Error Modeling and Analysis for InSAR Spatial Baseline Determination of Satellite Formation Flying

Table 1

Orbit elements of formation satellites.

Parameters of satellites	Satellite 1	Satellite 2
Semimajor axis	6886478 m	6886478 m
Inclination	97.4438°	97.4438°
Eccentricity	0.00117	0.001073
Argument of perigee	90°	90°
Right ascension of ascending node	0°	0.01171°
True anomaly	269.99677°	270.00622°