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58690 (1998 BP10)
Classification: Main-belt Asteroid          SPK-ID: 2058690
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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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 19 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1698923873383649 3.7419e-08  
a 2.332512434666324 8.5788e-09 au
q 1.93623632864444 8.7838e-08 au
i 6.747194990873416 3.4091e-06 deg
node 120.7467051555902 3.7719e-05 deg
peri 303.4784976357406 3.9384e-05 deg
M 199.9655990375244 1.1923e-05 deg
tp 2459778.922563848656
(2022-Jul-18.42256385)
4.4263e-05 TDB
period 1301.171009065369
3.56
7.1784e-06
1.965e-08
d
yr
n .2766738556975596 1.5264e-09 deg/d
Q 2.728788540688208 1.0036e-08 au
  Orbit Determination Parameters
   # obs. used (total)      735  
   data-arc span      13790 days (37.75 yr)  
   first obs. used      1982-08-21  
   last obs. used      2020-05-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .53045  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-12 22:50:00  

Additional Information
 Earth MOID = .958864 au 
 Jupiter MOID = 2.57903 au 
 T_jup = 3.541 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 16.03   n/a E2021B10  

58690 (1998 BP10)          Discovered 1998-Jan-27 by Klet at Klet
Reference: 20030614/Numbers.arcLast Updated: 2004-04-19

[ 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
1940-Nov-07 04:20 < 00:01 Iris 0.034382673878515 0.0343713945277543 0.0343939540084036 4.92724181337997 4.9272417794464 2429940.680682555 0.829416265463672 618.867287030825 34.3472324143311 24.731241799301 63078.6116861719 T 19 CATAB v2.0f-lin.ifort 2020-Nov-12 22:50:03 2020-Nov-12 22:50
2047-Oct-04 04:14 < 00:01 Iris 0.0111400112488226 0.011135691961353 0.011144333314257 4.80705309165777 4.80705298430618 2468987.676364434 0.618429174812966 353.754724603081 33.1272106599034 -52.8266631862228 40167.9428317283 T 19 CATAB v2.0f-lin.ifort 2020-Nov-12 22:50:03 2020-Nov-12 22:50
2154-Aug-31 14:47 00:01 Iris 0.029700023650007 0.0296736370535431 0.0297264105098286 4.75748863505599 4.7574885943706 2508035.115722008 1.36574087882183 1322.6316751087 32.5563553516498 -6.04574622841838 14748.1513197306 T 19 CATAB v2.0f-lin.ifort 2020-Nov-12 22:50:03 2020-Nov-12 22:50
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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