Actualités
[Jason-1] Start of Geodetic Phase
The Cnes-Nasa Joint Steering Group directed the Jason-1 Project to move the satellite to a geodetic orbit.

As mentioned in a previous <link http: www.aviso.oceanobs.com fr actualites _top external-link-new-window>operational news, the Cnes-Nasa Joint Steering Group directed the Jason-1 Project to move the satellite to a geodetic orbit.
Maneuvers
The target orbit was 12+297/406 with a mean altitude at the Equator of 1323.4 km.
Jason-1 maneuver operations were started on April 23rd with this baseline, and the first operations to lower the orbit were performed on April 25th.
After an initial series of 4 maneuvers were completed, we encountered a serious new propulsion anomaly which resulted in the unexpected overconsumption of hydrazine.
A 5th maneuver was designed in order to correct orbital eccentricity. At the time of this new anomaly, Jason-1 was -12.0 km below the reference altimetric orbit with 600m remaining to reach the -12.6 km goal, however there were very few grams of fuel remaining in the tank to continue orbit lowering.
Final orbit
After checking the current orbit carefully, the operational team determined that a geodetic mission was still possible. It was also decided to preserve all remaining fuel for future station keeping maneuvers which is mandatory in a geodetic orbit. Core payloads were switched ON on May 4th and after some POSEIDON2 radar (PRF) adjustments the mission was resumed on May 7th at 15:12:48 UTC.
Below are the characteristics of the new orbit which will be maintained, as before, within +/- 1km control box at the Equator:
Semi major axis: | 7702.437 km |
Eccentricity: | 1.3 to 2.8 10-4 |
Altitude equator: | 1324.0 km |
Orbital period: | 6730s (1h52'10'') |
Inclination: | 66.042° |
Cycle: | 406 days |
Sub cycles: | 3.9 - 10.9 - 47.5 - 179.5 days |
Products
The ground team is currently preparing for the restart of ground processing operations. For this new phase of the Jason-1 mission, the cycle numbering will restart at 500 and the first OSDRs should be produced within a few hours. Off-line products will be produced once a day for the IGDR, and every 11 days for the GDR's.
We will provide more detailed information as soon as the first science measurements on the new orbit become available.