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)
9
8
.
5
∘
5
1
.
6
∘
Right-ascension of ascending node (Ω)
1
6
1
.
5
∘
5
1
.
6
∘
Argument of Perigee (
ω
)
0
∘
3
3
1
.
9
∘
Mean anomaly
2
6
3
.
1
9
∘
2
8
.
2
2
∘
Mean orbital altitude
790 km
338.7 km
Period
101-minutes
91.31-minutes