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: 35,783.1 km
Apogee: 35,805.4 km
Inclination: 0.1 °
Period: 1,436.1 minutes
Semi major axis: 42165 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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1 38779U 12051B   24341.60750625 -.00000148  00000-0  00000-0 0  9992
2 38779   0.0555 256.4987 0002636 226.8162 254.3101  1.00270030 44519

Source of the keplerian elements: AFSPC