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(2005 TE49 = 2017 TV1)
Classification: Aten [NEO]          SPK-ID: 3293831
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

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.


Orbital Elements at Epoch 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3654189921713744 1.8892e-05  
a .9492244188564746 1.3672e-07 au
q .602359788373483 1.8019e-05 au
i 4.750052466674892 0.00040861 deg
node 195.0074541620432 5.229e-05 deg
peri 304.6716445923004 0.00068592 deg
M 286.6256289741685 0.0017635 deg
tp 2459465.348371230341
(2021-Sep-07.84837123)
0.0016695 TDB
period 337.7938822016907
0.92
7.2982e-05
1.998e-07
d
yr
n 1.065738661853711 2.3026e-07 deg/d
Q 1.296089049339466 1.8668e-07 au
  Orbit Determination Parameters
   # obs. used (total)      35  
   data-arc span      4389 days (12.02 yr)  
   first obs. used      2005-10-07  
   last obs. used      2017-10-13  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      2  
   norm. resid. RMS      .69825  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-14 22:56:17  

Additional Information
 Earth MOID = .00837299 au 
 Jupiter MOID = 3.72947 au 
 T_jup = 6.274 
[ 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 26.7   n/a MPO87828  

[ show close-approach data ]
Alternate Designations
 2005 TE49 = 2017 TV1 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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