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(2013 BV15)
Classification: Apollo [NEO]          SPK-ID: 3624597
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 41 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3833976192482819 1.0642e-06  
a 1.495015973421662 2.2729e-06 au
q .9218304084736438 2.1324e-07 au
i .5630676500433831 4.7685e-06 deg
node 177.9122155827599 0.00038614 deg
peri 8.57970157990054 0.00037828 deg
M 86.21314039638905 0.0034676 deg
tp 2459040.603800838828
(2020-Jul-10.10380084)
0.0060666 TDB
period 667.6781687033056
1.83
0.0015226
4.169e-06
d
yr
n .539181924577756 1.2296e-06 deg/d
Q 2.06820153836968 3.1443e-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.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      3  
   norm. resid. RMS      .29707  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:47:09  

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 41 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3863116592669438 1.0574e-06  
q .9230294262950267 2.2509e-07 au
tp 2456369.749843143483
(2013-Mar-18.24984314)
2.0224e-05 TDB
node 181.8664754556385 0.00047189 deg
peri 4.189200705490194 0.00046469 deg
i .5101029511603606 4.6487e-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.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      3  
   norm. resid. RMS      .29707  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:47:09  

Additional Information
 Jupiter MOID = 2.88737 au 
 T_jup = 4.471 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.118113242559029E-12 -2.170161686991331E-13 -7.90542983775899E-12 -9.953460301854538E-11 1.164014198941463E-10 1.571502451978463E-12
q -2.170161686991331E-13 5.066542507716161E-14 -1.993111193013475E-13 -1.294770929963206E-13 -5.620026006878801E-12 -1.605622785511097E-13
tp -7.90542983775899E-12 -1.993111193013475E-13 4.090067638199841E-10 4.514482670198893E-9 -4.129817767701133E-9 -3.969803777960374E-11
node -9.953460301854538E-11 -1.294770929963206E-13 4.514482670198893E-9 2.226848670357618E-7 -2.18823038373211E-7 -2.132991406219876E-9
peri 1.164014198941463E-10 -5.620026006878801E-12 -4.129817767701133E-9 -2.18823038373211E-7 2.159351037413694E-7 2.116629975878586E-9
i 1.571502451978463E-12 -1.605622785511097E-13 -3.969803777960374E-11 -2.132991406219876E-9 2.116629975878586E-9 2.161029442599547E-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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