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(2008 TS26)
Classification: Apollo [NEO]          SPK-ID: 3430497
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2454748.5 (2008-Oct-09.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5690024724449811 0.0062508  
a 1.921982968654026 0.014123 au
q .8283699074927406 0.0059456 au
i .8112648169775671 0.31235 deg
node 16.42828736237761 0.12087 deg
peri 301.6450280744966 0.76536 deg
M 14.88524237016752 0.052727 deg
tp 2454708.258316691372
(2008-Aug-29.75831669)
0.313 TDB
period 973.2462280990754
2.66
10.727
0.02937
d
yr
n .3698961163231473 0.004077 deg/d
Q 3.015596029815312 0.022158 au
  Orbit Determination Parameters
   # obs. used (total)      19  
   first obs. used      2008-10-09  
   last obs. used      2008-10-09  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      9  
   norm. resid. RMS      .31335  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 09:02:36  

Additional Information
 Earth MOID = 7.31995E-5 au 
 Jupiter MOID = 2.31847 au 
 T_jup = 3.707 
[ 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 33.2   n/a MPO147535  

[ hide close-approach data ]
Close-Approach Data   ...sorted by Date/Time (TDB)
Date/Time (TDB) Time Uncertainty
(days_HH:MM)
Body Nominal Distance (au) Minimum Distance (au) Maximum Distance (au) V-relative (km/s) V-infinity (km/s) JD (TDB) Time Uncertainty (minutes) Semi-major axis (km) Semi-minor axis (km) range-LOV angle (deg) N-sigma BP Orbit Ref. Reference Modified
2008-Oct-09 03:30 00:03 Earth 8.44275210330355e-05 7.78899906770342e-05 9.08443677453154e-05 15.7604153753418 13.6114640533442 2454748.646041792 2.65301597285378 270.218007971934 7.78686516198614 -19.4213263181688 17.6240135769884 T 8 CATAB v2.0e-lin.ifort 2017-Nov-28 11:55:09 2018-Dec-11 15:14
2008-Oct-09 05:27 00:04 Moon 0.00263568077494915 0.00263206047073332 0.00263930796913742 12.9705559191163 12.9695972175817 2454748.727108624 4.00628208966095 279.087356685594 7.45721837136483 49.9785775840223 71455.9798484663 T 8 CATAB v2.0e-lin.ifort 2017-Nov-28 11:55:09 2018-Dec-11 15:14
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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