NSS K (INTELSAT K)
Satellite information NSS K (INTELSAT K) - INTELSAT 101
| Spacetrack Directory Name | NSS K (INTELSAT K) |
| Alternative name | INTELSAT 101 |
| Follow NSS K (INTELSAT K) | NSS K (INTELSAT K) Tracker |
| Pass predictions NSS K (INTELSAT K) | Pass predictions NSS K (INTELSAT K) |
| Orbit launches |
1992-06-10 (34 years ago)
|
| Days in orbit | 12508 |
| Country/organisation of origin | Holandia (NETH) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 36311 km |
| Apogee | 37040 km |
| Orbit slope (inclination) | 15.04° |
| Laps per day | 1 |
| Height NSS K (INTELSAT K) | 36674.67 km |
Additional information NSS K (INTELSAT K)
NSS K (INTELSAT K), 21989 is a payload satellite owned by INTELSAT (NL) in GEO that was launched on Wed, 10 Jun 1992 UTC via an ATLAS IIA 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 NSS K (INTELSAT K) Date of exalting 10.06.1992y. Average height of ISS NSS K (INTELSAT K) hundred 36674.67 km. Average velocity NSS K (INTELSAT K) is 10954.55 km/h. Inclination NSS K (INTELSAT K) satellite 15.03°.TLE
Average velocity NSS K (INTELSAT K)
Average inclination NSS K (INTELSAT K)
Mean right ascension of the ascending node (RAAN) NSS K (INTELSAT K)
Mean argument of perigee NSS K (INTELSAT K)
Mean semi-major axis of the orbit NSS K (INTELSAT K)
Mean orbital eccentricity NSS K (INTELSAT K)
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