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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 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .532927015066597 3.5336e-05  
a 2.009489337165169 0.00014769 au
q .9385781829015812 2.0239e-06 au
i .4842895189228856 7.2597e-05 deg
node 238.1819789256523 0.0013863 deg
peri 223.9916136826997 0.0013979 deg
M 356.5136650134406 0.00049755 deg
tp 2459210.576126227137
(2020-Dec-27.07612623)
0.00032738 TDB
period 1040.46382684214
2.85
0.11471
0.0003141
d
yr
n .3459995347388656 3.8146e-05 deg/d
Q 3.080400491428758 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.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      5  
   norm. resid. RMS      .44729  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 23:17:14  

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_19:21 Mars 0.043694861544883 0.0402121575811924 0.0614683428148001 14.8469417054291 14.8465003938968 2444397.345185346 2600.76540608751 1465884.12231451 20.2162392919006 66.9708356741194 296933.193132837 T 6 CATAB v2.0g-lin.ifort 2021-Apr-15 23:17:14 2021-Apr-15 23:17
1983-Feb-14 11:33 5_06:09 Earth 0.120545368075638 0.06584887424032 0.175563638392435 12.2512797378066 12.2494754228268 2445379.981051906 7568.61603563297 2753102.42273602 15.6738319542695 5.82106903969452 101357.830428557 T 6 CATAB v2.0g-lin.ifort 2021-Apr-15 23:17:14 2021-Apr-15 23:17
1985-Nov-19 11:10 6_13:59 Earth 0.103579158690538 0.0394539899772461 0.167701266062889 11.7669790454213 11.764792717275 2446388.965334767 9479.20017268083 3197463.16015302 3.43683366557224 -0.734523118028045 48431.5169328164 T 6 CATAB v2.0g-lin.ifort 2021-Apr-15 23:17:14 2021-Apr-15 23:17
2018-Feb-28 22:17 09:02 Earth 0.290614923485344 0.28451052088989 0.296719619009036 17.8345799465983 17.834065858181 2458178.428324417 542.305401173088 304756.687923487 16.4477341307119 2.76940506259738 111910.056752979 T 6 CATAB v2.0g-lin.ifort 2021-Apr-15 23:17:14 2021-Apr-15 23:17
2020-Sep-30 20:49 00:11 Mars 0.0678735226017379 0.0678593803545362 0.067887667803193 15.697130751621 15.69686203827 2459123.367136464 11.4663681495057 998.193562457646 18.4655678072365 -45.0551165506048 374120.388535509 T 6 CATAB v2.0g-lin.ifort 2021-Apr-15 23:17:14 2021-Apr-15 23:17
2020-Dec-03 06:44 < 00:01 Moon 0.00221749773130161 0.00221736404686713 0.00221763146199802 8.03214962854925 8.03030939241264 2459186.780425134 0.0396132962947457 17.4650952497066 0.961869227900849 67.8041232981006 307011.141446314 T 6 CATAB v2.0g-lin.ifort 2021-Apr-15 23:17:14 2021-Apr-15 23:17
2020-Dec-03 10:06 < 00:01 Earth 0.00233258297609901 0.00233223310024646 0.00233293284847977 9.0043490452553 8.87658310494265 2459186.920941203 0.0691015972956383 16.8530667726214 0.991032965774788 -1.15158294720317 11530.0150956528 T 6 CATAB v2.0g-lin.ifort 2021-Apr-15 23:17:14 2021-Apr-15 23:17
2038-Feb-26 09:00 2_09:31 Earth 0.21202242778111 0.177050745255938 0.247001640296665 15.6171266919719 15.6163219797278 2465480.875174709 3450.68034344411 1745221.96856879 16.8342936212252 2.10904323052276 60325.298305558 T 6 CATAB v2.0g-lin.ifort 2021-Apr-15 23:17:14 2021-Apr-15 23:17
2040-Oct-23 18:22 2_01:17 Earth 0.49649549986718 0.457960189373276 0.535031656027574 24.143060990489 24.1428387072543 2466451.265357190 2957.01355503172 1921892.86005202 6.87440823605908 0.997747801761182 168745.702238494 T 6 CATAB v2.0g-lin.ifort 2021-Apr-15 23:17:14 2021-Apr-15 23:17
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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