INTELSAT 26 (JCSAT 4)
Satellite information INTELSAT 26 (JCSAT 4) - JCSAT-R
| Spacetrack Directory Name | INTELSAT 26 (JCSAT 4) |
| Alternative name | JCSAT-R |
| Follow INTELSAT 26 (JCSAT 4) | INTELSAT 26 (JCSAT 4) Tracker |
| Pass predictions INTELSAT 26 (JCSAT 4) | Pass predictions INTELSAT 26 (JCSAT 4) |
| Orbit launches |
1997-02-17 (29 years ago)
|
| Days in orbit | 10794 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Categories | |
| Perigee | 36135 km |
| Apogee | 36213 km |
| Orbit slope (inclination) | 12.4° |
| Laps per day | 1 |
| Orbit | GEO |
| Height INTELSAT 26 (JCSAT 4) | 36173.35 km |
Additional information INTELSAT 26 (JCSAT 4)
INTELSAT 26 (JCSAT 4), 24732 is a payload satellite owned by JSAT (US) in GEO that was launched on Mon, 17 Feb 1997 UTC via an ATLAS IIAS launch vehicle from the Air Force Eastern Test Range (AFETR). 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 INTELSAT 26 (JCSAT 4) Date of exalting 17.02.1997y. Average height of ISS INTELSAT 26 (JCSAT 4) hundred 36173.35 km. Average velocity INTELSAT 26 (JCSAT 4) is 11018.56 km/h. Inclination INTELSAT 26 (JCSAT 4) satellite 12.38°.TLE
Average velocity INTELSAT 26 (JCSAT 4)
Average inclination INTELSAT 26 (JCSAT 4)
Mean right ascension of the ascending node (RAAN) INTELSAT 26 (JCSAT 4)
Mean argument of perigee INTELSAT 26 (JCSAT 4)
Mean semi-major axis of the orbit INTELSAT 26 (JCSAT 4)
Mean orbital eccentricity INTELSAT 26 (JCSAT 4)
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