Comparing Multicarrier Ambiguity Resolution Methods for Geometry-Based GPS and Galileo Relative Positioning and Their Application to Low Earth Orbiting Satellite Attitude Determination

Table 3

Keplerian elements and other orbital information used to simulate LEO users.

	ENVISAT	ISS
Semimajor Axis (a)	7155 km	6712.5 km
Eccentricity (e)	0.0001030	0.0001202
Inclination (e)	98.5^∘	51.6^∘
Right-ascension of ascending node (Ω)	161.5^∘	51.6^∘
Argument of Perigee (ω)	0^∘	331.9^∘
Mean anomaly	263.19^∘	28.22^∘
Mean orbital altitude	790 km	338.7 km
Period	101-minutes	91.31-minutes