Orbit accuracy assessment for Seasat
Abstract
Laser range measurements are used to determine the orbit of Seasat during the period from July 28, 1978, to Aug. 14, 1978, and the influence of the gravity field, atmospheric drag, and solar radiation pressure on the orbit accuracy is investigated. It is noted that for the orbits of three-day duration, little distinction can be made between the influence of different atmospheric models. It is found that the special Seasat gravity field PGS-S3 is most consistent with the data for three-day orbits, but an unmodeled systematic effect in radiation pressure is noted. For orbits of 18-day duration, little distinction can be made between the results derived from the PGS gravity fields. It is also found that the geomagnetic field is an influential factor in the atmospheric modeling during this time period. Seasat altimeter measurements are used to determine the accuracy of the altimeter measurement time tag and to evaluate the orbital accuracy.
- Publication:
-
Journal of the Astronautical Sciences
- Pub Date:
- December 1980
- Bibcode:
- 1980JAnSc..28..371S
- Keywords:
-
- Laser Ranger/Tracker;
- Orbital Position Estimation;
- Satellite Orbits;
- Seasat Satellites;
- Atmospheric Effects;
- Error Analysis;
- Gravitational Effects;
- Position Errors;
- Radiation Pressure;
- Satellite Drag;
- Astrodynamics