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(2019 TZ)
Classification: Apollo [NEO]          SPK-ID: 3873326
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

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For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer 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.


Orbital Elements at Epoch 2458759.5 (2019-Oct-03.0) TDB
Reference: JPL 2 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3842427716212725 0.0012121  
a 1.087389655279307 0.00095584 au
q .6695680403024861 0.00072961 au
i 1.240616065190662 0.0053935 deg
node 150.3685145934624 0.055516 deg
peri 326.6808971756074 0.057504 deg
M 298.26361445535 0.15217 deg
tp 2458830.525601632181
(2019-Dec-13.02560163)		 0.08142 TDB
period 414.1676964404167
1.13		 0.5461
0.001495		 d
yr
n .8692131305604869 0.0011461 deg/d
Q 1.505211270256128 0.0013231 au
   Orbit Determination Parameters
   # obs. used (total)      17  
   data-arc span      4 days  
   first obs. used      2019-10-02  
   last obs. used      2019-10-06  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .43709  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Oct-06 05:59:14  

Additional Information
 Earth MOID = .0155036 au 
 Jupiter MOID = 3.59204 au 
 T_jup = 5.629 
[ show covariance matrix ]

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

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 26.6   .38294 MPO492740 autocmod 2.8

[ 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
2013-Apr-28 21:01 8_00:38 Earth 0.0215852055504858 0.0202359018715222 0.179617425381342 11.015071865149 11.0038596887382 2456411.375849974 11558.402732096 8526774.32929877 336.656996775185 69.6894392589379 11960.1978012993 T 2 CATAB v2.0f-lin.ifort 2019-Oct-06 05:59:16 2019-Oct-06 05:59
2019-Oct-09 10:17 < 00:01 Earth 0.0206115656183192 0.0203965576257365 0.0208265651926579 11.6429622153943 11.6318539790569 2458765.928347388 0.43256576725215 10701.2094431251 23.4367396093395 -0.0588840365838323 195.262084857352 T 2 CATAB v2.0f-lin.ifort 2019-Oct-06 05:59:16 2019-Oct-06 05:59
2020-Aug-03 15:31 1_00:18 Earth 0.472208525553233 0.462531846837873 0.481885215249204 10.0395284801442 10.0389664270102 2459065.146423092 1458.32310198523 482550.477587762 894.935449535122 0.809315999691505 825.199276775038 T 2 CATAB v2.0f-lin.ifort 2019-Oct-06 05:59:16 2019-Oct-06 05:59
2021-Feb-15 20:25 3_12:17 Earth 0.293981281794639 0.290901931787783 0.297100552499526 11.2934466144489 11.2926440468801 2459261.350879895 5056.96168419093 230415.876741535 4036.67933570428 47.892884126156 5050.06405514676 T 2 CATAB v2.0f-lin.ifort 2019-Oct-06 05:59:16 2019-Oct-06 05:59
2021-Jun-02 13:21 2_22:05 Earth 0.352369504020612 0.344368948627522 0.360372745741647 8.14398745661307 8.14305891428854 2459368.056269249 4205.38408982274 401961.285675533 654.06192544719 7.01758263487668 6757.14081477391 T 2 CATAB v2.0f-lin.ifort 2019-Oct-06 05:59:16 2019-Oct-06 05:59
2022-May-18 11:34 2_03:25 Earth 0.40105787459934 0.355064366404449 0.447077563411086 23.1824755375688 23.182188956048 2459717.981808882 3085.28058815358 2299846.55593799 1003.98459952646 -4.01369511970019 3894.23597887447 T 2 CATAB v2.0f-lin.ifort 2019-Oct-06 05:59:16 2019-Oct-06 05:59
2024-May-28 22:56 9_06:31 Venus 0.0641327890176352 0.0097254531150097 0.191345134759796 12.4337294511295 12.4310059035099 2460459.455533392 13350.5151745015 6368186.63631437 1139.4369625762 8.75728527789462 1223.4016819235 T 2 CATAB v2.0f-lin.ifort 2019-Oct-06 05:59:16 2019-Oct-06 05:59
2030-Apr-25 03:32 8_19:43 Earth 0.104677444076171 0.0207143187490479 0.275024610429874 8.18536381478381 8.1822535040436 2462616.647511277 12702.6939691087 8559790.83191862 229.556600914747 11.4165785371195 21117.591980634 T 2 CATAB v2.0f-lin.ifort 2019-Oct-06 05:59:16 2019-Oct-06 05:59
2036-Sep-29 10:08 6_09:04 Earth 0.217333830876551 0.075163055582073 0.3605014223432 17.7066979447818 17.7060055465756 2464965.922227005 9183.82602677869 7152138.66992251 48.4851057855342 4.46337563335338 45334.8915094732 T 2 CATAB v2.0f-lin.ifort 2019-Oct-06 05:59:16 2019-Oct-06 05:59
2038-Jun-22 00:28 9_20:53 Earth 0.433383686674221 0.402514060822306 0.464262307966075 9.43309008100428 9.43243830132026 2465596.519140273 14213.4398945368 1542713.02029754 1147.70726553727 3.73979573931204 2638.95529228279 T 2 CATAB v2.0f-lin.ifort 2019-Oct-06 05:59:16 2019-Oct-06 05:59
2039-May-09 02:07 6_19:04 Earth 0.19358607079091 0.0613271932848237 0.328407926077841 16.9402903273857 16.939477819064 2465917.588265910 9783.7445956157 6751420.08031332 702.331861351043 -6.86781587632746 4741.45849561384 T 2 CATAB v2.0f-lin.ifort 2019-Oct-06 05:59:16 2019-Oct-06 05:59
2062-Oct-11 15:51 22:17 Earth 0.0381193847731683 0.0307354676843211 0.0455045712995916 10.2176940393938 10.2108508424873 2474474.160079212 1337.05552090028 368401.260208571 3693.60103493804 1.30417653115477 38.8349460124713 T 2 CATAB v2.0f-lin.ifort 2019-Oct-06 05:59:16 2019-Oct-06 05:59
2063-Jul-31 00:07 3_10:07 Earth 0.483241867916265 0.472792353293466 0.493793212930861 10.1876901885963 10.1871489564178 2474766.505078793 4927.2885128347 629720.994467799 1451.32365545372 33.7415413633578 16694.8899024443 T 2 CATAB v2.0f-lin.ifort 2019-Oct-06 05:59:16 2019-Oct-06 05:59
2065-May-22 08:21 4_22:10 Earth 0.492846427006473 0.367733699954791 0.618021072068202 25.9803558008553 25.9801477078947 2475427.848220334 7090.45189040362 6246486.79155812 1231.79399249002 -2.45687185116658 2376.96615696442 T 2 CATAB v2.0f-lin.ifort 2019-Oct-06 05:59:16 2019-Oct-06 05:59
2079-Oct-18 13:28 9_06:04 Earth 0.172612270685514 0.0651479567083549 0.284532752367627 6.1428587837717 6.14034539879056 2480690.061425773 13323.8579291348 5643358.69213121 1134.4285186498 -10.7626498441493 42627.5430864025 T 2 CATAB v2.0f-lin.ifort 2019-Oct-06 05:59:16 2019-Oct-06 05:59
2080-Sep-30 23:30 9_13:02 Mars 0.0483058495863786 0.0452862528634105 0.184763932596383 8.60782916052512 8.60714061891138 2481038.478842574 13741.5580214312 8094790.27883963 233.990919196447 -69.6517750273698 49859.8312611964 T 2 CATAB v2.0f-lin.ifort 2019-Oct-06 05:59:16 2019-Oct-06 05:59
2104-Oct-05 01:44 5_16:59 Earth 0.128063714813812 0.000304964307996874 0.28624091930661 15.0351399755275 15.0337560944439 2489807.572007359 8219.43944869274 7887498.90841606 292.27750347532 -0.145887329073787 125.769261342888 T 2 CATAB v2.0f-lin.ifort 2019-Oct-06 05:59:16 2019-Oct-06 05:59
2105-Aug-12 13:12 1_21:57 Earth 0.456577155195647 0.415424270505296 0.500307568727303 9.82967593223776 9.82908222534006 2490119.050149865 2756.94993099106 2722090.61008582 2384.07171921705 38.7724697047856 11613.4620395637 T 2 CATAB v2.0f-lin.ifort 2019-Oct-06 05:59:16 2019-Oct-06 05:59
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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