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(2014 GC49)
Classification: Aten [NEO]          SPK-ID: 3667477
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 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6440016495444012 0.00079267  
a .7348058733394155 3.3247e-05 au
q .2615896788139176 0.00059425 au
i 6.428775521164979 0.016261 deg
node 193.2797028811371 0.00086328 deg
peri 207.5537160916248 0.012783 deg
M 327.1798416921342 0.16789 deg
tp 2459221.474688808094
(2021-Jan-06.97468881)
0.10872 TDB
period 230.0686029629605
0.63
0.015614
4.275e-05
d
yr
n 1.564750667251879 0.0001062 deg/d
Q 1.208022067864913 5.4658e-05 au
  Orbit Determination Parameters
   # obs. used (total)      13  
   data-arc span      1 day  
   first obs. used      2014-04-04  
   last obs. used      2014-04-05  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      6  
   norm. resid. RMS      .75221  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 09:45:23  

Additional Information
 Earth MOID = .000318845 au 
 Jupiter MOID = 4.21272 au 
 T_jup = 7.653 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456752.5 (2014-Apr-05.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6443053481291834 0.00079172  
q .2613510536148968 0.00059348 au
tp 2456690.849335797784
(2014-Feb-02.34933580)
0.064632 TDB
node 193.3256785408697 0.00065113 deg
peri 207.5065140322313 0.012622 deg
i 6.436687081144865 0.016248 deg
  Orbit Determination Parameters
   # obs. used (total)      13  
   data-arc span      1 day  
   first obs. used      2014-04-04  
   last obs. used      2014-04-05  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      6  
   norm. resid. RMS      .75221  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 09:45:23  

Additional Information
 Jupiter MOID = 4.21272 au 
 T_jup = 7.653 
Orbit Covariance (6×6)
  e q tp node peri i
e 6.268283534231968E-7 -4.698728728421315E-7 5.116691056737291E-5 3.795215080690706E-7 -9.985471861065368E-6 1.285133326496772E-5
q -4.698728728421315E-7 3.522195939775269E-7 -3.835420106898707E-5 -2.84141580865327E-7 7.485663425753083E-6 -9.633931623968265E-6
tp 5.116691056737291E-5 -3.835420106898707E-5 .00417730866462767 3.132936565597626E-5 -.0008147152508512838 .001048489185567838
node 3.795215080690706E-7 -2.84141580865327E-7 3.132936565597626E-5 4.239757468004815E-7 -5.848188552031852E-6 7.482998519507191E-6
peri -9.985471861065368E-6 7.485663425753083E-6 -.0008147152508512838 -5.848188552031852E-6 .0001593233897658084 -.0002050308706088565
i 1.285133326496772E-5 -9.633931623968265E-6 .001048489185567838 7.482998519507191E-6 -.0002050308706088565 .0002639999629573563

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 28.6   n/a MPO290464  

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