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(2020 DV3)
Classification: Apollo [NEO]          SPK-ID: 54005666
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

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Orbit Diagram
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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 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4691035012237648 0.00033672  
a 1.481975542435798 0.00074367 au
q .786775626751177 0.00010422 au
i 1.086269652999826 0.00072021 deg
node 164.2341707110939 0.00048166 deg
peri 282.5453481728775 0.0012176 deg
M 78.24682880271494 0.06421 deg
tp 2458857.273220719248
(2020-Jan-08.77322072)
0.009725 TDB
period 658.9614087885133
1.80
0.49601
0.001358
d
yr
n .5463142381309589 0.00041122 deg/d
Q 2.177175458120418 0.0010925 au
  Orbit Determination Parameters
   # obs. used (total)      32  
   data-arc span      6 days  
   first obs. used      2020-02-27  
   last obs. used      2020-03-04  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .5287  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Mar-04 05:53:00  

Additional Information
 Earth MOID = .0027235 au 
 Jupiter MOID = 3.06516 au 
 T_jup = 4.454 
[ 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 27.842   .38734 4 autocmod 2.8

[ 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
2011-Feb-26 06:30 9_11:22 Earth 0.0173560975672751 0.00274458755097472 0.13392401572724 12.4668529040576 12.4545326947911 2455618.771108571 13642.4673074532 5822319.45656717 32.2844996110551 9.15358905903029 12589.8204490809 T 4 CATAB v2.0f-lin.ifort 2020-Mar-04 05:53:01 2020-Mar-04 05:53
2020-Feb-24 21:56 00:02 Moon 0.0025859215524732 0.00258023629013298 0.00259160683824669 12.0403705177434 12.0393178712245 2458904.413806490 1.50826595795165 283.768353900572 16.740305667977 -2.69356825458233 1624.39020742573 T 4 CATAB v2.0f-lin.ifort 2020-Mar-04 05:53:01 2020-Mar-04 05:53
2020-Feb-25 07:15 < 00:01 Earth 0.00272007423805068 0.00271450874267282 0.00272563942474528 12.0598900430633 11.9783899309686 2458904.801892128 0.58864414767071 273.708406102163 7.46917686151823 0.144608998304405 988.427886584823 T 4 CATAB v2.0f-lin.ifort 2020-Mar-04 05:53:01 2020-Mar-04 05:53
2029-Mar-06 04:36 7_14:17 Earth 0.139297094030028 0.0106272228508143 0.268107404955065 16.1402188147975 16.1390336552286 2462201.691557770 10936.9091453798 6423534.52046503 21.2293433836994 0.901136129086306 13981.7272745614 T 4 CATAB v2.0f-lin.ifort 2020-Mar-04 05:53:01 2020-Mar-04 05:53
2029-May-26 22:10 3_13:03 Mars 0.0512637012092619 0.00765377170798285 0.145957443850254 13.5744293458118 13.5740179297638 2462283.423563167 5102.49693782057 4740669.43339294 423.852869324639 -8.59630804878783 2678.1404324242 T 4 CATAB v2.0f-lin.ifort 2020-Mar-04 05:53:01 2020-Mar-04 05:53
2030-Sep-18 00:56 7_08:07 Earth 0.365367536598283 0.220727407636791 0.510056148750026 22.8286057324608 22.8282862801377 2462762.538771422 10566.5782151894 7216879.7979539 218.070642673905 1.55819065719106 6236.32890043988 T 4 CATAB v2.0f-lin.ifort 2020-Mar-04 05:53:01 2020-Mar-04 05:53
2066-Nov-16 06:13 2_21:54 Earth 0.165297670156992 0.158887133614819 0.174587243056148 9.34733349427707 9.34560885626691 2475970.759060230 4193.72687342408 1158447.79880178 1557.37120834939 70.0717217350739 11980.1909918138 T 4 CATAB v2.0f-lin.ifort 2020-Mar-04 05:53:01 2020-Mar-04 05:53
2119-Sep-06 06:13 8_11:08 Mars 0.0238270467449622 0.0140419901304928 0.123584877131631 12.440294744654 12.4393288669086 2495256.759349041 12187.7851527805 5163347.84757301 738.437286930749 36.1547880720683 2854.80438013135 T 4 CATAB v2.0f-lin.ifort 2020-Mar-04 05:53:01 2020-Mar-04 05:53
2124-Sep-16 12:22 2_23:41 Venus 0.079329828029844 0.0792351613289537 0.0903777877402485 6.6724243612193 6.66832059750772 2497094.015000161 4300.92507334194 2045664.94437906 2980.2153545084 88.3120413404126 2599.60902831612 T 4 CATAB v2.0f-lin.ifort 2020-Mar-04 05:53:01 2020-Mar-04 05:53
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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