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JPL Small-Body Database Browser
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(2014 TX57)
Classification: Amor [NEO]          SPK-ID: 3693427
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 56 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4490985440993984 2.7883e-08  
a 1.86963970314948 6.9908e-08 au
q 1.029987234474617 3.7172e-08 au
i 11.77300178935723 5.7723e-06 deg
node 235.0071665220398 6.0609e-06 deg
peri 208.1885756675539 1.5302e-05 deg
M 254.5254527554274 3.5718e-05 deg
tp 2458874.077564513568
(2020-Jan-25.57756451)
0.00010787 TDB
period 933.7600947128254
2.56
5.2372e-05
1.434e-07
d
yr
n .3855380006474968 2.1624e-08 deg/d
Q 2.709292171824343 1.013e-07 au
  Orbit Determination Parameters
   # obs. used (total)      333  
   # delay obs. used      0  
   # Doppler obs. used      1  
   data-arc span      1779 days (4.87 yr)  
   first obs. used      2014-10-07  
   last obs. used      2019-08-21  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .30246  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Aug-21 05:18:09  

Additional Information
 Earth MOID = .0692764 au 
 Jupiter MOID = 2.5883 au 
 T_jup = 3.832 
[ 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 21.2   n/a E2015A35  
rotation period rot_per 5.421 h n/a LCDB (Rev. 2019-January); Warner et al., 2009 Published Reference List:
[Warner, B.D. (2015) Minor Planet Bull. 42, 115-127.]

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