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17977 (1999 JR54)
Classification: Main-belt Asteroid          SPK-ID: 2017977
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 32 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2444249881794968 4.0517e-08  
a 2.662166212769049 1.1387e-08 au
q 2.011466267681118 1.0867e-07 au
i 12.94111858981561 4.3835e-06 deg
node 34.0491606526905 1.6813e-05 deg
peri 308.5631159869957 1.799e-05 deg
M 225.8485354715822 8.2917e-06 deg
tp 2459591.713163501325
(2022-Jan-12.21316350)
3.8423e-05 TDB
period 1586.540554057023
4.34
1.018e-05
2.787e-08
d
yr
n .2269087916343681 1.4559e-09 deg/d
Q 3.31286615785698 1.4171e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1650  
   data-arc span      10457 days (28.63 yr)  
   first obs. used      1991-09-12  
   last obs. used      2020-04-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .51261  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-May-20 04:43:27  

Additional Information
 Earth MOID = 1.03313 au 
 Jupiter MOID = 2.21181 au 
 T_jup = 3.306 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457085.5 (2015-Mar-04.0) TDB
Reference: JPL 32 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2419945125657311 4.0313e-08  
q 2.0218170488257 1.079e-07 au
tp 2456413.438783376746
(2013-Apr-30.93878338)
3.2993e-05 TDB
node 34.19355161044373 1.6857e-05 deg
peri 308.1487748544773 1.8062e-05 deg
i 12.91283747278449 4.3738e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      1650  
   data-arc span      10457 days (28.63 yr)  
   first obs. used      1991-09-12  
   last obs. used      2020-04-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .51261  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-May-20 04:43:27  

Additional Information
 Jupiter MOID = 2.21181 au 
 T_jup = 3.306 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.62514474239889E-15 -4.335786596923437E-15 3.449031238758243E-13 -9.519686369341475E-16 6.244304366461891E-14 8.228743981390641E-16
q -4.335786596923437E-15 1.164332275314787E-14 -9.149428550923593E-13 3.623213200265972E-15 -1.610837288657427E-13 -2.938179470009018E-15
tp 3.449031238758243E-13 -9.149428550923593E-13 1.088544213983826E-9 2.592105653722593E-12 2.310451739611645E-10 -7.597024006713866E-13
node -9.519686369341475E-16 3.623213200265972E-15 2.592105653722593E-12 2.841651166981343E-10 -2.760767999554508E-10 -2.312138622012059E-11
peri 6.244304366461891E-14 -1.610837288657427E-13 2.310451739611645E-10 -2.760767999554508E-10 3.262422649088114E-10 2.230106230440592E-11
i 8.228743981390641E-16 -2.938179470009018E-15 -7.597024006713866E-13 -2.312138622012059E-11 2.230106230440592E-11 1.912974510183113E-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 14.1   n/a MPO467902  
diameter diameter 6.095 km 0.203 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.157   0.014 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

17977 (1999 JR54)          Discovered 1999-May-10 by LINEAR at Socorro
Reference: 20001013/Numbers.arcLast Updated: 2004-04-19

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Alternate Designations
 1999 JR54 = 1991 RT24 = 1998 FC87 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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