| Display title | Engineering:GSAT-6A |
| Default sort key | GSAT-6A |
| Page length (in bytes) | 13,537 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 1000044 |
| Page content language | en - English |
| Page content model | wikitext |
| Indexing by robots | Allowed |
| Number of redirects to this page | 0 |
| Counted as a content page | Yes |
| Page image |  |
| HandWiki item ID | None |
| Edit | Allow all users (infinite) |
| Move | Allow all users (infinite) |
| Page creator | imported>Raymond Straus |
| Date of page creation | 18:53, 4 February 2024 |
| Latest editor | imported>Raymond Straus |
| Date of latest edit | 18:53, 4 February 2024 |
| Total number of edits | 1 |
| Recent number of edits (within past 90 days) | 0 |
| Recent number of distinct authors | 0 |
Description | Content |
Article description: (description)
This attribute controls the content of the description and og:description elements. | GSAT-6A was a communication satellite launched by the Indian Space Research Organisation (ISRO) It featured a 6-metre (20 ft) unfurlable S-band antenna similar to the one used on GSAT-6. Around 17 minutes after lift-off, the three stage GSLV Mk.II rocket flying on GSLV F08 mission successfully injected... |
