FH 2A, 2B (ZX 1A, 1B)

ZX 1A (ChinaSat 1A)

Nation:	China
Type / Application:	Communication
Operator:
Contractors:	CAST
Equipment:
Configuration:	DFH-4 bus
Propulsion:
Power:	2 deployable solar arrays, batteries
Lifetime:	11 years
Mass:	5320 kg
Orbit:	GEO

Satellite	Date	LS		Launch Vehicle	Remarks
FH 2A (ZX 1A, ChinaSat 1A)	17.09.2011	Xi LC-2		CZ-3B/E

Further FH missions:

Further ZX (ChinaSat) missions:

ZX 1, 2, 3, 4 (DFH-2A 1, 2, 3, 4, 5) (DFH-2 Bus)
ZX 1A (ChinaSat 1A, FH 2A) (DFH-4 Bus)
ZX 2A (ChinaSat 2A, ST 2) (DFH-4 Bus)
ZX 5, 5R (ChinaSat 5, 5R) (AS-3000)
ZX 5A (ChinaSat 5A) (A2100A)
ZX 5B (ChinaSat 5B) (Spacebus-3000A)
ZX 5C (ChinaSat 5C) (DFH-3 Bus)
ZX 5D, 5E (ChinaSat 5D, 5E) (HS-376)
ZX 6 (ChinaSat 6) (DFH-3 Bus)
ZX 6A (ChinaSat 6A) (DFH-4 Bus)
ZX 6B (ChinaSat 6B) (Spacebus-4000C2)
ZX 7 (ChinaSat 7) (HS-376)
ZX 8 (ChinaSat 8) (LS-1300)
ZX 9 (ChinaSat 9) (Spacebus-4000C2)
ZX 9A (ChinaSat 9A) (DFH-4 Bus)
ZX 10 (ChinaSat 10) (DFH-4 Bus)
ZX 11 (ChinaSat 11) (DFH-4 Bus)
ZX 12 (ChinaSat 12) → ZX 15A (Spacebus-4000C2)
ZX 15 (ChinaSat 15) (DFH-4 Bus)
ZX 20, 20A (ST 1, 1B) (DFH-3 Bus)
ZX 22, 22A (FH 1A, 1B) (DFH-3 Bus)