Skip Page Navigation
NASA JPL Caltech
NASA Logo - Jet Propulsion Laboratory + View the NASA Portal
+ Center for Near-Earth Object Studies
JPL Home Earth Solar System Stars & Galaxies Technology
JPL Solar System Dynamics
BODIES ORBITS EPHEMERIDES TOOLS PHYSICAL DATA DISCOVERY FAQ SITE MAP
JPL Small-Body Database Browser
Search: [ help ]  
(2014 MR5)
Classification: Aten [NEO]          SPK-ID: 3673866
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]
Orbit Diagram
[ switch to new HTML5 viewer ]

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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1355963229464489 0.00015748  
a .9539090899367615 0.00014199 au
q .8245625249161431 0.00011164 au
i 17.02407132331107 0.065767 deg
node 84.66829301061725 0.011569 deg
peri 19.20754378360268 0.063353 deg
M 293.3337616524775 0.59736 deg
tp 2459063.517672328114
(2020-Aug-02.01767233)
0.57871 TDB
period 340.2976169115738
0.93
0.075981
0.000208
d
yr
n 1.057897505328537 0.0002362 deg/d
Q 1.08325565495738 0.00016124 au
  Orbit Determination Parameters
   # obs. used (total)      19  
   data-arc span      3 days  
   first obs. used      2014-06-20  
   last obs. used      2014-06-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .73999  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:40:01  

Additional Information
 Earth MOID = .0572949 au 
 Jupiter MOID = 4.01718 au 
 T_jup = 6.266 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456829.5 (2014-Jun-21.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1355578194501697 0.00015707  
q .8245433755855212 0.00011156 au
tp 2456681.608481086466
(2014-Jan-24.10848109)
0.054996 TDB
node 84.70370350410616 0.011692 deg
peri 19.24552666042938 0.063448 deg
i 17.02750273614993 0.065768 deg
  Orbit Determination Parameters
   # obs. used (total)      19  
   data-arc span      3 days  
   first obs. used      2014-06-20  
   last obs. used      2014-06-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .73999  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:40:01  

Additional Information
 Jupiter MOID = 4.01718 au 
 T_jup = 6.266 
Orbit Covariance (6×6)
  e q tp node peri i
e 2.467072949260591E-8 -1.008114218280206E-8 8.596986762844846E-6 -1.642266409825096E-6 9.194095892138299E-6 9.331823319359743E-6
q -1.008114218280206E-8 1.244457538550573E-8 -3.039576495700529E-6 1.936670555684164E-7 -1.525756051978329E-6 -1.239808068669338E-6
tp 8.596986762844846E-6 -3.039576495700529E-6 .003024564664568099 -.0005993460086360484 .003332266351940367 .003397836250550194
node -1.642266409825096E-6 1.936670555684164E-7 -.0005993460086360484 .0001367021876984144 -.0007399107936285972 -.000768782495249358
peri 9.194095892138299E-6 -1.525756051978329E-6 .003332266351940367 -.0007399107936285972 .004025632160071805 .00416712325760159
i 9.331823319359743E-6 -1.239808068669338E-6 .003397836250550194 -.000768782495249358 .00416712325760159 .004325396398877831

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 24.3   n/a MPO298936  

[ 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
1961-Jul-16 22:52 9_08:33 Earth 0.35752539299487 0.191286296643673 0.627645819531265 12.0372230514323 12.0366039093476 2437497.452909831 13472.8162896852 14746258.623793 52660.6347940597 32.3412686218385 398.318818729811 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
1973-Jun-06 06:32 3_09:25 Earth 0.196229690281745 0.138423647368682 0.446309133716164 11.0346965634534 11.0334659788985 2441839.772524395 4885.17038501347 14237746.8261895 25548.3336347107 -45.0539971498329 526.45742350108 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
1986-Jun-05 20:40 11:01 Earth 0.391739875431996 0.295031409281483 0.494421128963133 15.725086608029 15.7246540668071 2446587.361284465 660.805153503321 5527695.19823636 38869.6476452879 -25.017750518473 482.647029436771 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
1987-Jun-13 21:11 5_11:02 Earth 0.0583527545034945 0.0577261416192096 0.140160942871286 8.79942877282223 8.7942380883907 2446960.382961973 7862.22235652999 6016312.64582218 10239.7584221727 -83.1141509305219 496.772036735749 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
1988-Jul-14 05:00 3_03:39 Earth 0.336135283190815 0.263316938811344 0.415863102448245 11.6069071979888 11.6062242391651 2447356.708606688 4538.97992243819 4502480.68767482 51107.1222775406 31.4247645204447 373.813588852509 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
2000-Jun-05 05:29 13:19 Earth 0.238524143681535 0.191247433526111 0.294861236012946 11.9238051234327 11.9228682472384 2451700.728603396 799.076447896005 3478506.3187603 29386.9158017054 -40.8253299602031 534.75182166429 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
2001-Jun-23 22:26 3_13:06 Earth 0.143137707106073 0.106744725630901 0.189188597662802 8.98238930505221 8.98031670008582 2452084.434396103 5105.56750096478 2778898.19416321 26097.2193199775 40.132030179765 367.746980306096 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
2001-Nov-13 13:04 8_00:39 Earth 0.217737197866343 0.195500644794736 0.251617329926424 10.9341127289455 10.9329935013536 2452227.044654499 11559.4316371307 2889213.41870864 14270.3693805224 60.192010066988 983.901228177628 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
2002-Jul-27 06:41 10:36 Earth 0.471900977909482 0.430111496594803 0.514759088215621 14.9743109753148 14.9739339069484 2452482.778712474 636.340291289661 2389580.10642152 62508.0805992708 27.8604766354999 406.470170802774 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
2008-Jun-18 11:32 2_00:35 Venus 0.114133978955173 0.109808468239451 0.126148999919132 8.48573858695031 8.48349614233151 2454635.980708767 2914.54979774172 1551515.72894194 13103.2587566083 -74.3307707367846 3380.54296149111 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
2010-Apr-17 08:43 1_19:05 Venus 0.127378275390523 0.123670118097282 0.139972000737528 8.36586035429718 8.36382229941959 2455303.863465239 2585.22909687634 1753785.22783495 5256.48872191274 76.245759350448 1073.39256269747 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
2013-Jun-06 07:38 01:13 Earth 0.431504543299899 0.428335684384475 0.434703876877273 16.8054662877975 16.8050988522543 2456449.818209307 72.9112807269019 243359.861503195 31195.7089719689 -49.8300672153347 1193.01570060156 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
2014-Jun-11 15:06 00:04 Earth 0.0733901533752861 0.0726004503594947 0.0741798414047722 9.0400342993571 9.0360173071932 2456820.129158546 4.07643111499416 39344.1684172487 2532.029229507 -0.291233012999917 173.975018120413 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
2014-Dec-14 04:26 22:00 Earth 0.152909439426231 0.15259987994753 0.153222948103048 10.5996036726345 10.5979595957773 2457005.684731203 1320.48958275338 235349.14307158 15317.1149338888 -89.4456356203497 1093.60496931773 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
2015-Jul-11 03:16 10:35 Earth 0.303603774862889 0.300527555513304 0.30675722608568 11.0088018698756 11.0080046449667 2457214.636115956 634.728827168532 290398.506031839 27517.7945914655 58.0753373729286 1003.66907591136 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
2015-Oct-04 03:14 1_01:12 Earth 0.342830787577463 0.340223456674175 0.345585327147236 10.8937484500092 10.8930349903542 2457299.634436721 1511.98112328438 383950.732735505 23536.312551533 69.9206331722715 1269.4987374137 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
2027-Jun-05 15:17 01:00 Earth 0.289046617877152 0.2422410689037 0.339025268115905 13.1008416748654 13.1001380244803 2461562.136846446 60.0394215405954 2847918.97021374 34325.1880753769 -31.5808436914265 466.338714321877 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
2028-Jun-19 16:16 4_00:24 Earth 0.101275125835667 0.0776807627961738 0.147763219250571 8.74149982771079 8.73848960661384 2461942.177955058 5783.7525404406 3024932.88454483 19152.3230673645 50.0009349002499 409.962333778689 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
2029-Jul-23 13:38 1_03:52 Earth 0.424424537564463 0.377852053926073 0.473730323779394 13.6177331431728 13.6172721288645 2462341.067992646 1672.45111856227 2933530.24050592 55111.5835330962 35.174959907474 497.717661117809 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
2041-Jan-28 02:35 8_20:35 Venus 0.135653871282958 0.116028421624674 0.223002152657209 8.73324087057539 8.73140768302786 2466547.607729151 12755.174905896 6001974.75615521 11441.3243776203 -58.955987627663 5277.90942925637 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
2041-Jun-08 11:50 2_16:49 Earth 0.12645690959914 0.100343530764832 0.226116470358484 9.79503836186969 9.7928870104993 2466678.992959549 3888.96989088163 6278216.2098995 17009.6232148845 -52.7238357185576 528.935359347156 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
2042-Jul-04 08:46 5_08:12 Earth 0.246458855237544 0.179096414165735 0.326229930996041 10.1123594587999 10.1112903094163 2467069.865366508 7692.41596008434 4599963.18183221 38965.2983302355 35.1667623978334 389.95035948498 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
2054-Jun-05 11:51 08:51 Earth 0.338430509043888 0.235005449009555 0.452690276364176 14.3356885421071 14.3351393394728 2471423.994013964 531.265125456991 6216886.32028512 37043.4925563656 -27.5064580037663 462.552189966741 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
2055-Jun-17 00:58 7_19:02 Earth 0.0690469759309421 0.0623466770879976 0.176899099267853 8.67545305005569 8.67100379902326 2471800.540031331 11221.9212129968 6800137.44398571 13843.288638073 65.0853364217561 434.668976827435 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
2056-Jul-19 06:42 3_09:44 Earth 0.382407335235851 0.291059543805335 0.48610580280966 12.5699865436044 12.5694322231481 2472198.779301795 4904.08133266432 5957396.8772595 53609.300769012 33.9615843812198 440.129694067496 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
2068-Jun-06 15:31 3_01:25 Earth 0.171197607628767 0.125289194445207 0.347413443122672 10.5602844506789 10.5588105461366 2476539.146399991 4404.87622923461 10353981.1019582 22883.6753127233 -47.2346704491402 519.380955245623 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
2081-Jun-05 11:54 16:17 Earth 0.359050507393081 0.216128970056765 0.52095089314147 14.8744714612213 14.8739725508264 2481285.996116458 976.871950500563 8656277.26576323 37834.0494820877 -25.6899069911837 457.627465916794 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
2083-Jul-18 09:06 5_09:12 Earth 0.368226344675454 0.245487468568214 0.518191968526404 12.2629085702119 12.2623184853697 2482058.879185194 7751.49774648228 8463092.24405953 52395.22088959 33.5879528316496 427.37316259672 T 3 CATAB v2.0e-lin.ifort 2017-Nov-29 16:10:33 2018-Dec-11 16:18
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
ABOUT SSD CREDITS/AWARDS PRIVACY/COPYRIGHT GLOSSARY LINKS
FirstGov 2020-Sep-24 16:06 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin