Changes in accuracy of gravity recovery due to ground track variability: GRACE, CHAMP, and
GOCE
Changes in accuracy of gravity recovery due to ground track variability: GRACE, CHAMP, and GOCE
HR: 1340h
AN: G33A-0897 [Abstracts]
TI: Changes in accuracy of gravity recovery due to ground track variability: GRACE, CHAMP, and GOCE Changes in accuracy of gravity recovery due to ground track variability: GRACE, CHAMP, and GOCE
AU: * Klokocnik, J
EM: jklokocn@asu.cas.cz
AF: Astronom. Inst. Czech Acad. Sci., CZ 251 65 Ondrejov observatory
Czech Republic, Ondrejov, 251 65, Czech Republic
AU: Wagner, C A
EM: Carl.Wagner@noaa.gov
AF: NOAA, Lab. Satel. Altimetry, Silver Spring, MD, Silver Spring, 20910-3226, United States
AU: McAdoo, D
EM: Dave.McAdoo@noaa.gov
AF: NOAA, Lab. Satel. Altimetry, Silver Spring, MD, Silver Spring, 20910-3226, United States
AU: Kostelecky, J
EM: kost@fsv.cvut.cz
AF: Research Inst. of Geodesy, CZ 250 66 Zdiby 98, Zdiby, 250 66, Czech Republic
AU: Bezdek, A
EM: bezdek@asu.cas.cz
AF: Astronom. Inst. Czech Acad. Sci., CZ 251 65 Ondrejov observatory
Czech Republic, Ondrejov, 251 65, Czech Republic
AU: Novak, P
EM: Pavel.Novak@pecny.cz
AF: Dept. Math. Fac. Applied Sci., West Bohemian Univ., Universitni 6, Plzen, Plzen, 300 80,
Czech Republic
AU: Gruber, C
EM: gruber@asu.cas.cz
AF: Astronom. Inst. Czech Acad. Sci., CZ 251 65 Ondrejov observatory
Czech Republic, Ondrejov, 251 65, Czech Republic
AB:
Following an earlier recognition of degraded monthly geopotential recovery from GRACE (Gravity Recovery And
Climate Experiment) due to prolonged passage through a short repeat (low order resonant) orbit, we extend
these insights to the whole of this and other current and future continuous tracking missions, in particular to
CHAMP (CHAllenging Minisatellite Payload) and GOCE (Gravity field and steady state Ocean Circulation Explorer).
The extension from geopotential results for exact repeat missions to the general case for non-repeat free-falling
orbits is made through the proxy of the satellite ground track density, in particular its maximum spacing in
longitude over a given period of time. We illustrate wide track-density variations over time for these orbits in both
latitude and longitude and estimate geopotential recovery will be as widely affected as well within these regimes;
lesser density of the tracks leading to poorer recoveries. We have used recent models of atmospheric density to
estimate minimum and maximum drag and the orbit decrease of GRACE and provide a warning of future
degraded performance as other low order resonances are encountered. We have also found the variations of the
densities of the ground tracks of CHAMP correlate well with quality of geopotential parameters derived from this
satellite. Finally, implications for the GOCE orbit are also discussed, with some suggestions for its orbit in the
scheduled measuring phases of this mission, to avoid low-order resonances.
DE: 1214 Geopotential theory and determination (0903)
DE: 1217 Time variable gravity (7223, 7230)
DE: 1240 Satellite geodesy: results (6929, 7215, 7230, 7240)
SC: Geodesy [G]
MN: 2007 Fall Meeting