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(2012 FV23)
Classification: Apollo [NEO]          SPK-ID: 3601614
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 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3669780000131549 0.00069419  
a 1.55012548580593 0.0016324 au
q .9812635352554495 4.2771e-05 au
i 1.074200693128555 0.0015807 deg
node 74.61600772264774 0.028151 deg
peri 136.6611223045333 0.021676 deg
M 176.3647335644696 2.5723 deg
tp 2458855.151194945207
(2020-Jan-06.65119494)
4.4915 TDB
period 704.9344123794377
1.93
1.1135
0.003049
d
yr
n .5106858080383038 0.00080666 deg/d
Q 2.11898743635641 0.0022314 au
  Orbit Determination Parameters
   # obs. used (total)      27  
   data-arc span      6 days  
   first obs. used      2012-03-23  
   last obs. used      2012-03-29  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      7  
   norm. resid. RMS      .421  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 06:09:07  

Additional Information
 Earth MOID = .00487089 au 
 Jupiter MOID = 2.84427 au 
 T_jup = 4.372 
[ show covariance matrix ]

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 25.4   n/a MPO226101  

[ 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
2006-Feb-10 08:05 5_08:55 Mars 0.0922362113715307 0.0290475684998697 0.222038749275336 11.9886913731323 11.9884324697965 2453776.836572700 7734.97791360877 6611708.30012586 624.49081997748 18.3636922997681 6837.04221431984 T 8 CATAB v2.0g-lin.ifort 2021-Apr-15 06:09:08 2021-Apr-15 06:09
2010-Feb-03 17:34 7_17:45 Earth 0.461219318260288 0.420285842551946 0.502163892940616 4.43195011936509 4.43064643071821 2455231.231850562 11144.5163283486 2044581.99524482 470.001312970411 4.66938208778047 3243.90849224841 T 8 CATAB v2.0g-lin.ifort 2021-Apr-15 06:09:08 2021-Apr-15 06:09
2010-Jun-19 10:06 3_19:40 Earth 0.241839466278361 0.183753889867245 0.299923298631834 13.6745383461557 13.6737326240065 2455366.920765559 5500.22402486069 2896268.29381976 441.0643408352 0.108762197081031 110.861432755961 T 8 CATAB v2.0g-lin.ifort 2021-Apr-15 06:09:08 2021-Apr-15 06:09
2012-Mar-30 06:33 < 00:01 Earth 0.0169830102559056 0.0168958000427132 0.0170702130892587 6.19078912583068 6.16539441160324 2456016.772928499 0.27313267427956 4312.5072180552 7.72824274257178 0.00656029751545639 329.81729683385 T 8 CATAB v2.0g-lin.ifort 2021-Apr-15 06:09:08 2021-Apr-15 06:09
2014-Feb-19 21:54 3_00:13 Earth 0.425524561870272 0.366905900301305 0.484156907592481 19.1781005945676 19.1777740925809 2456708.412612548 4332.87280206686 2925892.30276554 31.2281889463157 -2.3652571239851 71986.6997721354 T 8 CATAB v2.0g-lin.ifort 2021-Apr-15 06:09:08 2021-Apr-15 06:09
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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