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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2021
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Article
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Tab 3
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Research Article
The
Relative Perturbation Analysis of Satellite Formation under the Requirement of Relative Position Maintenance with Millimeter-Level Accuracy
Table 3
Initial orbit parameters when the two satellites are 100 m apart.
Parameter name
Satellite 1
Satellite 2
Semimajor axis (km)
6878.14
6878.14
Eccentricity
0
0
Inclination (°)
97.4065
97.4065
RAAN (°)
0
0
Argument of perigee (°)
0
0
True anomaly (°)
0
0.000833015