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(2020 VZ6)
Classification: Apollo [NEO]          SPK-ID: 54096685
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

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 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .532927014500039 3.5336e-05  
a 2.009489335146291 0.00014769 au
q .9385781830971102 2.0239e-06 au
i .4842895332093373 7.2597e-05 deg
node 238.1819756972924 0.0013863 deg
peri 223.9916169237563 0.0013979 deg
M 356.5136650200629 0.00049755 deg
tp 2459210.576126192812
(2020-Dec-27.07612619)
0.00032738 TDB
period 1040.463825274152
2.85
0.11471
0.0003141
d
yr
n .3459995352602898 3.8146e-05 deg/d
Q 3.080400487195472 0.0002264 au
  Orbit Determination Parameters
   # obs. used (total)      76  
   data-arc span      21 days  
   first obs. used      2020-11-14  
   last obs. used      2020-12-05  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .44729  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Dec-06 05:25:14  

Additional Information
 Earth MOID = .00190404 au 
 Jupiter MOID = 2.10604 au 
 T_jup = 3.641 
[ 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 25.0   .27787 E2021-CC3 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
1980-Jun-06 20:17 1_19:20 Mars 0.0436949164842074 0.0402121503219013 0.0614611938140012 14.8469438936269 14.8465025827207 2444397.345194181 2599.8828073119 1465405.20349608 20.2162206534143 66.9706416825959 296933.409229115 T 5 CATAB v2.0f-lin.ifort 2020-Dec-06 05:25:14 2020-Dec-06 05:25
1983-Feb-14 11:33 5_06:07 Earth 0.120545630838161 0.0658621960151233 0.175550644594983 12.251288459977 12.2494841502155 2445379.981077849 7566.77221117427 2752439.75595347 15.6738407449181 5.82105612701812 101357.768359696 T 5 CATAB v2.0f-lin.ifort 2020-Dec-06 05:25:14 2020-Dec-06 05:25
1985-Nov-19 11:10 6_13:57 Earth 0.103578851246377 0.0394662891454304 0.167688353746259 11.7669691494016 11.7647828129265 2446388.965366099 9477.36183934464 3196834.60901741 3.43681069849022 -0.734517982919564 48431.3377622793 T 5 CATAB v2.0f-lin.ifort 2020-Dec-06 05:25:14 2020-Dec-06 05:25
2018-Feb-28 22:17 09:02 Earth 0.290614956432844 0.284510553361234 0.296719652432625 17.8345809401381 17.8340668518078 2458178.428326379 542.305391572598 304756.711616068 16.447734693616 2.76940475716495 111910.05435756 T 5 CATAB v2.0f-lin.ifort 2020-Dec-06 05:25:14 2020-Dec-06 05:25
2020-Sep-30 20:49 00:11 Mars 0.0678735230405144 0.0678593807918555 0.0678876682434305 15.697130742827 15.6968620294814 2459123.367136284 11.4663698236035 998.193666696026 18.4655679190361 -45.0551166267768 374120.388744774 T 5 CATAB v2.0f-lin.ifort 2020-Dec-06 05:25:14 2020-Dec-06 05:25
2020-Dec-03 06:44 < 00:01 Moon 0.00221749772330835 0.00221736403885141 0.00221763145402721 8.03214961702525 8.030309380899 2459186.780425222 0.0396133285780742 17.4650976788219 0.961869225596585 67.8041225523687 307011.138958949 T 5 CATAB v2.0f-lin.ifort 2020-Dec-06 05:25:14 2020-Dec-06 05:25
2020-Dec-03 10:06 < 00:01 Earth 0.00233258297302377 0.00233223309712275 0.00233293284545312 9.00434902983696 8.87658308915562 2459186.920941395 0.0691016908914832 16.8530691126735 0.991032966049577 -1.15158391469094 11530.0135244709 T 5 CATAB v2.0f-lin.ifort 2020-Dec-06 05:25:14 2020-Dec-06 05:25
2038-Feb-26 09:00 2_09:31 Earth 0.212022608686875 0.177052630118258 0.247000116462094 15.6171319643412 15.6163272530555 2465480.875185909 3450.51418991703 1745136.91758196 16.8343004135434 2.10904021357236 60325.2367483553 T 5 CATAB v2.0f-lin.ifort 2020-Dec-06 05:25:14 2020-Dec-06 05:25
2040-Oct-23 18:22 2_01:17 Earth 0.496495302660828 0.457962552094774 0.535028898764483 24.1430549194989 24.1428326361201 2466451.265368878 2956.81372314469 1921765.18011649 6.87446200180941 0.997738957295461 168742.818527442 T 5 CATAB v2.0f-lin.ifort 2020-Dec-06 05:25:14 2020-Dec-06 05:25
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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