Frederic Vachier ' web page

Saturday 24th of September 2016 ~ 01:01:18 UTC (45) Eugenia occult TYC 1298-00763-1u(mag 11.0)

Download the Google Earth File KMZ
green line is the central line of (45) Eugenia
blue lines show the estimate size of (45) Eugenia
red lines the 1-sigma error for the path
white lines show Petit-Prince

Event

Max duration : 14.9 seconds
Mag drop : 2.2
Shadow velocity : 12.3 km/s
Ingress Earth : 2016-09-24 0h54
Egress Earth : 2016-09-24 1h09
Moon illumination : 43%
Moon phase : Last quarter

Asteroidal system

Name : (45) Eugenia
Mag : 13.0
Asteroid Diameter : 184 km
Geocentric distance : 2.665 AU
Number of satellite : 2

Satellite : Petit-Prince
Diameter : 7 km
Max duration : 0.6 sec

Satellite : Petite-Princesse
Diameter : 5 km
Max duration : 0.4 sec

Occulted Star

Name : TYC 1298-00763-1u
Used RA : 05:39:27.4266 J2000
Used DEC : +16:06:27.080 J2000
Mv : 11.0
VizieR - Aladin

Historic

2015-07-01 : Create prediction

Prediction for (45) Eugenia and Petit-Prince (wide views)

Eugenia

Petit-Prince

Petite-Princesse

Ephemerides from IMCCE

Ephemeris for (45) Eugenia

Ephemeris for Petit-Prince

Ephemeris from Miriade for the date of occultation and geocenter frame. For more specific ephemeris please use the documentation of Miriade.

Orbitography for the (45) Eugenia system

Petit-Prince

Astrometric observations centered on (45) Eugenia.
Dot represents one observed position. The vector shows ephemeris position from observed position.

Petit-Prince

Geometry of orbit for the (45) Eugenia system view from Earth

Cyan circle show the position of the satellite Petit-Prince at the occultation date.

The black dots show next positions during almost a period

In the center, (45) Eugenia represented by an ellipsoid

Petite-Princesse

Astrometric observations centered on (45) Eugenia.
Dot represents one observed position. The vector shows ephemeris position from observed position.

Petite-Princesse

Geometry of orbit for the (45) Eugenia system view from Earth

Cyan circle show the position of the satellite Petite-Princesse at the occultation date.

The black dots show next positions during almost a period

In the center, (45) Eugenia represented by an ellipsoid

Propagation of the solutions

We use all orbits from 1,2 and 3 sigma issued from Genetical algorithm, and we see where the satellite is for the occultation date. North on top, and East on right.

Center at coordinates 0,0 is Primary
Black dots show the orbit with the best solution at the date of occultation
Green zone show orbits covering 1-sigma error
Blue zone for 2-sigma
Red zone for 3-sigma

Petit-Prince

This figure represent 2047836 orbits computed to the occultation date. Each orbit is classify throw its performance, given an accuracy in kilometer :

1-σ error = 221.90 km
2-σ error = 240.73 km
3-σ error = 263.05 km

Petite-Princesse

This figure represent 2119524 orbits computed to the occultation date. Each orbit is classify throw its performance, given an accuracy in kilometer :

1-σ error = 246.47 km
2-σ error = 264.15 km
3-σ error = 280.20 km

Contents

Orbital solution fitted by Genoid project (Vachier F., Berthier J., Carry B. & Pajuelo M.) IMCCE/CNRS
Ephemeris has made available with Miriade Project (Berthier J. & Vachier F.) IMCCE/CNRS
Occultation Prediction by Vachier F. using Occult (Occultation Prediction Software by D.Herald)
Ephemeris and offset based on ASTORB (Edward Bowell)