Research Article
Comparison between Two Methods to Calculate the Transition Matrix of Orbit Motion
Table 2
Keplerian parameters of the test orbits.
| Parameter | Topex/Poseidon | Molniya |
| Semiaxis major | 7714423.46 m | 26563000.0 m | Eccentricity | | 0.75 | Inclination | 66°.039 | 63°.435 | Longitude of node | 236°.72 | 0°.0 | Argument of perigee | 102°.83 | 270°.0 | Mean anomaly | 153°.54 | 0°.0 |
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