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(2008 VM)
Classification: Apollo [NEO]          SPK-ID: 3435552
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2454773.5 (2008-Nov-03.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3927650913013643 0.005061  
a 1.334394687981559 0.0079564 au
q .8102910365244266 0.0019251 au
i 4.088569220436611 0.052002 deg
node 42.01155018078764 0.0035667 deg
peri 69.17059125056484 0.055976 deg
M 327.2608899255694 0.38528 deg
tp 2454824.702274415797
(2008-Dec-24.20227442)
0.14484 TDB
period 563.021375589651
1.54
5.0356
0.01379
d
yr
n .6394073397710217 0.0057187 deg/d
Q 1.858498339438692 0.011081 au
  Orbit Determination Parameters
   # obs. used (total)      18  
   first obs. used      2008-11-03  
   last obs. used      2008-11-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      9  
   norm. resid. RMS      .87819  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 09:02:17  

Additional Information
 Earth MOID = .000312716 au 
 Jupiter MOID = 3.2738 au 
 T_jup = 4.828 
[ 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 30.2   n/a MPO147609  

[ 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-Nov-03 22:31 00:09 Earth 0.000309028348723821 0.000288965174158947 0.000329017537050289 11.0414646993849 10.2308212670327 2454774.437901463 9.15799304915532 964.537291395625 44.1089671910093 -18.7844143564991 155.60443643842 T 6 CATAB v2.0e-lin.ifort 2017-Nov-28 12:46:18 2018-Dec-11 15:17
2008-Nov-04 00:03 00:11 Moon 0.00253010671097422 0.00251519423306092 0.00254522455951988 11.6158706550398 11.6147554646631 2454774.502235625 10.499111081464 1365.35735917021 70.166555076127 56.8177270966972 10375.9378833187 T 6 CATAB v2.0e-lin.ifort 2017-Nov-28 12:46:18 2018-Dec-11 15:17
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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