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(2016 TB57)
Classification: Apollo [NEO]          SPK-ID: 3761035
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

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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.


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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 34 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1231560910237497 4.6715e-07  
a 1.102215396105623 5.0078e-07 au
q .9664708564550604 7.6023e-08 au
i .2983616900486701 9.6255e-07 deg
node 294.8246411911154 0.00017114 deg
peri 147.8366998183811 0.00017118 deg
M 359.0343141809594 0.00072526 deg
tp 2459001.633787043303
(2020-Jun-01.13378704)
0.00085228 TDB
period 422.6668006730031
1.16
0.00028805
7.886e-07
d
yr
n .851734745730632 5.8046e-07 deg/d
Q 1.237959935756185 5.6245e-07 au
  Orbit Determination Parameters
   # obs. used (total)      140  
   # delay obs. used      0  
   # Doppler obs. used      1  
   data-arc span      201 days  
   first obs. used      2016-09-12  
   last obs. used      2017-04-01  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      3  
   norm. resid. RMS      .38619  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-May-10 06:25:57  

Additional Information
 Earth MOID = 1.44709E-5 au 
 Jupiter MOID = 3.86974 au 
 T_jup = 5.634 
[ 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 26.1   n/a MPO419551  

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