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GSAT 10

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GSAT 10 is classified as:


NORAD ID: 38779
Int'l Code: 2012-051B
Perigee: 35,780.4 km
Apogee: 35,806.8 km
Inclination: 0.1 °
Period: 1,436.1 minutes
Semi major axis: 42164 km
RCS: 8.7376 m2 (large)
Launch date: September 28, 2012
Source: India (IND)
Launch site: FRENCH GUIANA (FRGUI)

GSAT-10 is a geostationary satellite operated by the Indian Space Research Organisation's GSAT-10, which carries Ku- and C-band transponders for relay services. Configured with 12 Ku-band, 12 C-band and 12 extended C-band transponders, GSAT-10 utilizes the I-3K satellite bus developed by ISRO, with a power capability of some six kilowatts and a liftoff mass estimated at 3,400 kg.
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NASA's NSSDC Master Catalog

Two Line Element Set (TLE):
1 38779U 12051B   19115.53382942 -.00000179 +00000-0 +00000-0 0  9994
2 38779 000.1010 094.8276 0003132 333.7711 059.8423 01.00272432023959
Source of the keplerian elements: AFSPC