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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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Orbit Diagram
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Note: This Java-based orbit viewer will eventually be retired.

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 two-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 is not working, here are some notes that might help.
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 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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