USA 67 R/B(2)
Satellite information USA 67 R/B(2) - PAM-D
| Spacetrack Directory Name | USA 67 R/B(2) |
| Alternative name | PAM-D |
| Follow USA 67 R/B(2) | USA 67 R/B(2) Tracker |
| Pass predictions USA 67 R/B(2) | Pass predictions USA 67 R/B(2) |
| Orbit launches |
1990-11-15 (35 years ago)
|
| Days in orbit | 13081 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Type | Rocket body |
| Perigee | 203 km |
| Apogee | 20773 km |
| Orbit slope (inclination) | 24.73° |
| Laps per day | 16 |
| Height USA 67 R/B(2) | 53.23 km |
Additional information USA 67 R/B(2)
USA 67 R/B(2), 20965 is space debris in HEO originally from a launch on Thu, 15 Nov 1990 UTC launched from the Air Force Eastern Test Range (AFETR). 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 USA 67 R/B(2) Date of exalting 15.11.1990y. Average height of ISS USA 67 R/B(2) hundred 53.23 km. Average velocity USA 67 R/B(2) is 28364.59 km/h. Inclination USA 67 R/B(2) satellite 24.73°.TLE
Average velocity USA 67 R/B(2)
Average inclination USA 67 R/B(2)
Mean right ascension of the ascending node (RAAN) USA 67 R/B(2)
Mean argument of perigee USA 67 R/B(2)
Mean semi-major axis of the orbit USA 67 R/B(2)
Mean orbital eccentricity USA 67 R/B(2)
ISS
Buy us a coffee!
