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(2000 SM10)
Classification: Apollo [NEO]          SPK-ID: 3050514
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 21 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5405199186120381 3.909e-07  
a 1.665029298956521 3.8634e-09 au
q .7650477977978837 6.5186e-07 au
i .5523811672665606 1.9529e-06 deg
node 259.7588850577363 0.00093028 deg
peri 177.5208053561672 0.00092105 deg
M 221.4497877148006 1.3039e-05 deg
tp 2459698.520165843856
(2022-Apr-29.02016584)
2.7876e-05 TDB
period 784.7498600722309
2.15
2.7313e-06
7.478e-09
d
yr
n .4587449049903168 1.5967e-09 deg/d
Q 2.565010800115159 5.9517e-09 au
  Orbit Determination Parameters
   # obs. used (total)      186  
   data-arc span      5484 days (15.01 yr)  
   first obs. used      2000-09-23  
   last obs. used      2015-09-29  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .46321  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-14 20:58:36  

Additional Information
 Earth MOID = .00870811 au 
 Jupiter MOID = 2.72863 au 
 T_jup = 4.077 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456471.5 (2013-Jun-28.0) TDB
Reference: JPL 21 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5400270490938136 3.9199e-07  
q .7646828397784532 6.4932e-07 au
tp 2456561.308335054471
(2013-Sep-25.80833505)
3.4907e-05 TDB
node 260.6218229759277 0.00093901 deg
peri 176.6810031394083 0.00093088 deg
i .5485783805565559 1.9038e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      186  
   data-arc span      5484 days (15.01 yr)  
   first obs. used      2000-09-23  
   last obs. used      2015-09-29  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .46321  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-14 20:58:36  

Additional Information
 Jupiter MOID = 2.72863 au 
 T_jup = 4.077 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.536537961626902E-13 -2.545251527681876E-13 1.350325171178157E-11 4.585860661247791E-11 -9.510547077095641E-12 3.296362041380132E-13
q -2.545251527681876E-13 4.216170850580287E-13 -2.236702414659239E-11 -7.597452465115557E-11 1.576476721145904E-11 -5.460208763240032E-13
tp 1.350325171178157E-11 -2.236702414659239E-11 1.218470754243592E-9 5.35996700883464E-9 -2.145724343781803E-9 3.045507534016418E-11
node 4.585860661247791E-11 -7.597452465115557E-11 5.35996700883464E-9 8.817398201610046E-7 -8.698312084032522E-7 -1.029914397941969E-9
peri -9.510547077095641E-12 1.576476721145904E-11 -2.145724343781803E-9 -8.698312084032522E-7 8.66536398747825E-7 1.108839351119158E-9
i 3.296362041380132E-13 -5.460208763240032E-13 3.045507534016418E-11 -1.029914397941969E-9 1.108839351119158E-9 3.624502862721798E-12

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 24.1   n/a MPO05065  
rotation period rot_per 18. h n/a LCDB (Rev. 2020-October); Warner et al., 2009 lower-limit; Result based on less than full coverage, so that the period may be wrong by 30 percent or so.
Published Reference List:
[Pravec, P.; Wolf, M.; Sarounova, L. (2000) http://www.asu.cas.cz/~ppravec/neo.htm]

[ show close-approach data ]
Alternate Designations
 2000 SM10 = 2015 RF2 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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