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(2016 GL135)
Classification: Apollo [NEO]          SPK-ID: 3750677
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5129549151007643 0.00025562  
a 1.441709837928841 0.00017044 au
q .7021776904141158 0.00028847 au
i 9.388775268789493 0.0072644 deg
node 55.86165230787656 0.015484 deg
peri 10.21274170483102 0.0037414 deg
M 341.5782186924078 0.18711 deg
tp 2459232.855218827023
(2021-Jan-18.35521883)
0.33436 TDB
period 632.2884081208789
1.73
0.11213
0.000307
d
yr
n .5693604301079901 0.00010097 deg/d
Q 2.181241985443567 0.00025787 au
  Orbit Determination Parameters
   # obs. used (total)      33  
   data-arc span      27 days  
   first obs. used      2016-04-03  
   last obs. used      2016-04-30  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      6  
   norm. resid. RMS      .28948  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 16:56:29  

Additional Information
 Earth MOID = .155776 au 
 Jupiter MOID = 3.16018 au 
 T_jup = 4.501 
[ 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 20.7   n/a MPO380433  

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