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5698 Nolde (4121 T-1)
Classification: Main-belt Asteroid          SPK-ID: 2005698
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 38 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1113538843869232 2.9707e-08  
a 3.120055770107342 1.4177e-08 au
q 2.772625440602057 9.4669e-08 au
i 1.552924652438641 3.3391e-06 deg
node 74.11219613234151 0.00014531 deg
peri 157.783554276412 0.00014638 deg
M 308.3857089367064 1.8633e-05 deg
tp 2459289.108706335396
(2021-Mar-15.60870634)
0.00010459 TDB
period 2012.991598651103
5.51
1.372e-05
3.756e-08
d
yr
n .1788383022766883 1.2189e-09 deg/d
Q 3.467486099612627 1.5756e-08 au
  Orbit Determination Parameters
   # obs. used (total)      2638  
   data-arc span      17983 days (49.23 yr)  
   first obs. used      1971-03-24  
   last obs. used      2020-06-17  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .46994  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Jun-23 16:23:01  

Additional Information
 Earth MOID = 1.7619 au 
 Jupiter MOID = 1.5216 au 
 T_jup = 3.206 
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Orbital Elements at Epoch 2456606.5 (2013-Nov-10.0) TDB
Reference: JPL 38 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1124400713969357 3.0045e-08  
q 2.775187993459229 9.5979e-08 au
tp 2457265.274605347011
(2015-Aug-30.77460535)
0.00010063 TDB
node 74.19769835423631 0.00014476 deg
peri 155.804506474224 0.0001458 deg
i 1.555147412866735 3.3435e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      2638  
   data-arc span      17983 days (49.23 yr)  
   first obs. used      1971-03-24  
   last obs. used      2020-06-17  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .46994  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Jun-23 16:23:01  

Additional Information
 Jupiter MOID = 1.5216 au 
 T_jup = 3.206 
Orbit Covariance (6×6)
  e q tp node peri i
e 9.026842631073252E-16 -2.858474415539077E-15 -4.493404905268509E-13 -4.020747233303226E-15 -5.872125140270226E-14 -8.077203250307298E-17
q -2.858474415539077E-15 9.211911438044044E-15 1.606263961733292E-12 2.008220468654467E-14 1.994142898933759E-13 2.74921547464989E-16
tp -4.493404905268509E-13 1.606263961733292E-12 1.012586662612303E-8 2.76361028853232E-12 1.769581092344445E-9 2.629837966946976E-13
node -4.020747233303226E-15 2.008220468654467E-14 2.76361028853232E-12 2.095625813356022E-8 -2.094814147579527E-8 2.048154853186878E-11
peri -5.872125140270226E-14 1.994142898933759E-13 1.769581092344445E-9 -2.094814147579527E-8 2.125780784777907E-8 -2.042896617806697E-11
i -8.077203250307298E-17 2.74921547464989E-16 2.629837966946976E-13 2.048154853186878E-11 -2.042896617806697E-11 1.117917924363638E-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 12.7   n/a MPO502208  
diameter diameter 16.690 km 0.097 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.048   0.008 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2012ApJ...759L...8M)  

5698 Nolde (4121 T-1)          Discovered 1971-Mar-26 by van Houten and Gehrels at Palomar
Reference: DISCOVERY.DBLast Updated: 2003-08-29

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Alternate Designations
 4121 T-1 = 1977 KP1 = 1978 RT8 = 1985 YX1 = 1990 WA3 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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