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(2016 TP93)
Classification: Centaur          SPK-ID: 3761427
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 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5546570877829372 1.3226e-05  
a 7.391337988218947 0.00023193 au
q 3.291679984854032 5.9037e-06 au
i 138.2835367967026 6.8773e-05 deg
node 347.2948605954729 3.9646e-05 deg
peri 331.9251247673553 0.00019103 deg
M 65.51602943292657 0.0030888 deg
tp 2457664.741063391760
(2016-Oct-03.24106339)
0.00092495 TDB
period 7339.779613342875
20.10
0.34546
0.0009458
d
yr
n .04904779420700336 2.3085e-06 deg/d
Q 11.49099599158386 0.00036057 au
  Orbit Determination Parameters
   # obs. used (total)      54  
   data-arc span      607 days (1.66 yr)  
   first obs. used      2015-11-29  
   last obs. used      2017-07-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .47129  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Sep-07 09:06:50  

Additional Information
 Earth MOID = 2.33776 au 
 Jupiter MOID = 1.52543 au 
 T_jup = -0.777 
[ 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 15.746   .30696 4 autocmod 2.8

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