THOR ALTAIR R/B
Satellite information THOR ALTAIR R/B
| Spacetrack Directory Name | THOR ALTAIR R/B |
| Follow THOR ALTAIR R/B | THOR ALTAIR R/B Tracker |
| Pass predictions THOR ALTAIR R/B | Pass predictions THOR ALTAIR R/B |
| Orbit launches |
1965-09-10 (60 years ago)
|
| Days in orbit | 22273 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 593 km |
| Apogee | 818 km |
| Orbit slope (inclination) | 98.38° |
| Laps per day | 15 |
| Height THOR ALTAIR R/B | 688.88 km |
Additional information THOR ALTAIR R/B
THOR ALTAIR R/B, 1583 is space debris in SSO originally from a launch on Fri, 10 Sep 1965 UTC launched from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
satellite THOR ALTAIR R/B Date of exalting 10.09.1965y. Average height of ISS THOR ALTAIR R/B hundred 688.88 km. Average velocity THOR ALTAIR R/B is 27048.68 km/h. Inclination THOR ALTAIR R/B satellite 98.38°.TLE
Average velocity THOR ALTAIR R/B
Average inclination THOR ALTAIR R/B
Mean right ascension of the ascending node (RAAN) THOR ALTAIR R/B
Mean argument of perigee THOR ALTAIR R/B
Mean semi-major axis of the orbit THOR ALTAIR R/B
Mean orbital eccentricity THOR ALTAIR R/B
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