INTELSAT 601
Satellite information INTELSAT 601 - INTELSAT 601 (IS-601)
| Spacetrack Directory Name | INTELSAT 601 |
| Alternative name | INTELSAT 601 (IS-601) |
| Follow INTELSAT 601 | INTELSAT 601 Tracker |
| Pass predictions INTELSAT 601 | Pass predictions INTELSAT 601 |
| Orbit launches |
1991-10-29 (34 years ago)
|
| Days in orbit | 12745 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| Perigee | 35959 km |
| Apogee | 36001 km |
| Orbit slope (inclination) | 13.48° |
| Laps per day | 1 |
| Height INTELSAT 601 | 35979.26 km |
Additional information INTELSAT 601
INTELSAT 601, 21765 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Tue, 29 Oct 1991 UTC via an ARIANE 44L 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 INTELSAT 601 Date of exalting 29.10.1991y. Average height of ISS INTELSAT 601 hundred 35979.26 km. Average velocity INTELSAT 601 is 11043.77 km/h. Inclination INTELSAT 601 satellite 13.46°.TLE
Average velocity INTELSAT 601
Average inclination INTELSAT 601
Mean right ascension of the ascending node (RAAN) INTELSAT 601
Mean argument of perigee INTELSAT 601
Mean semi-major axis of the orbit INTELSAT 601
Mean orbital eccentricity INTELSAT 601
ISS
Buy us a coffee!
