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| Spacecraft Orbit Number: | 650 | ||
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| Data Downlink Rate: | 3600 bps | ||
| Spacecraft Spin Rate: | 11.94 rpm | ||
| Spin Axis Attitude: | Longitude: 344 deg Latitude: 88.8 deg |
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| Trajectory: | Periselene: 82 km Aposelene: 117 km |
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| Period: | 118 minutes duration | ||
| Inclination: | 90.0 deg | ||
| Occultations: | none | ||
| Eclipses: | 45 minutes duration |
Late last week, mission controllers exeperienced a 15-hour period in
which they could not track the vehicle. Since then, tracking allocations
have been much better, and only a few short outages are anticipated.
Ames mission controllers plan to execute the first orbit trim maneuver
over the weekend. At that time, two axial burns are scheduled: one to
raise orbital periselene (closest distance from the Moon) and one to lower
orbital aposelene (furthest distance from the Moon). Although the targeted
orbit following this maneuver will not be exactly 100 km circular, the
new orbit (87 km by 113 km) is designed to be better able to compensate
for periodic perturbations, thus maintaining the desired 100 (+ or -)
20 km orbit for a longer time.
Alison Davis
Lunar Prospector Mission Office
NASA Ames Research Center
Moffett Field, Calif. 94035
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