CCE 1 (AMPTE)
Satellite information CCE 1 (AMPTE) - AMPTE/CCE
| Spacetrack Directory Name | CCE 1 (AMPTE) |
| Alternative name | AMPTE/CCE |
| Follow CCE 1 (AMPTE) | CCE 1 (AMPTE) Tracker |
| Pass predictions CCE 1 (AMPTE) | Pass predictions CCE 1 (AMPTE) |
| Orbit launches |
1984-08-16 (42 years ago)
|
| Days in orbit | 15363 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 998 km |
| Apogee | 49783 km |
| Orbit slope (inclination) | 3.38° |
| Laps per day | 2 |
| Height CCE 1 (AMPTE) | 34774.35 km |
Additional information CCE 1 (AMPTE)
CCE 1 (AMPTE), 15199 is a payload satellite owned by GSFC (US) in HEO that was launched on Thu, 16 Aug 1984 UTC via a DELTA 3924 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 CCE 1 (AMPTE) Date of exalting 16.08.1984y. Average height of ISS CCE 1 (AMPTE) hundred 34774.35 km. Average velocity CCE 1 (AMPTE) is 10564.87 km/h. Inclination CCE 1 (AMPTE) satellite 3.41°.TLE
Average velocity CCE 1 (AMPTE)
Average inclination CCE 1 (AMPTE)
Mean right ascension of the ascending node (RAAN) CCE 1 (AMPTE)
Mean argument of perigee CCE 1 (AMPTE)
Mean semi-major axis of the orbit CCE 1 (AMPTE)
Mean orbital eccentricity CCE 1 (AMPTE)
ISS
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