354 0.00399922727312564 0.0446576927702578 10.2996045541147 10.2867419955191 2431689.655822362 2717.02736048945 881629.574806495 50.3306924245565 11.2299612841893 7784.0408147445 T 60 CATAB v2.0c-linF95 2015-Jun-04 14:53:45 2015-Jun-04 14:53
1960-Oct-16 13:38 1_21:06 Earth 0.113782513986582 0.0899684521661351 0.141659480015863 11.1008573979568 11.0987476937037 2437224.068173779 2705.95171024534 1378765.77836183 43.9355913465985 -37.0950320596856 164782.622292864 T 60 CATAB v2.0c-linF95 2015-Jun-04 14:53:45 2015-Jun-04 14:53
1992-Oct-26 11:05 3_00:32 Jupiter 1.62422302541919 1.62282412278476 1.62563344467157 3.10494093960412 2.93217842155314 2448921.961591781 4351.55542096017 17372.0301944891 10.333174724961 28.9531496263339 586844.086853578 T 60 CATAB v2.0c-linF95 2015-Jun-04 14:53:45 2015-Jun-04 14:53
1994-Oct-31 02:39 08:44 Earth 0.247923471205552 0.232518053544502 0.263363587395056 15.035667481402 15.0349526850563 2449656.610193921 524.192641456386 750988.826951312 55.3358342348209 -18.4421366729486 170236.883311657 T 60 CATAB v2.0c-linF95 2015-Jun-04 14:53:45 2015-Jun-04 14:53
2004-Feb-05 22:34 14:32 Jupiter 1.78208146814071 1.78119372128878 1.78297752282771 3.2213562437511 3.07026659326391 2453041.440516016 872.248510183106 14927.5612868398 12.6246799060226 -15.4363475461917 298468.507678291 T 60 CATAB v2.0c-linF95 2015-Jun-04 14:53:45 2015-Jun-04 14:53
2013-Sep-16 17:13 < 00:01 Earth 0.0447618567116257 0.0447579873482077 0.0447657259936023 8.81037469708069 8.80361578958977 2456552.217692853 0.437938996149083 166.095778860372 16.6979328578463 -3.51803494753854 29060.8588431488 T 60 CATAB v2.0c-linF95 2015-Jun-04 14:53:45 2015-Jun-04 14:53
2047-Aug-19 06:13 1_06:20 Earth 0.0377305315498516 0.0158137255910054 0.0587360830148436 10.8335021842077 10.8269816785674 2468941.758700905 1819.76993148026 778447.663884866 53.8556470728335 2.85418884277617 3519.69049424134 T 60 CATAB v2.0c-linF95 2015-Jun-04 14:53:45 2015-Jun-04 14:53
2115-Jul-19 21:37 07:36 Earth 0.410311769363423 0.383996869994175 0.436558512193863 21.8582342787198 21.8579371899351 2493747.400628192 456.209830737872 1275368.88169235 81.2748964149284 4.69692610129129 55017.5939974022 T 60 CATAB v2.0c-linF95 2015-Jun-04 14:53:45 2015-Jun-04 14:53
Ephemeris | Orbit Diagram | Orbital Elements | Physical Parameters | Close-Approach Data ]
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