Earth, Planets and Space

Table 1 Summary of our synthetic test cases

From: Dipolar elementary current systems for ionospheric current reconstruction at low and middle latitudes

	T1	T2	T3	T4	T5	T6	T7	T8
Swarm-A long	\(195^\circ\)	\(195^\circ\)	\(195^\circ\)	\(315^\circ\)	\(315^\circ\)	\(315^\circ\)	\(195^\circ\)	\(195^\circ\)
Day	Sep-23	Sep-23	Sep-23	Sep-23	Sep-23	Sep-23	Jun-21	Jun-21
UT hour	18	22	02	10	15	19	18	21
LT hour	07	11	15	07	12	16	07	10

Orbit of Swarm-C is \(5^\circ\) eastward of Swarm-A. Orbital altitude is 442 km and inclination is assumed to be \(90^\circ\)

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