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(2015 VR64)
Classification: Apollo [NEO]          SPK-ID: 3733859
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.


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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3764755699049949 0.00011977  
a 1.481684293842064 0.00025787 au
q .9238663548985931 1.668e-05 au
i 1.489485746829252 0.00051331 deg
node 217.1112978508532 0.00094023 deg
peri 234.7928931450543 0.0015223 deg
M 169.5925054543261 0.23259 deg
tp 2458690.161184440362
(2019-Jul-25.66118444)
0.3446 TDB
period 658.7671625121332
1.80
0.17198
0.0004709
d
yr
n .5464753261640748 0.00014266 deg/d
Q 2.039502232785535 0.00035495 au
  Orbit Determination Parameters
   # obs. used (total)      62  
   data-arc span      6 days  
   first obs. used      2015-11-06  
   last obs. used      2015-11-12  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .44734  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:30:50  

Additional Information
 Earth MOID = .00621414 au 
 Jupiter MOID = 3.17024 au 
 T_jup = 4.500 
[ 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 27.4   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
1903-Mar-02 19:47 9_09:43 Earth 0.405550363771105 0.118832069766879 0.693031038588244 19.6044361857764 19.6041010529904 2416176.324061692 13542.9904084941 14343328.2480106 55.9554936589825 2.50088134066478 41490.118525014 T 10 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:06 2018-Dec-11 16:46
1905-Apr-08 17:01 9_00:25 Mars 0.0856767483620869 0.0223465176366488 0.333256004429328 11.9348234488949 11.9345434654799 2416944.209249137 12985.0982325661 12456265.9752964 33.9542146920222 15.1207171090889 97858.7534900085 T 10 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:06 2018-Dec-11 16:46
1944-Oct-31 23:10 3_11:22 Earth 0.0825252918378922 0.0502778946237227 0.114779551911628 9.84923782889188 9.84595917967272 2431395.465067451 5002.22312015873 1608656.26951917 6.52748943421966 1.58855062796067 43579.8000290066 T 10 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:06 2018-Dec-11 16:46
1954-Feb-27 07:44 7_01:04 Earth 0.335084859257339 0.153555986683196 0.517158269906387 17.4864049308582 17.4859501913708 2434800.822530497 10143.5056443089 9090687.88280951 55.7315965838421 3.59434479204336 49006.7021955732 T 10 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:06 2018-Dec-11 16:46
1963-Jul-25 20:28 6_09:44 Mars 0.0550453902260346 0.0199326594446125 0.284174323094228 9.87295440046315 9.87242759570666 2438236.353067970 9224.44662088842 11577174.4027356 34.2476896708435 -21.2323532992324 89615.1869382843 T 10 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:06 2018-Dec-11 16:46
1975-Oct-17 06:59 9_18:19 Earth 0.306694675064444 0.0705889755535179 0.543103770347318 16.6449824149634 16.6444604641368 2442702.791067100 14058.6104911255 11791018.7282785 10.7069257294095 -1.55825785238459 102556.797462404 T 10 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:06 2018-Dec-11 16:46
1979-Apr-07 11:24 6_07:58 Mars 0.0910851821537991 0.0675691939075632 0.234721819268523 11.6696068592059 11.6693375152451 2443970.974663773 9118.04496669355 8163372.01244182 56.2031546941157 -47.8889090953973 179870.288405337 T 10 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:06 2018-Dec-11 16:46
2005-Feb-24 16:32 2_06:42 Earth 0.28280112856368 0.229072716109654 0.336593777129307 15.9095797840471 15.9089875674251 2453426.188962348 3281.89390894699 2689232.88588956 55.2773370770065 4.47696277501082 51606.0587190537 T 10 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:06 2018-Dec-11 16:46
2015-Nov-12 20:12 < 00:01 Earth 0.00781221800506115 0.00780520637261321 0.0078192294837523 7.4501739334152 7.40425285264699 2457339.341324723 0.0379898998401582 345.313292025589 1.8611755051142 -0.123529574768688 1974.02866929558 T 10 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:06 2018-Dec-11 16:46
2015-Nov-13 03:12 < 00:01 Moon 0.00949561027618632 0.0094887021522383 0.00950251850698418 8.21903496104209 8.21861502209343 2457339.633213771 0.348517939542081 348.125826409527 2.04196444592227 -8.34022412838848 93919.9027843758 T 10 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:06 2018-Dec-11 16:46
2043-Feb-05 18:23 7_06:51 Earth 0.0368045956540046 0.0252221909178968 0.0782166366558 8.04962428020552 8.04062562706052 2467286.265732887 10491.3287077285 2355947.30724626 47.7219833240654 43.3058930457199 78325.262198457 T 10 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:06 2018-Dec-11 16:46
2051-Sep-21 13:05 17:27 Earth 0.499476273907117 0.499301634342823 0.499652266646699 5.90301997064182 5.90211620362401 2470436.044879070 1047.15486213147 41924.6079227384 123.532066100723 -77.9359909713929 300293.256027537 T 10 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:06 2018-Dec-11 16:46
2052-Feb-23 23:05 00:58 Earth 0.238274991120222 0.238023915180019 0.238526096663193 14.5562302523722 14.5554620132164 2470591.461570480 57.911992045491 13202.7721339706 47.2433705701239 18.500842324552 220974.5076586 T 10 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:06 2018-Dec-11 16:46
2061-Mar-07 18:51 1_13:00 Earth 0.463186051001312 0.411792313931243 0.514584240681774 21.3212141711134 21.3209443675384 2473891.285709580 2219.56886903112 2563909.20968329 56.3887245973534 1.62184303143661 30722.8972368901 T 10 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:06 2018-Dec-11 16:46
2062-Oct-08 11:15 1_20:43 Earth 0.486187562543553 0.426124443013437 0.546259855005418 21.9492256392016 21.9489759545887 2474470.968759449 2682.78433289348 2997184.26034226 10.8632809609235 -2.02094656275969 214494.252833407 T 10 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:06 2018-Dec-11 16:46
2071-Oct-21 03:44 4_22:13 Earth 0.259797845859276 0.151647430495605 0.367955962370788 15.2560727689255 15.255400499085 2477770.655314916 7093.29485674093 5393677.18551016 10.6293013704337 -0.856227934678423 46931.8693395861 T 10 CATAB v2.0e-lin.ifort 2017-Nov-30 08:41:06 2018-Dec-11 16:46
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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