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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 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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