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(2020 TE6)
Classification: Apollo [NEO]          SPK-ID: 54065913
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 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5397221510142035 0.00045365  
a 1.941455174215039 0.0017849 au
q .8936088114900431 5.9173e-05 au
i 1.849154802965861 0.0012168 deg
node 24.91409621288949 0.00013384 deg
peri 45.53400706344207 0.00079629 deg
M 296.5205902889252 0.089805 deg
tp 2459174.728764627149
(2020-Nov-21.22876463)
0.0062125 TDB
period 988.0740156730028
2.71
1.3626
0.003731
d
yr
n .3643451748448163 0.00050246 deg/d
Q 2.989301536940036 0.0027483 au
  Orbit Determination Parameters
   # obs. used (total)      35  
   data-arc span      2 days  
   first obs. used      2020-10-15  
   last obs. used      2020-10-17  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .34214  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Oct-18 08:07:20  

Additional Information
 Earth MOID = .000363599 au 
 Jupiter MOID = 2.33882 au 
 T_jup = 3.708 
[ 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 27.501   .2671 3 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
1975-Jan-07 16:01 4_08:05 Earth 0.0434049599720862 0.0344264838915087 0.057004717113125 9.76867389900829 9.76238785902506 2442420.167033843 6244.93674213642 910658.999150805 62.1655368774689 49.3675678383954 75059.5522538159 T 3 CATAB v2.0f-lin.ifort 2020-Oct-18 08:07:32 2020-Oct-18 08:07
2020-Oct-18 19:19 < 00:01 Earth 0.00153867023869454 0.00153494279292458 0.00154239717844179 10.7326540235066 10.5700761147246 2459141.304692113 0.179591387583453 180.49036390025 2.05458082696407 1.4585193751394 816.125839754044 T 3 CATAB v2.0f-lin.ifort 2020-Oct-18 08:07:32 2020-Oct-18 08:07
2020-Oct-18 23:40 < 00:01 Moon 0.000743684327614977 0.000740853807665861 0.000746525654537078 11.6565404585847 11.6527592475932 2459141.486188671 0.428775529687025 199.986881582449 2.20089043351038 -44.9814227807446 35686.6566298823 T 3 CATAB v2.0f-lin.ifort 2020-Oct-18 08:07:32 2020-Oct-18 08:07
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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