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(2002 LR24)
Classification: Apollo [NEO]          SPK-ID: 3127399
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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 12 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2026777019775196 0.00030743  
a 1.253617884047645 0.00049945 au
q .9995374921509472 1.2833e-05 au
i 20.0041641281328 0.031489 deg
node 256.4413382583997 0.0047569 deg
peri 38.57877338892359 0.010187 deg
M 267.8414685493387 3.6935 deg
tp 2459131.743934201378
(2020-Oct-09.24393420)
5.3384 TDB
period 512.679787413833
1.40
0.30638
0.0008388
d
yr
n .7021926918866601 0.00041963 deg/d
Q 1.507698275944342 0.00060067 au
  Orbit Determination Parameters
   # obs. used (total)      43  
   data-arc span      7 days  
   first obs. used      2002-06-08  
   last obs. used      2002-06-15  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .66719  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 09:15:05  

Additional Information
 Earth MOID = .021634 au 
 Jupiter MOID = 3.64603 au 
 T_jup = 5.054 
[ 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 24.3   n/a MPO32039  

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