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The Jason-1
Project should be ready to start distributing GDRs approximately
30 days after the end of Cycle 46. The distribution of GDR products
from cycle 46 onwards is based on the same data product latency
as for TOPEX/POSEIDON (approximately 30 days after the end of
the cycle). Reprocessed GDR products for cycles 1 to 45 will
gradually be made available once they have been processed and
validated. The expected completion date for reprocessed GDR
cycles is September 2003.
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The first
Jason-1 cycle began January 15, 2002 and corresponds to T/P
cycle 344. Here is a list of all T/P cycle start times: http://oceanesip.jpl.nasa.gov/sealevel/TopexCycleTimes.txt
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The orbit
accuracy for the Jason IGDR is approximately 3 cm, which is
comparable to the orbit accuracy for the Topex GDR.
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The following
fields have new algorithms in the Jason-1 Science Data Products:
- ocean
tides
- mean
sea surface
- geoid
- sea
state bias (instrument dependent)
- inverted
barometer correction
- wind
speed
- rain
flag
- land
flag
The Topex/Poseidon
and Jason-1 orbits also differ.
To form
a compatible data set with Topex/Poseidon GDRs or MGDRs, it
is recommended to use the Topex GDR Correction Product (GCP)
developed by Phil Callahan. For more information contact jason@podaac.jpl.nasa.gov
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The GDR
is identical to the IGDR except for the following points: a
more precise orbit is used, improved pole location data are
used, and DORIS TEC grids are used. These differences affect
the following parameters:
- latitude
[latitude]
- longitude
[longitude]
- altitude
[altitude, orb_state_flag and alt_hi_rate]
- orbital
altitude rate [orb_alt_rate]
- net
sum of the instrumental corrections (update of the Doppler
correction) [net_instr_corr_ku and net_instr_corr_c]
- corrected
ground retracked altimeter ranges [range_ku and range_c]
- altimeter
ionospheric correction [iono_corr_alt_ku]
- DORIS
ionospheric correction [iono_corr_doris_ku]
- pole
tide height [pole_tide]
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The following
is a condensed version of the
Topex/Poseidon Satellite Attitude Event Information and
contains the start and stop times of the yaw state.
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The following
is the complete
Jason-1 Satellite Attitude Event Information.