GSAT 3 (EDUSAT)
Satellite information GSAT 3 (EDUSAT)
| Spacetrack Directory Name | GSAT 3 (EDUSAT) |
| Follow GSAT 3 (EDUSAT) | GSAT 3 (EDUSAT) Tracker |
| Pass predictions GSAT 3 (EDUSAT) | Pass predictions GSAT 3 (EDUSAT) |
| Orbit launches |
2004-09-20 (21 years ago)
|
| Days in orbit | 8018 |
| Country/organisation of origin | Indie (IND) |
| Starting point | SRILR (Satish Dhawan Space Centre, India) |
| Perigee | 36066 km |
| Apogee | 36076 km |
| Orbit slope (inclination) | 11.51° |
| Laps per day | 1 |
| Height GSAT 3 (EDUSAT) | 36070.64 km |
Additional information GSAT 3 (EDUSAT)
GSAT 3 (EDUSAT), 28417 is a payload satellite owned by ISRO (IN) in GEO that was launched on Mon, 20 Sep 2004 UTC via a GSLV MK I launch vehicle from the Sirharikota (SRI). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
satellite GSAT 3 (EDUSAT) Date of exalting 20.09.2004y. Average height of ISS GSAT 3 (EDUSAT) hundred 36070.64 km. Average velocity GSAT 3 (EDUSAT) is 11031.85 km/h. Inclination GSAT 3 (EDUSAT) satellite 11.49°.TLE
Average velocity GSAT 3 (EDUSAT)
Average inclination GSAT 3 (EDUSAT)
Mean right ascension of the ascending node (RAAN) GSAT 3 (EDUSAT)
Mean argument of perigee GSAT 3 (EDUSAT)
Mean semi-major axis of the orbit GSAT 3 (EDUSAT)
Mean orbital eccentricity GSAT 3 (EDUSAT)
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