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(2014 EB25)
Classification: Apollo [NEO]          SPK-ID: 3663826
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2456728.5 (2014-Mar-12.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4211797936658173 0.023138  
a 1.379116063612455 0.040783 au
q .7982602444989468 0.0088774 au
i 10.98585816617038 0.51404 deg
node 352.6351380541152 0.010073 deg
peri 252.0847486821415 0.55161 deg
M 327.8598603660588 1.8683 deg
tp 2456781.313495303969
(2014-May-03.81349530)		 0.74011 TDB
period 591.5611607782354
1.62		 26.24
0.07184		 d
yr
n .6085592223911348 0.026994 deg/d
Q 1.959971882725962 0.05796 au
   Orbit Determination Parameters
   # obs. used (total)      12  
   first obs. used      2014-03-12  
   last obs. used      2014-03-12  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      9  
   norm. resid. RMS      .49803  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 09:30:33  

Additional Information
 Earth MOID = .00478385 au 
 Jupiter MOID = 3.11612 au 
 T_jup = 4.690 
[ hide covariance matrix ]
Orbit Covariance (6×6)
  e q tp node peri i
e .0005353647818094311 -.0001957062717894566 -.01621105128000862 .000182540107153755 .004033083505859013 .01187142076409827
q -.0001957062717894566 7.880799443658524E-5 .005283122725939417 -4.985065319588522E-5 -.002885035975189837 -.004254936584029693
tp -.01621105128000862 .005283122725939417 .5477662219834631 -.007020775601597433 .00270128689730272 -.3669692238702585
node .000182540107153755 -4.985065319588522E-5 -.007020775601597433 .0001014648712406825 -.001901677155178707 .00424452184848461
peri .004033083505859013 -.002885035975189837 .00270128689730272 -.001901677155178707 .3042685411454719 .07297921340827244
i .01187142076409827 -.004254936584029693 -.3669692238702585 .00424452184848461 .07297921340827244 .2642326880910998

[ 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 27.1   n/a MPO286775  

[ 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
2014-Mar-14 04:46 01:13 Moon 0.0071851637906042 0.00630451048686935 0.00807501696776647 13.6684056181983 13.6680719079481 2456730.698362770 73.1372442405535 45968.7204501002 176.323538065377 -16.0814297174701 2272.57317610584 T 5 CATAB v2.0g-lin.ifort 2021-Apr-15 09:30:34 2021-Apr-15 09:30
2014-Mar-14 09:56 01:17 Earth 0.00703765856028753 0.00609997781772784 0.00797483812392258 13.3016307197143 13.2731372932837 2456730.914066248 77.1004871890438 46651.7597478543 2072.46506784915 -3.91086914137338 33.5279629586341 T 5 CATAB v2.0g-lin.ifort 2021-Apr-15 09:30:34 2021-Apr-15 09:30
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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