| Semi-major axis | 7,714.43 km |
| Eccentricity | 0.000095 |
| Inclination | 66.04° |
| Argument of periapsis | 90.0° |
| Inertial longitude of the ascending node | 116.56° |
| Mean anomaly | 253.13° |
| Reference altitude | 1,336 km |
| Nodal period | 6,745.72 sec |
| Repeat period | 9.9156 days |
| Number of revolutions within a cycle | 127 |
| Number of passes within a cycle | 254 |
| Equatorial cross track separation | 315 km |
| Ground track control band | +1 km |
| Acute angle at Equator crossings | 39.5° |
| Longitude of Equator crossing of pass 1, cycles 1-365 | 99.9249° |
| Longitude of Equator crossing of pass 1, cycles 369-onward | 98.5° |
| Inertial nodal rate | -2.08°/day |
| Orbital speed | 7.2 km/s |
| Ground track speed | 5.8 km/s |
TOPEX/Poseidon was a joint altimetric mission between NASA and the Centre national d'études spatiales (CNES), the French space agency. It operated until Oct. 18, 2005, and collected 481 cycles of data. TOPEX/Poseidon was capable of measuring significant wave height, sigma naught (sigma0), dry and wet troposphere, and ionosphere, which can be used to calculate sea surface height and anomalies and total electron content.
TOPEX/Poseidon had a repeat period of approximately 10 days with 254 passes per cycle.
TOPEX/Poseidon began a drift maneuver on August 15, 2002, cycle 365, pass 111, and ended on September 16, 2002, cycle 368, pass 171. During this time, the satellite moved to a different orbit so that it and Jason-1 (which remained on the original orbit) would survey the Earth in a shorter amount of time and give a higher spatial resolution. Lists of cycle start times, maneuvers performed to maintain orbit, safe holds, and periods of no data collection are provided in the "Documentation" tab.
Type
Data Center
Launch
Objective
Switch Between TOPEX-A and TOPEX-B
Errors in MGDR-B
In the MGDR version B data cycles 1-190 there were some small errors, mostly the incorrect default values were placed in the data, but the flags are correct. View a full list of the errors.
Early Pointing Angle Problems
From cycle 1 through cycle 8 pass 189 (23 September through 8 December 1992, day of year, DOY, 343), the satellite attitude control system was not properly calibrated. This resulted in pointing the altimeter relatively far from nadir (typically 0.3, but up to 0.6) with a sinusoidal signature over each pass much of the time. Since the pointing angle/sea state corrections are less accurate for angles larger than about 0.3 and the geometric pointing correction cannot be done, these data will be less accurate than later data. The pointing calibration was improved on 1992 DOY 353 and 357 and 1993 DOY 046, but these changes were minor compared to the initial calibration on 1992 DOY 343. The user may want to begin analysis on data beginning with cycle 11.
Sigma0 Calibration
View a list of calibrations for the TOPEX backscatter.
The calibrations are provided to improve the sigma0 values provided by the project that are found in the Geophysical Data Record (GDRs). If you are using the merged GDRS, the calibrations have been applied to cycles 1-132, otherwise you need to apply the calibrations to the other cycles yourself. If you are applying the Generalized Predictive Control (GPC) correction to the GDR, it contains the calibration corrections.
Instruments Aboard TOPEX/Poseidon
Related Platforms
Frequently Asked Questions
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