THOR 1 (MARCOPOLO 2)
Satellite information THOR 1 (MARCOPOLO 2) - THOR I (MARCOPOLO 2)
| Spacetrack Directory Name | THOR 1 (MARCOPOLO 2) |
| Alternative name | THOR I (MARCOPOLO 2) |
| Follow THOR 1 (MARCOPOLO 2) | THOR 1 (MARCOPOLO 2) Tracker |
| Pass predictions THOR 1 (MARCOPOLO 2) | Pass predictions THOR 1 (MARCOPOLO 2) |
| Orbit launches |
1990-08-18 (36 years ago)
|
| Days in orbit | 13231 |
| Country/organisation of origin | Norwegia (NOR) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 36076 km |
| Apogee | 36099 km |
| Orbit slope (inclination) | 14.64° |
| Laps per day | 1 |
| Height THOR 1 (MARCOPOLO 2) | 36087.76 km |
Additional information THOR 1 (MARCOPOLO 2)
THOR 1 (MARCOPOLO 2), 20762 is a payload satellite owned by BSB (NO) in GEO that was launched on Sat, 18 Aug 1990 UTC via a DELTA 6925 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 THOR 1 (MARCOPOLO 2) Date of exalting 18.08.1990y. Average height of ISS THOR 1 (MARCOPOLO 2) hundred 36087.76 km. Average velocity THOR 1 (MARCOPOLO 2) is 11029.65 km/h. Inclination THOR 1 (MARCOPOLO 2) satellite 14.62°.TLE
Average velocity THOR 1 (MARCOPOLO 2)
Average inclination THOR 1 (MARCOPOLO 2)
Mean right ascension of the ascending node (RAAN) THOR 1 (MARCOPOLO 2)
Mean argument of perigee THOR 1 (MARCOPOLO 2)
Mean semi-major axis of the orbit THOR 1 (MARCOPOLO 2)
Mean orbital eccentricity THOR 1 (MARCOPOLO 2)
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