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JPL Small-Body Database Browser
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(2017 RV1)
Classification: Apollo [NEO, PHA]          SPK-ID: 3781388
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | 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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 42 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .628044740949703 7.9396e-07  
a 2.424700844668217 4.9328e-06 au
q .9018802307980408 1.0215e-07 au
i 2.045548123457872 1.6448e-06 deg
node 292.2973639627071 0.00014341 deg
peri 123.0279445567651 0.00014421 deg
M 139.6465925401171 0.00042325 deg
tp 2458065.549602139094
(2017-Nov-08.04960214)
1.2232e-05 TDB
period 1379.067972421897
3.78
0.0042084
1.152e-05
d
yr
n .2610458709789146 7.9661e-07 deg/d
Q 3.947521458538394 8.0309e-06 au
  Orbit Determination Parameters
   # obs. used (total)      504  
   # delay obs. used      1  
   # Doppler obs. used      1  
   data-arc span      260 days  
   first obs. used      2017-07-05  
   last obs. used      2018-03-22  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      3  
   norm. resid. RMS      .32603  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Apr-15 06:24:48  

Additional Information
 Earth MOID = .0112684 au 
 Jupiter MOID = 1.45205 au 
 T_jup = 3.208 
[ 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 20.1   n/a MPO438037  
rotation period rot_per 3.4460 h n/a LCDB (Rev. 2019-January); Warner et al., 2009 Result based on less than full coverage, so that the period may be wrong by 30 percent or so.
Published Reference List:
[Pravec, P.; Fatka, P.; Kusnirak, P.; Moskovitz, N.; et al. (2017) CBET 4435.]

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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