From: European Space Agency
Posted: Thursday, November 11, 2004
On 11 November at 10:30 UTC, close to the 331st apogee, SMART-1 will be in the middle of a "weak stability boundary". In this region the spacecraft is neither in an Earth-bound orbit, nor a Moon-bound orbit: it is in no man's land.
This region is dynamically unstable. A small perturbation from an external force would be sufficient to destabilise the orbit and send the spacecraft into a chaotic trajectory resulting in a lunar impact, Earth impact or a heliocentric orbit.
The osculating orbital elements with respect to the Earth have little meaning now the spacecraft is in the transition region. The plot below, instead, shows the trajectory of SMART-1 (in red) together with that of the Moon (in green) for the period 2-20 November 2004.
SMART-1 and Moon orbit for the period 2-20 November 2004
The spacecraft is currently proceeding unpowered and is planned to enter lunar orbit on 15 November, reaching the first perilune at 17:48 UTC. After capture has taken place, SMART-1 is expected to have a polar elliptical orbit around the Moon with the following osculating elements, as computed by the ESOC specialists.
EPOCH (UTC) 2004/11/15 17:47:12.1
Elements WRT Moon (J2000)
|Pericentre Distance (km)||
|Apocentre Distance (km)||
|Semi Major Axis (km)||
|Asc. Node (deg)||
|Arg. of Pericentre (deg)||
|True Anomaly (deg)||
|Osc. Orbital Period (h)||
In this diagram the osculating orbit of the first lunar orbit is plotted.
It should be noted that the orbit plane is not polar yet, as the inclination is only 81°. The pericentre is positioned close to the South pole at 52° South latitude
Expected first lunar orbit of SMART-1 after capture on 15.11.2004
SMART-1 Project Manager
ESA/ESTEC - SCI-PD
Keplerlaan 1- 2200 AG Noordwijk, The Netherlands
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