INTELSAT 604
Satellite information INTELSAT 604 - INTELSAT 604 (IS-604)
| Spacetrack Directory Name | INTELSAT 604 |
| Alternative name | INTELSAT 604 (IS-604) |
| Follow INTELSAT 604 | INTELSAT 604 Tracker |
| Pass predictions INTELSAT 604 | Pass predictions INTELSAT 604 |
| Orbit launches |
1990-06-23 (36 years ago)
|
| Days in orbit | 13226 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 36276 km |
| Apogee | 36343 km |
| Orbit slope (inclination) | 14.67° |
| Laps per day | 1 |
| Height INTELSAT 604 | 36309.69 km |
Additional information INTELSAT 604
INTELSAT 604, 20667 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Sat, 23 Jun 1990 UTC via a COMMERCIAL TITAN 3 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 604 Date of exalting 23.06.1990y. Average height of ISS INTELSAT 604 hundred 36309.69 km. Average velocity INTELSAT 604 is 11000.98 km/h. Inclination INTELSAT 604 satellite 14.66°.TLE
Average velocity INTELSAT 604
Average inclination INTELSAT 604
Mean right ascension of the ascending node (RAAN) INTELSAT 604
Mean argument of perigee INTELSAT 604
Mean semi-major axis of the orbit INTELSAT 604
Mean orbital eccentricity INTELSAT 604
ISS
Buy us a coffee!
