GSAT 10

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GSAT 10 is classified as:

Satellite-Based Augmentation System
Geostationary

NORAD ID: 38779

Int'l Code: 2012-051B

Perigee: 35,787.1 km

Apogee: 35,800.1 km

Inclination: 0.0 °

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.

1 38779U 12051B   24118.49347731 -.00000153  00000-0  00000-0 0  9997
2 38779   0.0300 266.9299 0001536  61.4554 148.2925  1.00272387 42289

Source of the keplerian elements: AFSPC