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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 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3654029747449724 1.8887e-05  
a .9492388248760176 1.3535e-07 au
q .602384134522899 1.8014e-05 au
i 4.749620893591434 0.00040855 deg
node 195.0159416134757 5.2419e-05 deg
peri 304.6499202112401 0.00068621 deg
M 77.76827373882588 0.0017189 deg
tp 2459127.527096868445
(2020-Oct-05.02709687)
0.0015974 TDB
period 337.8015720856136
0.92
7.2249e-05
1.978e-07
d
yr
n 1.065714400845832 2.2793e-07 deg/d
Q 1.296093515229136 1.8481e-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 = .00821436 au 
 Jupiter MOID = 3.72991 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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