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JPL Small-Body Database Browser
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(2016 LV)
Classification: Apollo [NEO]          SPK-ID: 3753664
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 14 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5360975410533484 0.00020367  
a 2.005831086352748 0.0008378 au
q .9305099731906731 1.9885e-05 au
i 2.128185707786705 0.00064208 deg
node 83.73309408685232 0.00030286 deg
peri 126.7555060175775 0.00039708 deg
M 18.45483056698647 0.24016 deg
tp 2458547.307852406247
(2019-Mar-04.80785241)
0.6589 TDB
period 1037.623892792969
2.84
0.65009
0.00178
d
yr
n .3469465212785232 0.00021737 deg/d
Q 3.081152199514822 0.0012869 au
  Orbit Determination Parameters
   # obs. used (total)      188  
   data-arc span      14 days  
   first obs. used      2016-06-03  
   last obs. used      2016-06-17  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .3072  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:25:37  

Additional Information
 Earth MOID = .00832246 au 
 Jupiter MOID = 1.8847 au 
 T_jup = 3.642 
[ 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 23.1   n/a MPO386982  

[ 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
1999-Jun-29 06:34 9_12:52 Earth 0.296206405422731 0.101130517230838 0.491863416241857 19.365665070561 19.3652005652296 2451358.773857547 13732.1048612968 9764088.65815884 23.5161247989631 2.90900123767391 88693.8752975575 T 14 CATAB v2.0e-lin.ifort 2017-Nov-30 13:02:36 2018-Dec-11 16:59
2002-Feb-09 03:47 6_00:10 Earth 0.447266199546874 0.280989051286842 0.614549395674057 23.8039361889691 23.8036859241615 2452314.657502245 8650.07804945014 8383689.92619205 101.284312947317 -6.73018134429436 71229.8411687448 T 14 CATAB v2.0e-lin.ifort 2017-Nov-30 13:02:36 2018-Dec-11 16:59
2016-Jun-01 23:43 < 00:01 Earth 0.00927478436469549 0.00926538874248721 0.00928417988537412 10.3616389593101 10.3338762216522 2457541.488057578 0.0567405823291461 466.006840878548 3.52223933947823 -0.308012267675973 1922.81119367231 T 14 CATAB v2.0e-lin.ifort 2017-Nov-30 13:02:36 2018-Dec-11 16:59
2027-Dec-11 03:22 6_16:41 Mars 0.0570597972080008 0.0122165511958675 0.175104447336949 13.8060204877446 13.8056570641116 2461750.640528441 9641.2075844103 5931140.38532939 101.485316497584 12.3656284416217 18101.3551160403 T 14 CATAB v2.0e-lin.ifort 2017-Nov-30 13:02:36 2018-Dec-11 16:59
2033-Jun-27 09:00 9_17:11 Earth 0.279578374980224 0.0875671651280533 0.472205371712934 18.6425411592165 18.6420299371111 2463775.874915432 13991.218901022 9612481.78065 24.4229580728854 2.85698384943382 78753.2623031003 T 14 CATAB v2.0e-lin.ifort 2017-Nov-30 13:02:36 2018-Dec-11 16:59
2036-Feb-14 23:00 9_03:11 Earth 0.35842296845847 0.140138812131273 0.580845048998815 21.2276978345047 21.2273476336435 2464738.458192099 13151.043910557 11155149.6994541 102.686416379465 -7.82101674086951 65000.8629100465 T 14 CATAB v2.0e-lin.ifort 2017-Nov-30 13:02:36 2018-Dec-11 16:59
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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