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JPL Small-Body Database Browser
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(2017 VF14)
Classification: Apollo [NEO]          SPK-ID: 3789391
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4450025026472701 0.00028225  
a 1.456948238189592 0.000583 au
q .8086026259676925 8.7663e-05 au
i .4411523830412671 0.00026953 deg
node 65.35113862188319 0.00065426 deg
peri 279.8735896013749 0.0014438 deg
M 187.0568883521076 0.33265 deg
tp 2459309.078297575679
(2021-Apr-04.57829758)
0.77875 TDB
period 642.3394726088716
1.76
0.38555
0.001056
d
yr
n .5604513117306251 0.0003364 deg/d
Q 2.105293850411492 0.00084243 au
  Orbit Determination Parameters
   # obs. used (total)      33  
   data-arc span      6 days  
   first obs. used      2017-11-15  
   last obs. used      2017-11-21  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .59726  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Apr-18 07:27:28  

Additional Information
 Earth MOID = .00183063 au 
 Jupiter MOID = 3.31716 au 
 T_jup = 4.519 
[ 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 28.5   n/a MPO473489  

[ 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
1959-Mar-17 08:57 2_19:50 Mars 0.0929714431078483 0.0468846517060396 0.169231707922713 9.82810260637088 9.82778928223146 2436644.872592737 4070.27025550154 4105166.4650825 146.007079875636 30.2863474651688 46731.6535922173 T 4 CATAB v2.0e-lin.ifort 2019-Apr-18 07:27:31 2019-Apr-18 07:34
1967-May-20 07:28 5_18:42 Mars 0.0406768788931871 0.00381105180206182 0.331173352284451 8.01158055827849 8.01070201295111 2439630.811413738 8322.18561350369 14493760.1515663 43.4372099658658 -5.38199125084254 13307.3066497948 T 4 CATAB v2.0e-lin.ifort 2019-Apr-18 07:27:31 2019-Apr-18 07:34
1985-Jun-23 09:12 8_22:41 Earth 0.054254113646617 0.000151179102096936 0.174453545009328 13.4548120806439 13.4511615082265 2446239.883250008 12881.0042603678 5993747.71146956 75.1828999439044 0.179329485103576 211.378853223727 T 4 CATAB v2.0e-lin.ifort 2019-Apr-18 07:27:31 2019-Apr-18 07:34
1994-Dec-07 13:32 2_08:21 Mars 0.0625322283069039 0.0466684261440113 0.187082785461162 8.02165400005003 8.02108323968473 2449694.063810831 3380.74078395431 6958877.43314932 163.768887979378 -48.2767179278896 43554.7460938167 T 4 CATAB v2.0e-lin.ifort 2019-Apr-18 07:27:31 2019-Apr-18 07:34
2003-Feb-10 10:29 4_01:15 Mars 0.0628378814849593 0.00298579063212596 0.168040019509284 9.56230596876031 9.56182950175013 2452680.936761621 5835.43357829612 5248208.16275945 33.9123452691296 2.72727600695989 12780.624711852 T 4 CATAB v2.0e-lin.ifort 2019-Apr-18 07:27:31 2019-Apr-18 07:34
2007-Jan-11 17:36 9_11:40 Venus 0.128980435190685 0.0385902716769865 0.219281807260098 7.08746492170657 7.08508902812413 2454112.233648058 13659.6929139695 4502016.10589191 90.4877613440007 -1.5554163109584 3235.19829474181 T 4 CATAB v2.0e-lin.ifort 2019-Apr-18 07:27:31 2019-Apr-18 07:34
2010-Jun-19 07:02 4_17:44 Earth 0.123805452144519 0.0466075967215305 0.200996681658565 15.500700991087 15.4993125076647 2455366.792789013 6824.48871351697 3849114.73176593 81.0980477925701 0.0429193737731123 60.9908029047643 T 4 CATAB v2.0e-lin.ifort 2019-Apr-18 07:27:31 2019-Apr-18 07:34
2017-Nov-13 12:26 < 00:01 Moon 0.00242542423837685 0.00242381036071672 0.00242704320536436 12.8789250746782 12.8778758484649 2458071.018270594 0.311510914155629 192.922685433105 2.31670702656243 -65.322909969485 149098.761575383 T 4 CATAB v2.0e-lin.ifort 2019-Apr-18 07:27:31 2019-Apr-18 07:34
2017-Nov-13 15:30 < 00:01 Earth 0.00204483054232693 0.00204110182387508 0.0020485590241977 11.9202559451935 11.8104376754661 2458071.146015446 0.249375756299106 182.634772396553 1.95386909798287 -0.318628008254169 1121.11386583643 T 4 CATAB v2.0e-lin.ifort 2019-Apr-18 07:27:31 2019-Apr-18 07:34
2024-Nov-27 04:30 4_02:37 Earth 0.216989735025287 0.138132564516675 0.295850197772069 18.3826378542659 18.381969859243 2460641.687176607 5917.44161626104 3932596.21650827 20.3186210909139 0.706286711848368 17594.425092038 T 4 CATAB v2.0e-lin.ifort 2019-Apr-18 07:27:31 2019-Apr-18 07:34
2026-Dec-01 23:05 2_09:24 Mars 0.064602619511023 0.0384685642359905 0.128682264481424 9.24220313866233 9.24172363512544 2461376.461532782 3443.97219666788 3535420.42415903 106.780115079521 36.5494841523326 52605.2993236476 T 4 CATAB v2.0e-lin.ifort 2019-Apr-18 07:27:31 2019-Apr-18 07:34
2031-Dec-08 22:19 6_17:54 Earth 0.439075980818039 0.297406080920404 0.580794448038367 25.0840752935901 25.0838333708598 2463209.429655125 9714.40495807492 7069467.55773777 34.0526153665575 1.78579817629008 55058.0551810433 T 4 CATAB v2.0e-lin.ifort 2019-Apr-18 07:27:31 2019-Apr-18 07:34
2033-Mar-14 07:16 2_18:52 Mars 0.0093429013290296 0.00321111490222807 0.130061904829222 8.32367165150456 8.31998946691886 2463670.802698931 4012.40341097773 6046247.27302515 38.2579444135171 -20.1240625383017 12494.915876216 T 4 CATAB v2.0e-lin.ifort 2019-Apr-18 07:27:31 2019-Apr-18 07:34
2033-Jun-06 03:27 7_17:25 Earth 0.338298971658018 0.179778470149887 0.496821158283431 21.7644230504754 21.7640611675182 2463754.643987690 11124.6780049761 7904908.17314232 67.6402860477922 0.392898131483428 4592.50747642884 T 4 CATAB v2.0e-lin.ifort 2019-Apr-18 07:27:31 2019-Apr-18 07:34
2040-Jun-19 02:45 8_17:25 Earth 0.0999690144790019 0.00230088737922027 0.23125892412267 14.7833745391501 14.7815715220292 2466324.614665702 12565.0278838392 6547516.0489315 52.0988927894528 1.32890229464006 6044.77965866626 T 4 CATAB v2.0e-lin.ifort 2019-Apr-18 07:27:31 2019-Apr-18 07:34
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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