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Intelsat 5A
 Part of the Intelsat program
  The Intelsat 5A series is very similar to the Intelsat 5 series. Modifications include a larger communications payload with internal weight savings to accommodate the additional mass. The 5A series (F1-F6) is also known as Intelsat 5 (F10-F15).
 Spacecraft
3-axis stabilized to 0.4 deg with momentum wheels. Hydrazine propulsion system. Passive thermal control. Dual solar arrays provide 1800 W (BOL). Nickel hydrogen batteries.
 Payload
26 C-Band and 6 Ku-Band transponders. 15000 voice circuits and 2 TV channels.
 
| Country of Origin | International |  | Customer/User | ITSO |  | Manufacturer(s) | Ford Aerospace |  | Size | 1.6 x 2.1 x 2.8 m box, 15.9 m solar array span |  | Orbit | F10: GEO over Pacific / F11: GEO over Indian Ocean / F12: GEO over Atlantic / F13: GEO over Atlantic / F15: GEO over Indian Ocean |  | Design Life | 9 years |  Launch Facts
 
|  |  |  |  | Name | Int'l Desig. | Date | Site | Vehicle | Orbit | Mass(kg) |  | Notes |  |  |  |  |  | Intelsat 5A F-10 | 1985-025A | 3/22/85 | ESMC | Atlas Centaur | GEO | 2013 |  |  |  |  |  | Intelsat 5A F-11 | 1985-055A | 6/30/85 | ESMC | Atlas Centaur | GEO | 1098 |  |  |  |  |  | Intelsat 5A F-12 | 1985-087A | 9/29/85 | ESMC | Atlas Centaur | GEO | 1096 |  | Telephone communications; 31 deg E |  |  |  | Intelsat 5A F-14 | none | 5/30/86 | Kourou | Ariane 2 | FTO |  |  | 3rd stage failed to ignite; destroyed by range safety |  |  |  | Intelsat 5A F-13 | 1988-040A | 5/17/88 | Kourou | Ariane 2 | GEO | 2013 |  | Replaced Intelsat 5 F-3; 53 deg W |  |  |  | Intelsat 5A F-15 | 1989-006A | 1/27/89 | Kourou | Ariane 2 | GEO | 1977 |  | International communications; 18 deg W |  |  |      ![[MSL Home]](../buttons/msl.gif)  ![[Feedback]](../buttons/feedback.gif)  ![[Glossary]](../buttons/glossary.gif)  Information in The Mission and Spacecraft Library is provided without 
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