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97834 (2000 PN6)
Classification: Mars-crossing Asteroid          SPK-ID: 2097834
[ 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.


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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 16 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2856121842029784 4.1592e-08  
a 2.302470292030371 1.1729e-08 au
q 1.644856722861107 9.6093e-08 au
i 22.83775218180426 5.5449e-06 deg
node 148.5096370192328 1.2696e-05 deg
peri 280.6591403336333 1.5919e-05 deg
M 198.0128671231618 1.0945e-05 deg
tp 2459574.705697909745
(2021-Dec-26.20569791)		 4.1546e-05 TDB
period 1276.114019529421
3.49		 9.7513e-06
2.67e-08		 d
yr
n .282106453256233 2.1557e-09 deg/d
Q 2.960083861199635 1.508e-08 au
   Orbit Determination Parameters
   # obs. used (total)      653  
   data-arc span      7740 days (21.19 yr)  
   first obs. used      1998-02-25  
   last obs. used      2019-05-06  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .51389  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-May-30 06:30:02  

Additional Information
 Earth MOID = .80856 au 
 Jupiter MOID = 2.62024 au 
 T_jup = 3.435 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456953.5 (2014-Oct-23.0) TDB
Reference: JPL 16 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2857224735355205 4.149e-08  
q 1.644132622643402 9.5717e-08 au
tp 2457024.089917110972
(2015-Jan-01.58991711)		 3.2444e-05 TDB
node 148.5504067871607 1.2694e-05 deg
peri 280.7761149670405 1.5904e-05 deg
i 22.8395023290983 5.5453e-06 deg
   Orbit Determination Parameters
   # obs. used (total)      653  
   data-arc span      7740 days (21.19 yr)  
   first obs. used      1998-02-25  
   last obs. used      2019-05-06  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .51389  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-May-30 06:30:02  

Additional Information
 Jupiter MOID = 2.62024 au 
 T_jup = 3.435 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.721388890118675E-15 -3.955836586800463E-15 -6.026704715682574E-13 2.098847578733464E-15 -2.116486823513249E-13 -1.790840353140185E-14
q -3.955836586800463E-15 9.161700664585152E-15 1.444985978585143E-12 -3.855223857830825E-15 5.014812463745039E-13 4.216727324197622E-14
tp -6.026704715682574E-13 1.444985978585143E-12 1.052626544827364E-9 9.858133841866576E-12 3.304742489248213E-10 1.430206599966287E-11
node 2.098847578733464E-15 -3.855223857830825E-15 9.858133841866576E-12 1.611420197685568E-10 -1.453691618986789E-10 2.802370708749181E-11
peri -2.116486823513249E-13 5.014812463745039E-13 3.304742489248213E-10 -1.453691618986789E-10 2.52934052358579E-10 -2.10942479402447E-11
i -1.790840353140185E-14 4.216727324197622E-14 1.430206599966287E-11 2.802370708749181E-11 -2.10942479402447E-11 3.075024359558223E-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 15.2   n/a MPO474856  
diameter diameter 2.154 km 0.471 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2016AJ....152...63N)  
geometric albedo albedo 0.347   0.211 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2016AJ....152...63N)  

97834 (2000 PN6)          Discovered 2000-Aug-02 by LINEAR at Socorro
Reference: 20050224/Numbers.arcLast Updated: 2005-02-28

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Alternate Designations
 2000 PN6 = 1998 FF89 
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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