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(2020 RV5)
Classification: Amor [NEO]          SPK-ID: 54054277
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 27 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .576111592406041 9.2013e-06  
a 2.503765146047984 5.6528e-05 au
q 1.061317020747536 9.2425e-07 au
i 2.754465013645401 3.1446e-05 deg
node 196.653768500132 2.8631e-05 deg
peri 188.6416895377785 2.1395e-05 deg
M 324.9273751517243 0.0011918 deg
tp 2459141.479050158378
(2020-Oct-18.97905016)
1.9145e-05 TDB
period 1447.067571263097
3.96
0.049006
0.0001342
d
yr
n .2487789838906887 8.4251e-06 deg/d
Q 3.946213271348431 8.9095e-05 au
  Orbit Determination Parameters
   # obs. used (total)      161  
   data-arc span      100 days  
   first obs. used      2020-08-12  
   last obs. used      2020-11-20  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .49734  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-20 05:22:24  

Additional Information
 Earth MOID = .0656327 au 
 Jupiter MOID = 1.51112 au 
 T_jup = 3.211 
[ 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 23.942   .40084 27 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
1914-Oct-16 05:48 8_01:29 Earth 0.023111625543662 0.0228782255436069 0.0254729322134374 7.48618266894243 7.47076677071912 2420421.741327709 11608.5648096373 395573.261379965 7.08975991900381 -81.8571811109189 506511.898817734 T 27 CATAB v2.0f-lin.ifort 2020-Nov-20 05:22:24 2020-Nov-20 05:22
1918-Aug-18 22:21 1_10:46 Earth 0.476463397878973 0.450690076117574 0.502240708679945 21.8554731689614 21.8552172955601 2421824.431437211 2085.75869542839 1287148.0414968 3.746890085667 -3.07294074597702 896494.62420379 T 27 CATAB v2.0f-lin.ifort 2020-Nov-20 05:22:24 2020-Nov-20 05:22
1957-Nov-20 03:33 2_17:45 Earth 0.164192281739172 0.136139278471508 0.192271452280037 12.0342979384141 12.032949400401 2436162.647888502 3944.94540964173 1403354.47116816 4.17115532094822 4.24077869741758 361764.295862658 T 27 CATAB v2.0f-lin.ifort 2020-Nov-20 05:22:24 2020-Nov-20 05:22
1961-Sep-04 15:50 2_08:07 Earth 0.241171683946522 0.212128081147723 0.270222190497613 14.4169110080645 14.416144661233 2437547.159917657 3366.77740143631 1449887.72269667 3.48627382080009 -2.59722873039079 386980.670271757 T 27 CATAB v2.0f-lin.ifort 2020-Nov-20 05:22:24 2020-Nov-20 05:22
2016-Nov-22 22:44 04:15 Earth 0.277357197160327 0.274870830557127 0.279843588732443 14.2610498314721 14.2603761855628 2457715.447021412 254.942540986297 124055.101900648 4.85499924547845 2.0130578656832 243554.34320411 T 27 CATAB v2.0f-lin.ifort 2020-Nov-20 05:22:24 2020-Nov-20 05:22
2020-Oct-18 17:19 < 00:01 Earth 0.066155242130571 0.0661524244252195 0.0661580598354901 6.62022965056753 6.61414305103689 2459141.221699319 0.0471641518673626 140.253926359348 2.80694358403541 0.240802127621615 40997.4310320049 T 27 CATAB v2.0f-lin.ifort 2020-Nov-20 05:22:24 2020-Nov-20 05:22
2024-Sep-15 01:32 05:30 Earth 0.198361414680667 0.19603041843329 0.200692405510202 11.5731938592515 11.5720331492924 2460568.564085483 329.915687950668 116225.725834127 3.08492234016717 0.29662203806046 36363.433236145 T 27 CATAB v2.0f-lin.ifort 2020-Nov-20 05:22:24 2020-Nov-20 05:22
2028-Aug-26 13:55 06:45 Earth 0.469515199222256 0.464774912341342 0.474255543276636 19.8925587115554 19.8922734290325 2462010.079733002 405.458223049766 236521.519022132 3.41391097636033 -2.01220125621862 616275.108200463 T 27 CATAB v2.0f-lin.ifort 2020-Nov-20 05:22:24 2020-Nov-20 05:22
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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