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(2015 VM64)
Classification: Apollo [NEO]          SPK-ID: 3733853
[ 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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6202772846134578 0.00051717  
a 1.886717604451484 0.0022752 au
q .7164295319299098 0.00011181 au
i 16.3097170978266 0.01115 deg
node 46.03832624100892 0.0011396 deg
peri 76.71960033620101 0.0037971 deg
M 254.7839226452676 1.1061 deg
tp 2459277.154911812656
(2021-Mar-03.65491181)		 3.4087 TDB
period 946.583172044822
2.59		 1.7122
0.004688		 d
yr
n .380315233390768 0.00068794 deg/d
Q 3.057005676973059 0.0036865 au
   Orbit Determination Parameters
   # obs. used (total)      91  
   data-arc span      4 days  
   first obs. used      2015-11-07  
   last obs. used      2015-11-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .48181  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:30:53  

Additional Information
 Earth MOID = .0124379 au 
 Jupiter MOID = 2.30516 au 
 T_jup = 3.665 
[ 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 26.1   n/a MPO361299  

[ 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
1906-Nov-09 19:55 17:42 Earth 0.018122236499239 0.0062238363944401 0.0300379587445903 18.976693026857 18.9689436154986 2417524.330076696 1061.52090673436 594414.357114453 18.8532473339691 -2.06885682846972 4771.76370736888 T 9 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:00 2018-Dec-11 16:46
1907-Apr-05 08:31 09:44 Mars 0.0597480714589415 0.0494041503056468 0.0718294633013733 18.4675005831742 18.4672411191052 2417670.854588986 584.27511116975 756731.901529616 127.569262470575 -41.4426400548314 46295.1612524689 T 9 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:00 2018-Dec-11 16:46
1912-Apr-22 16:05 1_17:51 Earth 0.24844520110631 0.210721648752288 0.288812204608136 23.8039046439362 23.8034540994777 2419515.170115680 2510.88270057855 2329890.70809884 234.0224623099 -32.8482464490606 84114.2322812989 T 9 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:00 2018-Dec-11 16:46
1919-Nov-01 12:48 4_11:28 Earth 0.165365352557181 0.077131877958986 0.253643252113728 22.9634640604766 22.9627623837556 2422264.033549430 6448.18401358177 4403029.38461768 14.6484684524061 1.5146507645285 42064.5013110471 T 9 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:00 2018-Dec-11 16:46
1925-Apr-14 22:40 5_03:26 Earth 0.140092278010173 0.136057300841606 0.199544746580736 19.0668000344605 19.0658024912697 2424255.444358040 7406.17561603177 5615107.24933208 239.423792603817 -76.2245381395023 85867.0506450451 T 9 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:00 2018-Dec-11 16:46
1932-Oct-24 13:58 6_08:20 Earth 0.309706829389837 0.166609254153354 0.452908561006736 26.9601306512789 26.9598115400015 2427005.082047053 9140.41173342661 7143911.25374624 15.2831530891638 2.02777084025798 100186.776690154 T 9 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:00 2018-Dec-11 16:46
1938-Apr-08 10:07 8_23:14 Earth 0.165363931460585 0.134150174964975 0.298982434845841 15.5687966331299 15.5677616555125 2428996.921778667 12913.810339546 8502834.52423505 230.20802466707 54.2191034592529 94553.9111709875 T 9 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:00 2018-Dec-11 16:46
1945-Oct-16 19:50 7_15:35 Earth 0.468920678437674 0.275937331768503 0.662136273559961 31.4975528274172 31.497372427056 2431745.326205313 11014.7362792029 9643143.37031277 18.0917676423854 2.82512830713108 177972.618620929 T 9 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:00 2018-Dec-11 16:46
2015-Nov-10 21:57 < 00:01 Earth 0.0140286189526521 0.0139975727667814 0.0140596649879432 18.6322290129372 18.6220325046981 2457337.414561259 0.0241572884838821 1546.44568385232 4.17010074686495 0.0595893801714208 1069.82681963065 T 9 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:00 2018-Dec-11 16:46
2021-Apr-22 10:07 7_18:47 Earth 0.212848270102912 0.120714092829459 0.369998524145485 23.0304751575239 23.0299316013178 2459326.921584330 11207.3894254438 8698883.70982469 242.115148737322 -34.551167893494 73031.7693236054 T 9 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:00 2018-Dec-11 16:46
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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