INSAT 2E (APR-1)
Satellite information INSAT 2E (APR-1)
| Spacetrack Directory Name | INSAT 2E (APR-1) |
| Follow INSAT 2E (APR-1) | INSAT 2E (APR-1) Tracker |
| Pass predictions INSAT 2E (APR-1) | Pass predictions INSAT 2E (APR-1) |
| Orbit launches |
1999-04-02 (27 years ago)
|
| Days in orbit | 10023 |
| Country/organisation of origin | Indie (IND) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| Perigee | 35919 km |
| Apogee | 35999 km |
| Orbit slope (inclination) | 11.51° |
| Laps per day | 1 |
| Height INSAT 2E (APR-1) | 35960.26 km |
Additional information INSAT 2E (APR-1)
INSAT 2E (APR-1), 25666 is a payload satellite owned by ISRO (IN) in GEO that was launched on Fri, 02 Apr 1999 UTC via an ARIANE 42P launch vehicle from the French Guiana (FRGUI). 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 INSAT 2E (APR-1) Date of exalting 02.04.1999y. Average height of ISS INSAT 2E (APR-1) hundred 35960.26 km. Average velocity INSAT 2E (APR-1) is 11046.25 km/h. Inclination INSAT 2E (APR-1) satellite 11.48°.TLE
Average velocity INSAT 2E (APR-1)
Average inclination INSAT 2E (APR-1)
Mean right ascension of the ascending node (RAAN) INSAT 2E (APR-1)
Mean argument of perigee INSAT 2E (APR-1)
Mean semi-major axis of the orbit INSAT 2E (APR-1)
Mean orbital eccentricity INSAT 2E (APR-1)
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