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(2013 BV15)
Classification: Apollo [NEO]          SPK-ID: 3624597
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

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.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 42 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3833975854314671 1.0638e-06  
a 1.49501585646708 2.2713e-06 au
q .921830386915845 2.1304e-07 au
i .5630689101745775 4.7089e-06 deg
node 177.9121306057908 0.00038152 deg
peri 8.579794244436162 0.00037389 deg
M 86.21331634023575 0.0034652 deg
tp 2459040.603493285509
(2020-Jul-10.10349329)		 0.0060623 TDB
period 667.6780903549594
1.83		 0.0015216
4.166e-06		 d
yr
n .5391819878477849 1.2288e-06 deg/d
Q 2.068201326018316 3.1422e-06 au
   Orbit Determination Parameters
   # obs. used (total)      149  
   # delay obs. used      3  
   # Doppler obs. used      4  
   data-arc span      26 days  
   first obs. used      2013-01-17  
   last obs. used      2013-02-12  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      3  
   norm. resid. RMS      .29566  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 07:34:38  

Additional Information
 Earth MOID = .00515375 au 
 Jupiter MOID = 2.88737 au 
 T_jup = 4.471 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456320.5 (2013-Jan-28.0) TDB
Reference: JPL 42 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3863116251845585 1.0569e-06  
q .9230294049296639 2.2493e-07 au
tp 2456369.749849013515
(2013-Mar-18.24984901)		 1.9996e-05 TDB
node 181.8663716042372 0.00046632 deg
peri 4.189312189613409 0.00045935 deg
i .5101041526157336 4.5923e-06 deg
   Orbit Determination Parameters
   # obs. used (total)      149  
   # delay obs. used      3  
   # Doppler obs. used      4  
   data-arc span      26 days  
   first obs. used      2013-01-17  
   last obs. used      2013-02-12  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      3  
   norm. resid. RMS      .29566  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 07:34:38  

Additional Information
 Jupiter MOID = 2.88737 au 
 T_jup = 4.471 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.11713406175781E-12 -2.172276858178113E-13 -7.816196022643544E-12 -9.897639693188345E-11 1.159464110167947E-10 1.566931197521413E-12
q -2.172276858178113E-13 5.059483512618304E-14 -1.749800002829739E-13 3.305023472205574E-13 -6.050625504307794E-12 -1.649707506787339E-13
tp -7.816196022643544E-12 -1.749800002829739E-13 3.998483239191042E-10 4.394890211096207E-9 -4.021069030707812E-9 -3.858878082439588E-11
node -9.897639693188345E-11 3.305023472205574E-13 4.394890211096207E-9 2.174583041555744E-7 -2.13751571726206E-7 -2.080873618778275E-9
peri 1.159464110167947E-10 -6.050625504307794E-12 -4.021069030707812E-9 -2.13751571726206E-7 2.110058391879563E-7 2.065964253576416E-9
i 1.566931197521413E-12 -1.649707506787339E-13 -3.858878082439588E-11 -2.080873618778275E-9 2.065964253576416E-9 2.108948242389769E-11

[ 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 MPO254838  

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