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(2017 TC1)
Classification: Apollo [NEO]          SPK-ID: 3782059
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458029.5 (2017-Oct-03.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .9695289870703989 0.00022194  
a 2.489970639167797 0.009728 au
q .07587192754040901 0.0002562 au
i 9.288061353112155 0.0035624 deg
node 274.3660039745766 0.095957 deg
peri 253.0705217336933 0.066416 deg
M 347.5260992041125 0.078056 deg
tp 2458079.226689903706
(2017-Nov-21.72668990)
0.019752 TDB
period 1435.125119099564
3.93
8.4103
0.02303
d
yr
n .2508492083435022 0.0014701 deg/d
Q 4.904069350795185 0.01916 au
  Orbit Determination Parameters
   # obs. used (total)      54  
   data-arc span      22 days  
   first obs. used      2017-10-01  
   last obs. used      2017-10-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .46565  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Nov-06 06:17:49  

Additional Information
 Earth MOID = .114589 au 
 Jupiter MOID = .866535 au 
 T_jup = 2.424 
[ 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 20.9   n/a MPO428364  

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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