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(2000 LG6)
Classification: Aten [NEO]          SPK-ID: 3042555
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 12 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1106319987404861 8.5938e-07  
a .9172698139037533 2.2491e-05 au
q .8157904210072673 2.0783e-05 au
i 2.829739957053455 0.0026337 deg
node 72.5453917757692 0.013924 deg
peri 8.164591656756558 0.026466 deg
M 311.0656338270869 0.10758 deg
tp 2459244.116975378232
(2021-Jan-29.61697538)
0.094284 TDB
period 320.8810568972909
0.88
0.011802
3.231e-05
d
yr
n 1.121911039189922 4.1262e-05 deg/d
Q 1.018749206800239 2.4979e-05 au
  Orbit Determination Parameters
   # obs. used (total)      12  
   data-arc span      3 days  
   first obs. used      2000-06-04  
   last obs. used      2000-06-07  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      6  
   norm. resid. RMS      .93703  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-14 20:56:39  

Additional Information
 Earth MOID = .00152846 au 
 Jupiter MOID = 4.06021 au 
 T_jup = 6.506 
[ hide covariance matrix ]
Orbital Elements at Epoch 2451701.5 (2000-Jun-06.0) TDB
Reference: JPL 12 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1236658910121748 6.1688e-05  
q .7951322183054718 9.774e-05 au
tp 2451550.911945468069
(2000-Jan-07.41194547)
0.011444 TDB
node 73.92655725960637 5.1887e-05 deg
peri 7.997879312755081 0.0013494 deg
i 3.08058768656983 0.0019446 deg
  Orbit Determination Parameters
   # obs. used (total)      12  
   data-arc span      3 days  
   first obs. used      2000-06-04  
   last obs. used      2000-06-07  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      6  
   norm. resid. RMS      .93703  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-14 20:56:39  

Additional Information
 Jupiter MOID = 4.06021 au 
 T_jup = 6.506 
Orbit Covariance (6×6)
  e q tp node peri i
e 3.80536341930817E-9 -6.029350270933348E-9 7.048416414049243E-7 -3.157981267057194E-9 -7.473109360101613E-8 1.1992026716423E-7
q -6.029350270933348E-9 9.553119296857406E-9 -1.116725043828001E-6 5.003930972648405E-9 1.184536037942932E-7 -1.90008650484159E-7
tp 7.048416414049243E-7 -1.116725043828001E-6 .0001309647761534942 -5.818699736501787E-7 -1.346052159987198E-5 2.218607310137968E-5
node -3.157981267057194E-9 5.003930972648405E-9 -5.818699736501787E-7 2.692274352726775E-9 6.479257867780295E-8 -9.968732570702544E-8
peri -7.473109360101613E-8 1.184536037942932E-7 -1.346052159987198E-5 6.479257867780295E-8 1.821013694796175E-6 -2.379012256613868E-6
i 1.1992026716423E-7 -1.90008650484159E-7 2.218607310137968E-5 -9.968732570702544E-8 -2.379012256613868E-6 3.781314281977333E-6

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 29.0   n/a MPO01663  

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