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| Spacecraft Orbit Number: | 211 |
|---|---|
| Data Downlink Rate: | 3600 bps |
| Spin Rate: | 11.94 rpm |
| Spin Axis Attitude: | |
| Longitude | 250.7 degrees |
| Latitude | 89.2 degrees |
| Trajectory: | |
| Periselene: | 86 km |
| Aposelene: | 114 km |
| Period: | 118 minutes |
| Occultations: | 43 minutes duration |
| Eclipses: | 30 minutes duration |
On Wed. Jan. 28 at 23:48 GMT, five (5) configuration commands were sent
to the Magnetometer/Electron Reflectometer instrument box.
Lunar Prospector is in its second week of mapping orbit operations and
has transitioned into a production mode. Now, telemetry and orbit ephemeris
products are routinely generated in support of science data processing.
While Lunar Prospector has no onboard tape recorders, it stores up to
53 minutes of data in solid state memory and continuously replays that
delayed stream of data, along with the real-time stream. This provides
access (that would otherwise be unavailable) to data collected during
ground station occultations -- when the spacecraft passes behind the moon
as viewed from Earth.
LP telemetry contains measurements made by each science instrument at
regular intervals. Knowing the time of the measurements and having an
orbit ephemeris indicating where the spacecraft was at those times, allows
scientists to compile a history of measurements over each region of the
moon. A very large number of measurements is required since the various
data signals being measured by each instrument are low in power and high
in noise level. It is only by taking a large number of such measurements
that the noise on the signal can be "averaged out" (since, typically,
such noise is random in nature), leaving only the true measurement behind.
Having successfully placed Lunar Prospector into the required mapping
orbit and having checked out the spacecraft, scientists and engineers
are now focusing the bulk of their attention on the important task of
science data collection and processing (while, of course, continuing to
monitor spacecraft health and other relevant vehicle and mission parameters).
David Morse
Ames Research Center
Moffett Field, CA 94035
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