INSAT-3E - Wikipedia

The VWBot has performed a web search with the contents of this page, and it appears to include material copied directly from:

http://space.skyrocket.de/doc_sdat/insat-3e.htm (Copyvios report)

It will soon be reviewed to determine if there are any copyright issues. The content should not be mirrored or otherwise reused until the issue has been resolved.

If substantial content is duplicated, unless evidence is provided to the contrary (e.g. evidence of permission to use this content under terms consistent with the Wikimedia Terms of Use or public domain status; see Wikipedia:Donating copyrighted materials), editors will assume that this text is a copyright violation, and will soon delete the copy. Before removing this notice, you should:

Check if VWBot is in error: If so, simply note so on this article's discussion page.
Replace the copyrighted text with your own work. Note that simply modified or rephrased text is still an infringement—to remove the copyrighted contents you will need to completely remove them and then write totally new text to replace it.
If you hold the copyright to this text and permit its use under the terms consistent with Wikipedia's policies, please see Wikipedia:Donating copyrighted materials for instructions on how to verify the licensing.
Replace the copyrighted content with a wikified reference.
Check whether it is reasonable to revert to one of the previous versions of the article
Remove the copyrighted content if it is not critical to the article.

INSAT-3E is the fourth satellite launched in the INSAT-3 series. It is an exclusive communication satellite to further augment the communication services that are being provided by the INSAT System. Weighing 2775 kg at lift-off, INSAT-3E carries 24 Normal C-band and 12 Extended C-band transponders.