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86104 (1999 RF110)
Classification: Main-belt Asteroid          SPK-ID: 2086104
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | 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 27 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .06662766422595681 3.6301e-08  
a 3.029778433738391 1.8947e-08 au
q 2.827911373576224 1.1819e-07 au
i 8.361216050064188 3.9522e-06 deg
node 297.6647202292229 3.3741e-05 deg
peri 132.3480808893723 5.7385e-05 deg
M 318.4334572728746 4.4455e-05 deg
tp 2459422.910934459293
(2021-Jul-27.41093446)		 0.00023791 TDB
period 1926.25922562222
5.27		 1.8069e-05
4.947e-08		 d
yr
n .1868907337140529 1.7531e-09 deg/d
Q 3.231645493900559 2.0209e-08 au
   Orbit Determination Parameters
   # obs. used (total)      1170  
   data-arc span      7850 days (21.49 yr)  
   first obs. used      1999-07-23  
   last obs. used      2021-01-18  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .50942  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Feb-24 07:42:42  

Additional Information
 Earth MOID = 1.85055 au 
 Jupiter MOID = 1.96642 au 
 T_jup = 3.224 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457538.5 (2016-May-30.0) TDB
Reference: JPL 27 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .06595812862353348 3.6518e-08  
q 2.831382859238432 1.1857e-07 au
tp 2457472.285498354875
(2016-Mar-24.78549836)		 0.00024085 TDB
node 297.947832472104 3.3879e-05 deg
peri 128.131568634139 5.78e-05 deg
i 8.339259201359404 3.9475e-06 deg
   Orbit Determination Parameters
   # obs. used (total)      1170  
   data-arc span      7850 days (21.49 yr)  
   first obs. used      1999-07-23  
   last obs. used      2021-01-18  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .50942  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Feb-24 07:42:42  

Additional Information
 Jupiter MOID = 1.96642 au 
 T_jup = 3.224 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.33355094586333E-15 -4.288900378234776E-15 -1.467604500415913E-12 3.618307679824012E-15 -2.612134305525783E-13 -2.602217615017504E-15
q -4.288900378234776E-15 1.405934293649927E-14 4.456618044377242E-12 -1.157701761713968E-14 7.87519795676064E-13 9.416155436444943E-15
tp -1.467604500415913E-12 4.456618044377242E-12 5.800881098178814E-8 7.183357749336299E-11 1.131524101949159E-8 2.313201222907552E-11
node 3.618307679824012E-15 -1.157701761713968E-14 7.183357749336299E-11 1.147768170937708E-9 -1.121742611976844E-9 3.890337587080514E-11
peri -2.612134305525783E-13 7.87519795676064E-13 1.131524101949159E-8 -1.121742611976844E-9 3.340817800372323E-9 -3.410696540864545E-11
i -2.602217615017504E-15 9.416155436444943E-15 2.313201222907552E-11 3.890337587080514E-11 -3.410696540864545E-11 1.558249611823495E-11

[ 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 14.14   n/a E2021B10  

86104 (1999 RF110)          Discovered 1999-Sep-08 by LINEAR at Socorro
Reference: 20040830/Numbers.arcLast Updated: 2004-09-06

[ 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
1914-Apr-29 20:22 00:03 Jupiter 1.98167707625578 1.98167659118197 1.98167756132959 4.10497800437637 3.99949874186355 2420252.348705307 2.83534344532418 66.0544504372827 20.6622910082418 83.7036087328962 3407038.03687359 T 27 CATAB v2.0f-lin.ifort 2021-Feb-24 07:42:45 2021-Feb-24 07:42
1961-Nov-09 17:10 00:02 Jupiter 1.98062734155741 1.98062684891754 1.98062783419739 4.09081836202933 3.98490747285001 2437613.215289033 1.53652537811781 68.1762893501549 20.5292908556396 82.5036554070735 3374327.51306444 T 27 CATAB v2.0f-lin.ifort 2021-Feb-24 07:42:45 2021-Feb-24 07:42
2009-May-22 12:36 < 00:01 Jupiter 1.98265073834718 1.98265024334041 1.98265123335394 4.07856662908999 3.9724389647882 2454974.025094913 0.316293017518819 69.5212494841817 20.524627241428 82.498659293509 3329349.17245178 T 27 CATAB v2.0f-lin.ifort 2021-Feb-24 07:42:45 2021-Feb-24 07:42
2056-Dec-03 02:48 00:01 Jupiter 1.9908299204468 1.99082940929458 1.99083043159915 4.07119684748004 3.96531458204374 2472335.616434306 1.13082677400928 73.3445386729232 20.8185573137024 81.8912794026774 3286351.9526035 T 27 CATAB v2.0f-lin.ifort 2021-Feb-24 07:42:45 2021-Feb-24 07:42
2104-Jun-17 09:46 00:02 Jupiter 1.99490994867889 1.99490938021477 1.99491051714346 4.04943105352999 3.94318502573124 2489697.906808941 2.44106577728678 96.9266309620411 21.1313486392083 80.6392267322716 3237313.75709373 T 27 CATAB v2.0f-lin.ifort 2021-Feb-24 07:42:45 2021-Feb-24 07:42
2151-Dec-31 16:49 00:04 Jupiter 1.99406456018558 1.99406386888368 1.99406525148963 4.01204945498813 3.90474033779979 2507061.200966643 3.77722561730589 152.775114253074 21.2652244508107 80.4701991825713 3177928.25774234 T 27 CATAB v2.0f-lin.ifort 2021-Feb-24 07:42:45 2021-Feb-24 07:42
2199-Jul-16 03:11 00:05 Jupiter 1.99637693598096 1.99637607381937 1.99637779814959 3.97648370838642 3.86831526302845 2524424.632351719 5.12829101815272 234.565024963614 21.3431619854207 81.0384727067329 3124182.15677599 T 27 CATAB v2.0f-lin.ifort 2021-Feb-24 07:42:45 2021-Feb-24 07:42
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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