CTS
Satellite information CTS
| Spacetrack Directory Name | CTS |
| Follow CTS | CTS Tracker |
| Pass predictions CTS | Pass predictions CTS |
| Orbit launches |
1976-01-17 (50 years ago)
|
| Days in orbit | 18498 |
| Country/organisation of origin | Kanada (CA) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35749 km |
| Apogee | 35858 km |
| Orbit slope (inclination) | 3.72° |
| Laps per day | 1 |
| Height CTS | 35797.63 km |
Additional information CTS
CTS, 8585 is a payload satellite owned by CRC (CA) in GEO that was launched on Sat, 17 Jan 1976 UTC via a DELTA 2914 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 CTS Date of exalting 17.01.1976y. Average height of ISS CTS hundred 35797.63 km. Average velocity CTS is 11067.49 km/h. Inclination CTS satellite 3.76°.TLE
Average velocity CTS
Average inclination CTS
Mean right ascension of the ascending node (RAAN) CTS
Mean argument of perigee CTS
Mean semi-major axis of the orbit CTS
Mean orbital eccentricity CTS
ISS
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